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MBB/Kawasaki BK 117

The MBB/Kawasaki BK 117 is a twin-engined light utilitytransport helicopter. It was jointly developed and manufactured by Messerschmitt-Bölkow-Blohm (MBB) of Germany and Kawasaki of Japan. MBB was later purchased by Daimler-Benz and eventually became a part of Eurocopter, which was later rebranded as Airbus Helicopters.

BK 117
A BK 117 of the German police
Role Utility/transport
National origin Germany/Japan
Manufacturer Messerschmitt-Bölkow-Blohm (MBB)/Kawasaki Heavy Industries
First flight 13 June 1979
Introduction 9 December 1982
Status in production, in active service
Primary users DRF
ADAC
Produced 1979–present
Developed into Eurocopter EC145

On 25 February 1977, MBB and Kawasaki signed a cooperative agreement to abandon their independent efforts to design twin-engined general purpose helicopters in favour of a collaborative venture to development of a new rotorcraft for that role. While the programme's costs were shared equally, the workshare was divided into certain areas of the design. MBB utilised their expertise with the rigid rotor system used on the earlier Bo 105 to develop the majority of the dynamic systems and flight controls, while Kawasaki focused on the airframe, structural elements, and various other components. On 13 June 1979, MBB's flying prototype conducted its maiden flight at Ottobrunn, Bavaria, Germany; months later, it was followed by the Kawasaki prototype at Gifu, Chūbu region, Japan on 10 August 1979.

Each company established their own final assembly line, producing the BK 117 for their respective regions. The BK 117 has proven to be popular for passenger services and VIP-transport, the cabin can be outfitted with various seating configurations, seating between seven and ten passengers. It is also used for a diverse range of operations, such as aerial crane and sling work, law enforcement, and military transport, and is exceptional as an air ambulance and search and rescue platform. During the 1990s, due to its popularity, a refined derivative, initially marketed as the BK 117 C-2 before being rebranded as the EC 145 and later as the H145, was developed from the BK 117 C-1 version; this improved version of the rotorcraft has since succeeded the original BK 117 in production.

Development

Origins

According to aviation author J. Mac. McCellan, the BK 117 has its origins in an earlier rotorcraft designed and produced by German aerospace manufacturer Messerschmitt-Bölkow-Blohm (MBB), the MBB Bo 105.[1] This helicopter, which proved to be a commercial success, had made use of a revolutionary hingeless main rotor composed of fibreglass, which was developed by German engineer Ludwig Bölkow. Having established a reputation for reliability and safety, during the early 1970s MBB, along with one of its major shareholders, Boeing Vertol, began studying options for producing an enlarged derivative of the type to accompany the Bo 105.[2] However, Boeing soon withdrew from the venture, leading to MBB searching for another partner; this was found in the form of Japanese company Kawasaki Heavy Industries.[3]

On 25 February 1977, MBB and Kawasaki signed an agreement to cooperate on the development of a new rotorcraft. Under the terms of this agreement, the two corporations merged their previously separate projects to produce twin-engined general purpose helicopters, these being the Bo 107 by MBB and the KH-7 from Kawasaki.[4] All of the privately incurred development costs were shared equally between the two partners; in November 1977, the programme received a huge boost when the government of West Germany announced that it would fund half of the costs of development.[5] By April 1978, project definition studies had been completed, enabling the joint venture to proceed with the detail design phase of development.[5]

Separate elements of the design were assigned to each company; MBB were responsible for developing the rotors (these were based on the rigid rotor system previously used on MBB's Bo 105), tailboom, flight controls and hydraulic system while Kawasaki undertook the development of the landing gear, airframe, main transmission, electrical system and other minor components.[3] German vehicle manufacturer BMW acted as a consultant on the styling of the BK 117.[5] As per their agreement, each company established their own final assembly line for the type, on which they would produce the rotorcraft to meet demands within their respective local markets.[6][3]

Originally, each company intended to construct a pair of prototypes (in actuality, Kawasaki opted to only build a single prototype) which were to be completed by 1979; one for flight testing purposes and the others for tie down testing and static testing. On 13 June 1979, MBB's flying prototype conducted its maiden flight at Ottobrunn, Bavaria, Germany; months later, it was followed by the Kawasaki prototype at Gifu, Chūbu region, Japan on 10 August 1979.[6][5] The pace of development on the programme had been slower than expected, a problem that was exacerbated by a shortage of skilled manpower that was available at MBB. Although it was originally planned for the rotorcraft's airworthiness certification to be achieved before the end of 1980, German certification was not achieved until 9 December 1982, being quickly followed by the receipt of Japanese certification on 17 December 1982. On 29 March 1983, the type secured the all-important United States Federal Aviation Administration (FAA) certification, clearing it for widespread use.[7][5]

Further development

During 1983, the initial production version, designated as the BK 117A-1 was first delivered.[5] Improved variants were quickly developed; in early 1985, the BK 117A-3, featuring an increased maximum takeoff weight and an enlarged tail rotor with twisted airfoils, was certified; two years later, the BK 117A-4, equipped with LTS 101-750B-1 engines for improved hot/high performance and increased maximum takeoff weight, along with improvements to the main rotor transmission and tail rotor mast, as well as a larger capacity fuel tank, was introduced.[5] During 1990, MBB's American division launched a dedicated corporate version of the BK 117; it was furnished with a Honeywell-built SPZ-7000 digital automatic flight control system and a cocoon-type interior system; optional extras included a Bendix/King electronic flight instrumentation system (EFIS) and a clamshell cabin door. During 1992, the BK 117C-1, equipped with a revised EFIS panel and an improved environmental control system, along with greater hot-and-high performance, was introduced to service.[5]

