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Brantly B-2

The Brantly B-2 is an American two-seat light helicopter produced by the Brantly Helicopter Corporation.

Brantly B-2
Brantly B2 in a hover
Role Light Helicopter
Manufacturer Brantly Helicopter Corporation
Designer Newby O. Brantly
First flight 21 February 1953
Introduction 1958
Status In production (2011)[1]
Number built 334

Design and development edit

After the failure of his first design, the Brantly B-1, Newby O. Brantly decided to design a simpler and less complicated helicopter for the private buyer.[citation needed] The B-2 had a single main rotor and an anti-torque tail rotor and first flew on 21 February 1953. This was followed by an improved second prototype that first flew on 14 August 1956.

The B-2A was introduced with a modified cabin, and the B-2B had a larger 180 hp fuel-injected engine. The B-2B has a three-bladed articulated main rotor and an all-metal fuselage, it can be operated with skid, wheel or float landing gear. The piston engine is fitted vertically in the fuselage behind the cabin.

Operational history edit

The basic design has remained in production for over 50 years.[1] The United States Army ordered five B-2s (designated the YHO-3) to be evaluated in the Light Observation Helicopter competition in 1958, although it lost the bid, the Army operated the H-5T unmanned variant as target from 1986.[2] Introduced in the early 1970s, an improved larger version with five seats was designated the Brantly 305.[3]

Variants edit

 
The unbuilt Brantly B2J10 10-seat transport helicopter. Was to be powered by two Allison 250-C18 or two Boeing 550-1-12C engines.
  • Brantly B-2: Two-seat single-engined light utility helicopter.
    • Brantly YHO-3: United States military designation for the B2.
  • Brantly B-2A: Initial production version.
  • Brantly B-2B: Improved version, fitted with new metal rotor blades, and an uprated fuel-injected 180 hp Lycoming piston engine.
  • Brantly 305: Larger five-seat version.
  • H-2: Designation of the B-2B built by Brantly-Hynes between 1976 and 1979.
  • Brantly B-2J10: Projected tandem-rotor version with longer and wider fuselage for carrying passengers and/or cargo. Unbuilt.
  • V750 UAV: An UAV version developed by Qingdao Haili Helicopters Co. Ltd., a joint venture between Brantly International Inc, Qingdao Wenquan International Aviation Investment Co., Ltd, and Qingdao Brantly Investment Consultation Co., Ltd.[4] Maiden flight was completed on May 7, 2011, and received an order from an unnamed customer[5]

Accidents and incidents edit

The B-2 has had 21 fatal accidents between February 1964 and August 2009.[6]

Survivors edit

A B2B belonging to the Flying Gyrocopter and Old Aircraft museum at Midden-Zeeland, Netherlands was reportedly about to fly again November 2009.[7]

A Greek road-assistance company named Express Service based in Thessaloniki operated a B2B Brantly-Hynes helicopter for several years. That helicopter started flying in 1978 and had the Greek registration number SX-AHH. First captain was the pilot Kaltekis Spyridon.

B2 sn#18 is in Chino awaiting restoration after the 2005/2010 floods at Corona airport,a month underwater did little corrosive damage... , a B2B acquired for spares to complete restoration (dual serial numbers found "spliced together bird")

Specifications (B-2B with skid landing gear) edit

Data from Jane's All the World's Aircraft 1976–77.[8]

General characteristics

  • Crew: 2
  • Length: 21 ft 9 in (6.63 m)
  • Height: 6 ft 9 in (2.06 m)
  • Empty weight: 1,020 lb (463 kg)
  • Max takeoff weight: 1,670 lb (757 kg)
  • Fuel capacity: 31 US gal (26 imp gal; 120 L)
  • Powerplant: 1 × Avco Lycoming IVO-360-A1A air-cooled flat-four engine, 180 hp (130 kW)
  • Main rotor diameter: 23 ft 9 in (7.24 m)
  • Main rotor area: 442 sq ft (41.1 m2)