At one stage, there was considerable attention paid to the concept of a dedicated militarised variant of the type.[5] During the 1985 Paris Air Show, the concept of an armed attack helicopter derivative, referred to as the BK 117A-3M, was revealed to the general public. As promoted, this variant would have been capable of being armed with launchers for eight Euromissile HOT 2 missiles and a chin-mounted Lucas-built turret for a Browning 12.7mm machine gun, aimed using a helmet-mounted sight.[5] It was also to be equipped with various advanced targeting sensors, including an SFIM APX-M 397 roof-mounted stabilized sight. In order to provide sufficient ground clearance for the gun turret, the use of higher skid landing gear would have also been necessitated.[5]

During the 1990s, as a result of the commercial success of the type, a refined derivative, initially marketed as the BK 117 C-2 prior to its rebranding as the EC 145 and later as the H145, was developed from the BK 117 C-1 version; this improved version of the rotorcraft has succeeded and eventually replaced the original BK 117 in production. In total, 443 BK 117s were manufactured by the two partners; 329 (and two prototypes) were produced by MBB at their Donauworth facility while 111 (and one prototype) were completed by Kawasaki in Japan. during the 1980s, an agreement was formed with Indonesian Aerospace, enabling the type to be produced under license in Indonesia, which was accordingly designated as the NBK 117; however, according to economics author Sören Eriksson, the Indonesian production programme was terminated after only a handful of rotorcraft were completed.[8][5]

Since exiting production, third parties have produced their own upgrade programmes for existing BK 117s. In 2010, Airwork launched its conversion programme for the type, replacing the original LTS101-750B-1 engine with the newer LTS101-850B-2 engine, increasing both its performance, reliability and safety margins, resulting in the BK117-850D2; by 2016, Airwork had upgraded nearly 50 rotorcraft in this manner.[9]

Design

The MBB/Kawasaki BK 117 is a twin-engined medium utilitytransport helicopter. It possessed several attributes that lend itself to performing many different roles, such as twin-engine redundancy, sizable clamshell-shaped rear-facing double doors, and a relatively spacious cabin; one mission to which it was deemed to be particularly suitable was the emergency medical services (EMS).[10] The airframe is composed of rivetted metal, making minimal use of composite materials, and machined to a high standard; in order to free up internal space, both the engines and transmission are positioned above the main cabin. Considerable efforts were made to reduce the weight of the aircraft where possible albeit without compromising the aircraft's structural integrity.[3] The cabin could be outfitted with various interiors in order to suit its purpose, or to incorporate greater comfort levels, which included measures to dampen both noise and vibration.[11]

Early versions of the BK 117 were powered by a pair of Lycoming LTS101 turboshaft engines, rated to generate 550 shp at takeoff with considerable reserve power to guard against a single engine failure.[3] While each engine possesses sufficient power to maintain flight and even takeoff in the event of a single engine being rendered inoperable, the type also has favourable autorotation capabilities. In order to extend their operational lifespan and increase their reliability, MBB tuned the engines to operate at lower-than-standard revolutions per minute (RPM).[11] The engines are regulated using a specialised control system which smoothly and evenly regulate RPM and torque between both engines, even during vigorous manoeuvers.[3] Power management has been greatly eased via the addition of an automatic engine-governor system, allowing pilots to simply monitor the torque and engine temperature gauges. The aircraft can be suitably equipped for flight under instrument flight rules (IFR) as well as for single-pilot operations.[3]

According to aviation publication Flying, as a consequence of its uncommon rigid main rotor system, the BK 117 possessed relatively high stability and manoeuvrability which, amongst other capabilities, reportedly gave the type the ability to perform a steeper approach than any other helicopter in its class.[3] The four-bladed main rotor was smaller and slower-turning than many of its contemporaries, reducing both vibration and noise while also enabling the type to use more compact landing sites. The high-mounted tail boom and tail rotor of the BK 117 also presented several benefits, such as enhanced safety to personnel on the ground.[12] In terms of its flight performance, the type was considered to be suitable for the execution of various aerobatic manoeuvres, such as flying loops and rolls, while retaining such levels of inherent stability that pilots could readily release both the cyclic and collective controls, unlike the majority of rotorcraft.[11] The controls of the BK 117 are heavy and distinctly "un-twitchy".[citation needed] An optional Sperry-built three-axis stability augmentation system also served to improve the rotorcraft's ease of handling.[11]

Operational history

A single BK 117 A-3 (c/n 7106) was leased by the Canadian Forces Air Command for a test program and designated as the CH-143. When the program was over, the aircraft was returned to MBB Canada.[13]

A BK117 helicopter contracted by the New South Wales Rural Fire Service to fight fires crashed on 17 August 2018, the pilot died in the crash.[14]

Variants

 
BK 117 P-2 (D-HBKA)
German prototype, first flown 13 June 1979. Now exhibited at the Bückeburg helicopter museum, Bückeburg, Germany.
BK 117 S-01 (D-HDRF)
Initial pre-production prototype. Now preserved on top of the DRF-Headquarters at Stuttgart Airport.
BK 117 P-3/P-5 (JQ0003)
Japanese prototype, first flown 10 August 1979. Now exhibited at Kakamigahara Aerospace Museum, Kakamigahara/Gifu, Japan
BK 117 A-1
Powered by two Lycoming LTS 101-650B-1 engines. First flown 23 April 1982.
BK 117 A-3
Introduced in March 1985, the A-3 has a larger tail rotor with improved blades, Yaw CSAS, improved stability (SPAS) and the take-off weight increased to 3,200 kg (7,055 lb).- The Canadian Armed forces leased a single BK 117-A3 for a test program and designated it the CH-143. When the program was over, the aircraft was returned to MBB Canada[15]
BK 117 A-4
Introduced in July 1986, the A-4 has increased transmission limits at take-off power, improved tail rotor head. German aircraft have provision for extra internal fuel, giving enhanced performance.
BK 117 A-3M
Military version introduced in 1986. The A-3M is fitted with taller skids and can carry 11 troops. A Browning 12.7 mm (0.5 in) machine gun can be mounted under the fuselage in a Lucas turret with 450 rounds and controlled by a helmet-mounted sight. The A-3M also has outrigger pylons which can hold up to eight HOT II or TOW antitank missiles or a variety of air-to-air missiles, rocket-pods, or forward-firing cannons. Provisions for a doorway gunner's position with a 12.7 mm (0.5 in) gun can also be installed.
BK 117 B-1
Introduced in December 1987, the B-1 is fitted with LTS 101-750B-1 engines to provide increased performance, and a 140 kg (309 lb) increase in payload.
BK 117 B-1C
UK-certified version with reduced range and endurance.
BK 117 B-2
Maximum Gross Weight increased to 3,350 kg, 2 x Allied Signal Lycoming LTS101-750B-1 engines fitted as standard, new tail rotor blades, improved "hot and high" performance, take-off/landing limitation increased to 15,000 ft, improved flight performance for: HIGE/HOGE, single engine service ceiling.
BK 117 C-1
Powered by two Turbomeca Arriel 1E engines. Later models may be upgraded to Arriel 1E2 engines.
NBK 117
License-built model produced in Indonesia by Indonesian Aerospace.[16]
BK 117-850D2
Introduced in 2010, the 850D2 variant is an STC (Supplementary Type Certificate) development (i.e., re-engined) of BK 117 B-2 incorporating Honeywell LTS 101-850B-2 engines aimed at improving OEI and Category A performance.[17] Development and certification was conducted in New Zealand by Airwork of Ardmore, NZ, in conjunction with Flight Structures Ltd.[18]

NOTE: All later variants are derived from the BK 117 by Eurocopter Deutschland and later Airbus Helicopters.
The variants BK 117-C2, -D2 and -D3 are therefore better known under its commercial naming convention EC145 and H145 and don't share the same EASA Type Certificate (see EASA Helicopter Type Rating List).[19]

Operators

Military and government

  Australia
 
A Polizei BK 117
  Chile
  Colombia
  Germany
 
SX-HFH. a BK-117 of the Hellenic Fire Service
  Greece
  Japan
  Madagascar
  Peru
  Russia
 
Saitama Prefectural Police BK 117
  Spain
  South Africa
  United States

Civil

 
A PolAir 5' BK 117 in flight

The majority of the helicopters are operated by various emergency services although it is also operated by private individuals, companies and executive charter operators.

  Australia
  Canada
  Germany
  Kenya
  • Everett Aviation[41]
  New Zealand
 
BK 117 in service with Auckland Rescue Helicopter Trust
  Switzerland
  Taiwan
  • Daily Air Corporation[46]
  Thailand
  • Si Chang Flying Services[47]
  United States

Former

  Bophuthatswana
  Canada
  Ciskei
 
BK 117 in service with the South African Air Force
  Transkei
  Venda

Specifications (BK 117 B-2)

Data from Jane's All The World's Aircraft 1993–94[55]

General characteristics

  • Crew: 1
  • Capacity: up to 10 passengers
  • Length: 9.91 m (32 ft 6 in) (fuselage length)
  • Height: 3.85 m (12 ft 8 in) (rotors turning)
  • Empty weight: 1,727 kg (3,807 lb)
  • Max takeoff weight: 3,350 kg (7,385 lb)
  • Fuel capacity: 697 L (183 US Gallons, 153 Imp Gallons) internal fuel
  • Powerplant: 2 × Textron Lycoming LTS 101-750B-1 turboshaft, 442 kW (593 hp) each
  • Main rotor diameter: 11.00 m (36 ft 1 in)
  • Main rotor area: 95.03 m2 (1,022.9 sq ft)

Performance

  • Maximum speed: 250 km/h (160 mph, 130 kn) at sea level
  • Never exceed speed: 278 km/h (173 mph, 150 kn)
  • Range: 541 km (336 mi, 292 nmi)
  • Service ceiling: 4,575 m (15,010 ft) (max certified altitude)
  • Hover Ceiling: 3,565 m (11,700 ft) (in ground effect)
  • Rate of climb: 11.00 m/s (2,165 ft/min)