Performance

  • Maximum speed: 100 mph (160 km/h, 87 kn) at sea level
  • Cruise speed: 90 mph (140 km/h, 78 kn) (75% power)
  • Range: 250 mi (400 km, 220 nmi)
  • Service ceiling: 10,800 ft (3,300 m)
  • Rate of climb: 1,900 ft/min (9.7 m/s)

See also edit

Related lists

References edit

  1. ^ a b Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 189. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^ Harding 1990, pp. 73–74.
  3. ^ Frawley, Gerard. The International Directory of Civil Aircraft. Aerospace Publications Pty Ltd, 1997. ISBN 1-875671-26-9.
  4. ^ http://www.aviationweek.com/aw/blogs/defense/index.jsp?plckController=Blog&plckScript=blogScript&plckElementId=blogDest&plckBlogPage=BlogViewPost&plckPostId=Blog:27ec4a53-dcc8-42d0-bd3a-01329aef79a7Post:de32542d-5108-45db-b600-be5e7ad5f935 [dead link]
  5. ^ . Archived from the original on 2011-06-07. Retrieved 2011-09-06.
  6. ^ "R44 Accident Database". Griffin Helicopters. Retrieved 30 January 2010.[permanent dead link]
  7. ^ FlyPast, November 2009, p.17
  8. ^ Taylor 1976, p. 252.

Bibliography edit

  • "Aircraft Production List: 5: The Brantly B-2: Part One". Archive. No. 4. Air-Britain. 1990. pp. 91–92. ISSN 0262-4923.
  • Bridgman, Leonard; Taylor, John W. R., eds. (1958). Jane's All the World's Aircraft 1958–59. London: Sampson Low, Marston & Company. Ltd.
  • Elliott, Bryn (January–February 1999). "On the Beat: The First 60 Years of Britain's Air Police". Air Enthusiast. No. 79. pp. 68–75. ISSN 0143-5450.
  • Elliott, Bryn (May–June 1999). "On the Beat: The First 60 Years of Britain's Air Police, Part Two". Air Enthusiast. No. 81. pp. 64–69. ISSN 0143-5450.
  • Frawley, Gerard. The International Directory of Civil Aircraft. Aerospace Publications Pty Ltd, 1997. ISBN 1-875671-26-9.
  • Harding, Stephen (1990). U.S Army Aircraft since 1947. Shrewsbury, UK: Airlife. ISBN 1-85310-102-8.
  • Taylor, John W. R., ed. (1976). Jane's All the World's Aircraft 1976–77. London: Jane's Yearbooks. ISBN 0-354-00538-3.

Further reading edit

  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). London: Orbis Publishing.
  • 'Aviation Week, 1965
  • "British-built Brantlys?" FLIGHT, 30 January 1959

External links edit

  • Specs & Photo at Flugzeuginfo.net
  • Brantly B-2J10 at Stingray's List of Rotorcraft