See also

Related development

References

Citations

  1. ^ McCellan 1986, p. 64.
  2. ^ McCellan 1986, pp. 64, 66.
  3. ^ a b c d e f g h McCellan 1986, p. 66.
  4. ^ Air International April 1989, p. 163.
  5. ^ a b c d e f g h i j k l "The Market for Light Military Rotorcraft." 21 August 2012 at the Wayback Machine Forecast International, November 2010.
  6. ^ a b Air International April 1989, p. 164.
  7. ^ Air International April 1989, pp. 164–165.
  8. ^ Eriksson 2013, p. 153.
  9. ^ Williams, Daniel. "50 And Counting For The BK117-850D2." 17 November 2017 at the Wayback Machine Aviation Week, 12 September 2016.
  10. ^ McCellan 1986, p. 62, 64.
  11. ^ a b c d McCellan 1986, pp. 66–67.
  12. ^ McCellan 1986, p. 67.
  13. ^ "MBB CH-143 BK 117". Royal Canadian Air Force. Archived from the original on 10 September 2005. Retrieved 25 March 2007.
  14. ^ Khalil, Shireen (17 August 2018). "nsw act Pilot of Rural Fire Service helicopter dies after crash". news.com.au. from the original on 17 August 2018. Retrieved 17 August 2018.
  15. ^ a b . canadianwings.com. Archived from the original on 22 September 2013. Retrieved 2 February 2013.
  16. ^ The Emerging Technological Trajectory of the Pacific Rim by Denis Fred Simon, page 193.
  17. ^ "Honeywell Announces LTS101-850B-2 Engine Upgrade for Eurocopter BK117." 12 July 2011 at the Wayback Machine Honeywell, 22 February 2009.
  18. ^ "Airwork (NZ)’s BK117-850D2 takes to the skies over Australia and New Zealand." 7 February 2013 at the Wayback Machine Flight Structures Ltd, 1 May 2010.
  19. ^ (PDF). Archived from the original (PDF) on 19 April 2021. Retrieved 19 April 2021.{{cite web}}: CS1 maint: archived copy as title (link)
  20. ^ a b . fire.nsw.gov.au. Archived from the original on 25 April 2013. Retrieved 5 February 2013.
  21. ^ . stepforward.wa.gov.au. Archived from the original on 9 February 2013. Retrieved 2 February 2013.
  22. ^ a b c "World Air Forces 2013" (PDF). Flightglobal Insight. 2013. (PDF) from the original on 2 November 2013. Retrieved 2 February 2013.
  23. ^ "(MBB BK 117) Carabineros de Chile". from the original on 16 June 2013. Retrieved 2 February 2013.
  24. ^ "Kawasaki BK-117B-1". Demand media. from the original on 22 September 2013. Retrieved 2 February 2013.
  25. ^ "H145M LUH SOF". www.luftwaffe.de (in German). from the original on 29 December 2017. Retrieved 29 December 2017.
  26. ^ . © Ebner Verlag GmbH & Co. KG. Archived from the original on 16 October 2017. Retrieved 2 February 2013.
  27. ^ Scharenborg 2022, p. 70
  28. ^ Saitama Prefectural Police (ed.). "航空隊の紹介". from the original on 6 November 2018. Retrieved 6 November 2018.
  29. ^ Martin, Guy (September 2019). "Madagascar's military receives more aircraft". Air International. Vol. 97, no. 3. p. 9. ISSN 0306-5634.
  30. ^ . cavok-aviation. Archived from the original on 21 September 2013. Retrieved 2 February 2013.
  31. ^ Mlandenov Air International December 2016, pp. 85–86.
  32. ^ . aeroflight.co.uk. Archived from the original on 7 January 2013. Retrieved 2 February 2013.
  33. ^ . Eurocopter. Archived from the original on 22 September 2013. Retrieved 2 February 2013.
  34. ^ "County of Riverside Sheriff Aircraft Registration". FlightAware. Retrieved 26 November 2021.{{cite web}}: CS1 maint: url-status (link)
  35. ^ "Careflight: Our Helicopters". careflight.org. from the original on 30 June 2015. Retrieved 29 June 2015.
  36. ^ . lifesaver.org.au. Archived from the original on 14 January 2013. Retrieved 2 February 2013.
  37. ^ . stars.ca. Archived from the original on 29 October 2013. Retrieved 2 February 2013.
  38. ^ . eurocopter.com. Archived from the original on 16 November 2012. Retrieved 2 February 2013.
  39. ^ "BK-117C". Demand media. from the original on 21 September 2013. Retrieved 2 February 2013.
  40. ^ "DRF Luftrettung BK 117". from the original on 16 June 2013. Retrieved 2 February 2013.
  41. ^ "Everatt's BK 117 C1". everettaviation.com. from the original on 10 March 2013. Retrieved 2 February 2013.
  42. ^ "Auckland Rescue Helicopter Trust (fleet)". rescuehelicopter.org.nz. from the original on 25 March 2015. Retrieved 7 March 2015.
  43. ^ "Westpac Rescue Helicopter". lifeflight.org.nz. from the original on 12 April 2018. Retrieved 11 April 2018.
  44. ^ "Learn more about our Canterbury Westpac Rescue Helicopter". airrescue.co.nz. from the original on 23 June 2020. Retrieved 23 June 2020.
  45. ^ . otagorescue.co.nz. Archived from the original on 30 June 2013. Retrieved 2 July 2013.
  46. ^ (PDF). dailyair.com.tw. Archived from the original (PDF) on 19 November 2012. Retrieved 2 February 2013.
  47. ^ "MBB-Kawasaki BK-117B-1 - Si Chang Flying Service - SFS".
  48. ^ "airmethods fleet". airmethods.com. from the original on 12 February 2013. Retrieved 2 February 2013.
  49. ^ "KidsFlight 1". stlouischildrens.org. from the original on 21 September 2013. Retrieved 2 February 2013.
  50. ^ . Orlando Health. Archived from the original on 6 October 2013. Retrieved 12 June 2015.
  51. ^ "World Air Forces 1991 pg. 37". flightglobal.com. from the original on 2 April 2015. Retrieved 6 March 2015.
  52. ^ "World Air Forces 1991 pg. 41". flightglobal.com. from the original on 2 April 2015. Retrieved 6 March 2015.
  53. ^ "World Air Forces 1991 pg. 65". flightglobal.com. from the original on 2 April 2015. Retrieved 6 March 2015.
  54. ^ "World Air Forces 1991 pg. 71". flightglobal.com. from the original on 2 December 2016. Retrieved 6 March 2015.
  55. ^ Lambert 1993, pp. 159–160.

Bibliography

  • "BK 117...a Terrestrial Space Ship". Air International, Vol 36 No 4, April 1989. Bromley, UK:Fine Scroll. ISSN 0306-5634. pp. 163–170.
  • Eriksson, Sören. "Clusters and Economic Growth in Asia." Edward Elgar Publishing, 2013. ISBN 0-85793-009-5.
  • Hatch, Paul. "World's Air Forces". Flight International, 5–11 December 1990. pp. 35–81.
  • Hoyle, Craig. "World Air Forces Directory". Flight International, Vol. 182, No. 5370, 11–17 December 2012. pp. 40–64. ISSN 0015-3710.
  • Lambert, Mark. Jane's All The World's Aircraft 1993–94. Coulsdon, UK:Jane's Data Division, 1993. ISBN 0-7106-1066-1.
  • McCellan, J. Mac. "Paramedic." Flying, February 1986. Vol. 113, No. 2. pp. 62–67. ISSN 0015-4806.
  • Mlandenov, Alexander. "Russia's Responders". Air International, Vol. 91, No. 6, December 2016. pp. 78–87. ISSN 0306-5634.
  • Prétat, Samuel. "EC 145 & UH-72." Éditions Minimonde76, 2015. ISBN 9-782954-18181-3. (in French)
  • Scharenborg, Martin. "Fighting the fires". Air International, Vol. 103 No. 2, September 2022. pp. 68–72. ISSN 0306-5634.

External links

  • BK 117 in aeromedical services

kawasaki, twin, engined, light, utility, transport, helicopter, jointly, developed, manufactured, messerschmitt, bölkow, blohm, germany, kawasaki, japan, later, purchased, daimler, benz, eventually, became, part, eurocopter, which, later, rebranded, airbus, he. The MBB Kawasaki BK 117 is a twin engined light utility transport helicopter It was jointly developed and manufactured by Messerschmitt Bolkow Blohm MBB of Germany and Kawasaki of Japan MBB was later purchased by Daimler Benz and eventually became a part of Eurocopter which was later rebranded as Airbus Helicopters BK 117A BK 117 of the German policeRole Utility transportNational origin Germany JapanManufacturer Messerschmitt Bolkow Blohm MBB Kawasaki Heavy IndustriesFirst flight 13 June 1979Introduction 9 December 1982Status in production in active servicePrimary users DRFADACProduced 1979 presentDeveloped into Eurocopter EC145On 25 February 1977 MBB and Kawasaki signed a cooperative agreement to abandon their independent efforts to design twin engined general purpose helicopters in favour of a collaborative venture to development of a new rotorcraft for that role While the programme s costs were shared equally the workshare was divided into certain areas of the design MBB utilised their expertise with the rigid rotor system used on the earlier Bo 105 to develop the majority of the dynamic systems and flight controls while Kawasaki focused on the airframe structural elements and various other components On 13 June 1979 MBB s flying prototype conducted its maiden flight at Ottobrunn Bavaria Germany months later it was followed by the Kawasaki prototype at Gifu Chubu region Japan on 10 August 1979 Each company established their own final assembly line producing the BK 117 for their respective regions The BK 117 has proven to be popular for passenger services and VIP transport the cabin can be outfitted with various seating configurations seating between seven and ten passengers It is also used for a diverse range of operations such as aerial crane and sling work law enforcement and military transport and is exceptional as an air ambulance and search and rescue platform During the 1990s due to its popularity a refined derivative initially marketed as the BK 117 C 2 before being rebranded as the EC 145 and later as the H145 was developed from the BK 117 C 1 version this improved version of the rotorcraft has since succeeded the original BK 117 in production Contents 1 Development 1 1 Origins 1 2 Further development 2 Design 3 Operational history 4 Variants 5 Operators 5 1 Military and government 5 2 Civil 5 3 Former 6 Specifications BK 117 B 2 7 See also 8 References 8 1 Citations 8 2 Bibliography 9 External linksDevelopment EditOrigins Edit According to aviation author J Mac McCellan the BK 117 has its origins in an earlier rotorcraft designed and produced by German aerospace manufacturer Messerschmitt Bolkow Blohm MBB the MBB Bo 105 1 This helicopter which proved to be a commercial success had made use of a revolutionary hingeless main rotor composed of fibreglass which was developed by German engineer Ludwig Bolkow Having established a reputation for reliability and safety during the early 1970s MBB along with one of its major shareholders Boeing Vertol began studying options for producing an enlarged derivative of the type to accompany the Bo 105 2 However Boeing soon withdrew from the venture leading to MBB searching for another partner this was found in the form of Japanese company Kawasaki Heavy Industries 3 On 25 February 1977 MBB and Kawasaki signed an agreement to cooperate on the development of a new rotorcraft Under the terms of this agreement the two corporations merged their previously separate projects to produce twin engined general purpose helicopters these being the Bo 107 by MBB and the KH 7 from Kawasaki 4 All of the privately incurred development costs were shared equally between the two partners in November 1977 the programme received a huge boost when the government of West Germany announced that it would fund half of the costs of development 5 By April 1978 project definition studies had been completed enabling the joint venture to proceed with the detail design phase of development 5 Separate elements of the design were assigned to each company MBB were responsible for developing the rotors these were based on the rigid rotor system previously used on MBB s Bo 105 tailboom flight controls and hydraulic system while Kawasaki undertook the development of the landing gear airframe main transmission electrical system and other minor components 3 German vehicle manufacturer BMW acted as a consultant on the styling of the BK 117 5 As per their agreement each company established their own final assembly line for the type on which they would produce the rotorcraft to meet demands within their respective local markets 6 3 Originally each company intended to construct a pair of prototypes in actuality Kawasaki opted to only build a single prototype which were to be completed by 1979 one for flight testing purposes and the others for tie down testing and static testing On 13 June 1979 MBB s flying prototype conducted its maiden flight at Ottobrunn Bavaria Germany months later it was followed by the Kawasaki prototype at Gifu Chubu region Japan on 10 August 1979 6 5 The pace of development on the programme had been slower than expected a problem that was exacerbated by a shortage of skilled manpower that was available at MBB Although it was originally planned for the rotorcraft s airworthiness certification to be achieved before the end of 1980 German certification was not achieved until 9 December 1982 being quickly followed by the receipt of Japanese certification on 17 December 1982 On 29 March 1983 the type secured the all important United States Federal Aviation Administration FAA certification clearing it for widespread use 7 5 Further development Edit During 1983 the initial production version designated as the BK 117A 1 was first delivered 5 Improved variants were quickly developed in early 1985 the BK 117A 3 featuring an increased maximum takeoff weight and an enlarged tail rotor with twisted airfoils was certified two years later the BK 117A 4 equipped with LTS 101 750B 1 engines for improved hot high performance and increased maximum takeoff weight along with improvements to the main rotor transmission and tail rotor mast as well as a larger capacity fuel tank was introduced 5 During 1990 MBB s American division launched a dedicated corporate version of the BK 117 it was furnished with a Honeywell built SPZ 7000 digital automatic flight control system and a cocoon type interior system optional extras included a Bendix King electronic flight instrumentation system EFIS and a clamshell cabin door During 1992 the BK 117C 1 equipped with a revised EFIS panel and an improved environmental control system along with greater hot and high performance was introduced to service 5 At one stage there was considerable attention paid to the concept of a dedicated militarised variant of the type 5 During the 1985 Paris Air Show the concept of an armed attack helicopter derivative referred to as the BK 117A 3M was revealed to the general public As promoted this variant would have been capable of being armed with launchers for eight Euromissile HOT 2 missiles and a chin mounted Lucas built turret for a Browning 12 7mm machine gun aimed using a helmet mounted sight 5 It was also to be equipped with various advanced targeting sensors including an SFIM APX M 397 roof mounted stabilized sight In order to provide sufficient ground clearance for the gun turret the use of higher skid landing gear would have also been necessitated 5 During the 1990s as a result of the commercial success of the type a refined derivative initially marketed as the BK 117 C 2 prior to its rebranding as the EC 145 and later as the H145 was developed from the BK 117 C 1 version this improved version of the rotorcraft has succeeded and eventually replaced the original BK 117 in production In total 443 BK 117s were manufactured by the two partners 329 and two prototypes were produced by MBB at their Donauworth facility while 111 and one prototype were completed by Kawasaki in Japan during the 1980s an agreement was formed with Indonesian Aerospace enabling the type to be produced under license in Indonesia which was accordingly designated as the NBK 117 however according to economics author Soren Eriksson the Indonesian production programme was terminated after only a handful of rotorcraft were completed 8 5 Since exiting production third parties have produced their own upgrade programmes for existing BK 117s In 2010 Airwork launched its conversion programme for the type replacing the original LTS101 750B 1 engine with the newer LTS101 850B 2 engine increasing both its performance reliability and safety margins resulting in the BK117 850D2 by 2016 Airwork had upgraded nearly 50 rotorcraft in this manner 9 Design EditThe MBB Kawasaki BK 117 is a twin engined medium utility transport helicopter It possessed several attributes that lend itself to performing many different roles such as twin engine redundancy sizable clamshell shaped rear facing double doors and a relatively spacious cabin one mission to which it was deemed to be particularly suitable was the emergency medical services EMS 10 The airframe is composed of rivetted metal making minimal use of composite materials and machined to a high standard in order to free up internal space both the engines and transmission are positioned above the main cabin Considerable efforts were made to reduce the weight of the aircraft where possible albeit without compromising the aircraft s structural integrity 3 The cabin could be outfitted with various interiors in order to suit its purpose or to incorporate greater comfort levels which included measures to dampen both noise and vibration 11 Early versions of the BK 117 were powered by a pair of Lycoming LTS101 turboshaft engines rated to generate 550 shp at takeoff with considerable reserve power to guard against a single engine failure 3 While each engine possesses sufficient power to maintain flight and even takeoff in the event of a single engine being rendered inoperable the type also has favourable autorotation capabilities In order to extend their operational lifespan and increase their reliability MBB tuned the engines to operate at lower than standard revolutions per minute RPM 11 The engines are regulated using a specialised control system which smoothly and evenly regulate RPM and torque between both engines even during vigorous manoeuvers 3 Power management has been greatly eased via the addition of an automatic engine governor system allowing pilots to simply monitor the torque and engine temperature gauges The aircraft can be suitably equipped for flight under instrument flight rules IFR as well as for single pilot operations 3 According to aviation publication Flying as a consequence of its uncommon rigid main rotor system the BK 117 possessed relatively high stability and manoeuvrability which amongst other capabilities reportedly gave the type the ability to perform a steeper approach than any other helicopter in its class 3 The four bladed main rotor was smaller and slower turning than many of its contemporaries reducing both vibration and noise while also enabling the type to use more compact landing sites The high mounted tail boom and tail rotor of the BK 117 also presented several benefits such as enhanced safety to personnel on the ground 12 In terms of its flight performance the type was considered to be suitable for the execution of various aerobatic manoeuvres such as flying loops and rolls while retaining such levels of inherent stability that pilots could readily release both the cyclic and collective controls unlike the majority of rotorcraft 11 The controls of the BK 117 are heavy and distinctly un twitchy citation needed An optional Sperry built three axis stability augmentation system also served to improve the rotorcraft s ease of handling 11 Operational history EditThis section needs expansion You can help by adding to it November 2017 A single BK 117 A 3 c n 7106 was leased by the Canadian Forces Air Command for a test program and designated as the CH 143 When the program was over the aircraft was returned to MBB Canada 13 A BK117 helicopter contracted by the New South Wales Rural Fire Service to fight fires crashed on 17 August 2018 the pilot died in the crash 14 Variants Edit STARS Air Ambulance at Foothills Medical Centre BK 117 P 2 D HBKA German prototype first flown 13 June 1979 Now exhibited at the Buckeburg helicopter museum Buckeburg Germany BK 117 S 01 D HDRF Initial pre production prototype Now preserved on top of the DRF Headquarters at Stuttgart Airport BK 117 P 3 P 5 JQ0003 Japanese prototype first flown 10 August 1979 Now exhibited at Kakamigahara Aerospace Museum Kakamigahara Gifu Japan BK 117 A 1 Powered by two Lycoming LTS 101 650B 1 engines First flown 23 April 1982 BK 117 A 3 Introduced in March 1985 the A 3 has a larger tail rotor with improved blades Yaw CSAS improved stability SPAS and the take off weight increased to 3 200 kg 7 055 lb The Canadian Armed forces leased a single BK 117 A3 for a test program and designated it the CH 143 When the program was over the aircraft was returned to MBB Canada 15 BK 117 A 4 Introduced in July 1986 the A 4 has increased transmission limits at take off power improved tail rotor head German aircraft have provision for extra internal fuel giving enhanced performance BK 117 A 3M Military version introduced in 1986 The A 3M is fitted with taller skids and can carry 11 troops A Browning 12 7 mm 0 5 in machine gun can be mounted under the fuselage in a Lucas turret with 450 rounds and controlled by a helmet mounted sight The A 3M also has outrigger pylons which can hold up to eight HOT II or TOW antitank missiles or a variety of air to air missiles rocket pods or forward firing cannons Provisions for a doorway gunner s position with a 12 7 mm 0 5 in gun can also be installed BK 117 B 1 Introduced in December 1987 the B 1 is fitted with LTS 101 750B 1 engines to provide increased performance and a 140 kg 309 lb increase in payload BK 117 B 1C UK certified version with reduced range and endurance BK 117 B 2 Maximum Gross Weight increased to 3 350 kg 2 x Allied Signal Lycoming LTS101 750B 1 engines fitted as standard new tail rotor blades improved hot and high performance take off landing limitation increased to 15 000 ft improved flight performance for HIGE HOGE single engine service ceiling BK 117 C 1 Powered by two Turbomeca Arriel 1E engines Later models may be upgraded to Arriel 1E2 engines NBK 117 License built model produced in Indonesia by Indonesian Aerospace 16 BK 117 850D2 Introduced in 2010 the 850D2 variant is an STC Supplementary Type Certificate development i e re engined of BK 117 B 2 incorporating Honeywell LTS 101 850B 2 engines aimed at improving OEI and Category A performance 17 Development and certification was conducted in New Zealand by Airwork of Ardmore NZ in conjunction with Flight Structures Ltd 18 NOTE All later variants are derived from the BK 117 by Eurocopter Deutschland and later Airbus Helicopters The variants BK 117 C2 D2 and D3 are therefore better known under its commercial naming convention EC145 and H145 and don t share the same EASA Type Certificate see EASA Helicopter Type Rating List 19 Operators EditMilitary and government Edit AustraliaFire and Rescue NSW 20 formerly New South Wales Rural Fire Service A Polizei BK 117 New South Wales Police Force 20 Western Australia Police 21 ChileChilean Air Force 22 Carabineros de Chile 23 24 ColombiaColombian National Armada 22 GermanyBundeswehr 25 failed verification Polizei 26 SX HFH a BK 117 of the Hellenic Fire Service GreeceHellenic Fire Service Operates three BK 117C1s 27 JapanPrefectural police departments 28 MadagascarMalagasy Air Force 29 PeruPeruvian National Police 30 Russia Saitama Prefectural Police BK 117 Ministry of Emergency Situations 31 SpainGuardia Civil 32 South AfricaSouth African Air Force 22 South African Police Service 33 United StatesRiverside County Sheriff s Department California 34 Civil Edit A PolAir 5 BK 117 in flight The majority of the helicopters are operated by various emergency services although it is also operated by private individuals companies and executive charter operators AustraliaCareFlight 35 Westpac Life Saver Rescue Service 36 CanadaShock Trauma Air Rescue Society 37 GermanyADAC 38 39 DRF Luftrettung 40 KenyaEverett Aviation 41 New Zealand BK 117 in service with Auckland Rescue Helicopter Trust Auckland Rescue Helicopter Trust 42 Life Flight New Zealand 43 Canterbury West Coast Air Rescue Trust 44 Otago Rescue Helicopter Trust 45 SwitzerlandRega air rescue 7 H145 since 2018 replacing the EC145 TaiwanDaily Air Corporation 46 ThailandSi Chang Flying Services 47 United StatesAir Methods 48 St Louis Children s Hospital 49 Orlando Regional Medical Center 50 Former Edit BophuthatswanaBophuthatswana Air Force 51 CanadaCanadian Forces Air Command 15 Ciskei BK 117 in service with the South African Air Force Ciskei Defence Force 52 TranskeiTranskei Defence Force 53 VendaVenda Defence Force 54 Specifications BK 117 B 2 EditData from Jane s All The World s Aircraft 1993 94 55 General characteristicsCrew 1 Capacity up to 10 passengers Length 9 91 m 32 ft 6 in fuselage length Height 3 85 m 12 ft 8 in rotors turning Empty weight 1 727 kg 3 807 lb Max takeoff weight 3 350 kg 7 385 lb Fuel capacity 697 L 183 US Gallons 153 Imp Gallons internal fuel Powerplant 2 Textron Lycoming LTS 101 750B 1 turboshaft 442 kW 593 hp each Main rotor diameter 11 00 m 36 ft 1 in Main rotor area 95 03 m2 1 022 9 sq ft Performance Maximum speed 250 km h 160 mph 130 kn at sea level Never exceed speed 278 km h 173 mph 150 kn Range 541 km 336 mi 292 nmi Service ceiling 4 575 m 15 010 ft max certified altitude Hover Ceiling 3 565 m 11 700 ft in ground effect Rate of climb 11 00 m s 2 165 ft min See also Edit Aviation portalHelicopter Air ambulanceRelated development MBB Bo 105 Eurocopter EC135 Eurocopter EC145References EditCitations Edit McCellan 1986 p 64 McCellan 1986 pp 64 66 a b c d e f g h McCellan 1986 p 66 Air International April 1989 p 163 a b c d e f g h i j k l The Market for Light Military Rotorcraft Archived 21 August 2012 at the Wayback Machine Forecast International November 2010 a b Air International April 1989 p 164 Air International April 1989 pp 164 165 Eriksson 2013 p 153 Williams Daniel 50 And Counting For The BK117 850D2 Archived 17 November 2017 at the Wayback Machine Aviation Week 12 September 2016 McCellan 1986 p 62 64 a b c d McCellan 1986 pp 66 67 McCellan 1986 p 67 MBB CH 143 BK 117 Royal Canadian Air Force Archived from the original on 10 September 2005 Retrieved 25 March 2007 Khalil Shireen 17 August 2018 nsw act Pilot of Rural Fire Service helicopter dies after crash news com au Archived from the original on 17 August 2018 Retrieved 17 August 2018 a b BK 117 CH 143 canadianwings com Archived from the original on 22 September 2013 Retrieved 2 February 2013 The Emerging Technological Trajectory of the Pacific Rim by Denis Fred Simon page 193 Honeywell Announces LTS101 850B 2 Engine Upgrade for Eurocopter BK117 Archived 12 July 2011 at the Wayback Machine Honeywell 22 February 2009 Airwork NZ s BK117 850D2 takes to the skies over Australia and New Zealand Archived 7 February 2013 at the Wayback Machine Flight Structures Ltd 1 May 2010 Archived copy PDF Archived from the original PDF on 19 April 2021 Retrieved 19 April 2021 a href Template Cite web html title Template Cite web cite web a CS1 maint archived copy as title link a b FireAir 1 fire nsw gov au Archived from the original on 25 April 2013 Retrieved 5 February 2013 WA Police Air Wing stepforward wa gov au Archived from the original on 9 February 2013 Retrieved 2 February 2013 a b c World Air Forces 2013 PDF Flightglobal Insight 2013 Archived PDF from the original on 2 November 2013 Retrieved 2 February 2013 MBB BK 117 Carabineros de Chile Archived from the original on 16 June 2013 Retrieved 2 February 2013 Kawasaki BK 117B 1 Demand media Archived from the original on 22 September 2013 Retrieved 2 February 2013 H145M LUH SOF www luftwaffe de in German Archived from the original on 29 December 2017 Retrieved 29 December 2017 Einsatzfahrzeug D HNWQ c n 7554 c Ebner Verlag GmbH amp Co KG Archived from the original on 16 October 2017 Retrieved 2 February 2013 Scharenborg 2022 p 70 Saitama Prefectural Police ed 航空隊の紹介 Archived from the original on 6 November 2018 Retrieved 6 November 2018 Martin Guy September 2019 Madagascar s military receives more aircraft Air International Vol 97 no 3 p 9 ISSN 0306 5634 Base Aerea Lima Callao Policia Nacional del Peru cavok aviation Archived from the original on 21 September 2013 Retrieved 2 February 2013 Mlandenov Air International December 2016 pp 85 86 Spanish Guardia Civil aeroflight co uk Archived from the original on 7 January 2013 Retrieved 2 February 2013 South African Police Service signs for its 7th Eurocopter AS 350 B3 at AAD 2004 Eurocopter Archived from the original on 22 September 2013 Retrieved 2 February 2013 County of Riverside Sheriff Aircraft Registration FlightAware Retrieved 26 November 2021 a href Template Cite web html title Template Cite web cite web a CS1 maint url status link Careflight Our Helicopters careflight org Archived from the original on 30 June 2015 Retrieved 29 June 2015 lifesaver Fleet lifesaver org au Archived from the original on 14 January 2013 Retrieved 2 February 2013 STARS fleet stars ca Archived from the original on 29 October 2013 Retrieved 2 February 2013 ADAC Air Rescue confirms the choice of Eurocopter to renew its helicopter fleet with the EC145 T2 and EC135 eurocopter com Archived from the original on 16 November 2012 Retrieved 2 February 2013 BK 117C Demand media Archived from the original on 21 September 2013 Retrieved 2 February 2013 DRF Luftrettung BK 117 Archived from the original on 16 June 2013 Retrieved 2 February 2013 Everatt s BK 117 C1 everettaviation com Archived from the original on 10 March 2013 Retrieved 2 February 2013 Auckland Rescue Helicopter Trust fleet rescuehelicopter org nz Archived from the original on 25 March 2015 Retrieved 7 March 2015 Westpac Rescue Helicopter lifeflight org nz Archived from the original on 12 April 2018 Retrieved 11 April 2018 Learn more about our Canterbury Westpac Rescue Helicopter airrescue co nz Archived from the original on 23 June 2020 Retrieved 23 June 2020 Otago Rescue Helicopter Trust fleet otagorescue co nz Archived from the original on 30 June 2013 Retrieved 2 July 2013 Daily Air Operations PDF dailyair com tw Archived from the original PDF on 19 November 2012 Retrieved 2 February 2013 MBB Kawasaki BK 117B 1 Si Chang Flying Service SFS airmethods fleet airmethods com Archived from the original on 12 February 2013 Retrieved 2 February 2013 KidsFlight 1 stlouischildrens org Archived from the original on 21 September 2013 Retrieved 2 February 2013 ORMC Aircare 1 Orlando Health Archived from the original on 6 October 2013 Retrieved 12 June 2015 World Air Forces 1991 pg 37 flightglobal com Archived from the original on 2 April 2015 Retrieved 6 March 2015 World Air Forces 1991 pg 41 flightglobal com Archived from the original on 2 April 2015 Retrieved 6 March 2015 World Air Forces 1991 pg 65 flightglobal com Archived from the original on 2 April 2015 Retrieved 6 March 2015 World Air Forces 1991 pg 71 flightglobal com Archived from the original on 2 December 2016 Retrieved 6 March 2015 Lambert 1993 pp 159 160 Bibliography Edit BK 117 a Terrestrial Space Ship Air International Vol 36 No 4 April 1989 Bromley UK Fine Scroll ISSN 0306 5634 pp 163 170 Eriksson Soren Clusters and Economic Growth in Asia Edward Elgar Publishing 2013 ISBN 0 85793 009 5 Hatch Paul World s Air Forces Flight International 5 11 December 1990 pp 35 81 Hoyle Craig World Air Forces Directory Flight International Vol 182 No 5370 11 17 December 2012 pp 40 64 ISSN 0015 3710 Lambert Mark Jane s All The World s Aircraft 1993 94 Coulsdon UK Jane s Data Division 1993 ISBN 0 7106 1066 1 McCellan J Mac Paramedic Flying February 1986 Vol 113 No 2 pp 62 67 ISSN 0015 4806 Mlandenov Alexander Russia s Responders Air International Vol 91 No 6 December 2016 pp 78 87 ISSN 0306 5634 Pretat Samuel EC 145 amp UH 72 Editions Minimonde76 2015 ISBN 9 782954 18181 3 in French Scharenborg Martin Fighting the fires Air International Vol 103 No 2 September 2022 pp 68 72 ISSN 0306 5634 External links Edit Wikimedia Commons has media related to MBB Kawasaki BK 117 Manufacturer s website BK 117 in aeromedical services BK 117 factsheet Retrieved from https en wikipedia org w index php title MBB Kawasaki BK 117 amp oldid 1138855191, wikipedia, wiki, book, books, library,

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