brantly, american, seat, light, helicopter, produced, brantly, helicopter, corporation, brantly, hover, role, light, helicopter, manufacturer, brantly, helicopter, corporation, designer, newby, brantly, first, flight, february, 1953, introduction, 1958, status. The Brantly B 2 is an American two seat light helicopter produced by the Brantly Helicopter Corporation Brantly B 2 Brantly B2 in a hover Role Light Helicopter Manufacturer Brantly Helicopter Corporation Designer Newby O Brantly First flight 21 February 1953 Introduction 1958 Status In production 2011 1 Number built 334 Contents 1 Design and development 2 Operational history 3 Variants 4 Accidents and incidents 5 Survivors 6 Specifications B 2B with skid landing gear 7 See also 8 References 9 Bibliography 10 Further reading 11 External linksDesign and development editAfter the failure of his first design the Brantly B 1 Newby O Brantly decided to design a simpler and less complicated helicopter for the private buyer citation needed The B 2 had a single main rotor and an anti torque tail rotor and first flew on 21 February 1953 This was followed by an improved second prototype that first flew on 14 August 1956 The B 2A was introduced with a modified cabin and the B 2B had a larger 180 hp fuel injected engine The B 2B has a three bladed articulated main rotor and an all metal fuselage it can be operated with skid wheel or float landing gear The piston engine is fitted vertically in the fuselage behind the cabin Operational history editThe basic design has remained in production for over 50 years 1 The United States Army ordered five B 2s designated the YHO 3 to be evaluated in the Light Observation Helicopter competition in 1958 although it lost the bid the Army operated the H 5T unmanned variant as target from 1986 2 Introduced in the early 1970s an improved larger version with five seats was designated the Brantly 305 3 Variants edit nbsp The unbuilt Brantly B2J10 10 seat transport helicopter Was to be powered by two Allison 250 C18 or two Boeing 550 1 12C engines Brantly B 2 Two seat single engined light utility helicopter Brantly YHO 3 United States military designation for the B2 Brantly B 2A Initial production version Brantly B 2B Improved version fitted with new metal rotor blades and an uprated fuel injected 180 hp Lycoming piston engine Brantly 305 Larger five seat version H 2 Designation of the B 2B built by Brantly Hynes between 1976 and 1979 Brantly B 2J10 Projected tandem rotor version with longer and wider fuselage for carrying passengers and or cargo Unbuilt V750 UAV An UAV version developed by Qingdao Haili Helicopters Co Ltd a joint venture between Brantly International Inc Qingdao Wenquan International Aviation Investment Co Ltd and Qingdao Brantly Investment Consultation Co Ltd 4 Maiden flight was completed on May 7 2011 and received an order from an unnamed customer 5 Accidents and incidents editThe B 2 has had 21 fatal accidents between February 1964 and August 2009 6 Survivors editB 2 N2143U was purchased in 1962 and flown by Dean Svec for all of its total of 2 108 hrs It was retired in 2006 and is now on permanent public display at the Crawford Auto Aviation Museum Western Reserve Historical Society in Cleveland Ohio A B2B belonging to the Flying Gyrocopter and Old Aircraft museum at Midden Zeeland Netherlands was reportedly about to fly again November 2009 7 A Greek road assistance company named Express Service based in Thessaloniki operated a B2B Brantly Hynes helicopter for several years That helicopter started flying in 1978 and had the Greek registration number SX AHH First captain was the pilot Kaltekis Spyridon B2 sn 18 is in Chino awaiting restoration after the 2005 2010 floods at Corona airport a month underwater did little corrosive damage a B2B acquired for spares to complete restoration dual serial numbers found spliced together bird Specifications B 2B with skid landing gear editData from Jane s All the World s Aircraft 1976 77 8 General characteristicsCrew 2 Length 21 ft 9 in 6 63 m Height 6 ft 9 in 2 06 m Empty weight 1 020 lb 463 kg Max takeoff weight 1 670 lb 757 kg Fuel capacity 31 US gal 26 imp gal 120 L Powerplant 1 Avco Lycoming IVO 360 A1A air cooled flat four engine 180 hp 130 kW Main rotor diameter 23 ft 9 in 7 24 m Main rotor area 442 sq ft 41 1 m2 Performance Maximum speed 100 mph 160 km h 87 kn at sea level Cruise speed 90 mph 140 km h 78 kn 75 power Range 250 mi 400 km 220 nmi Service ceiling 10 800 ft 3 300 m Rate of climb 1 900 ft min 9 7 m s See also editRelated lists List of military aircraft of the United StatesReferences edit a b Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 189 WDLA UK Lancaster UK 2011 ISSN 1368 485X Harding 1990 pp 73 74 Frawley Gerard The International Directory of Civil Aircraft Aerospace Publications Pty Ltd 1997 ISBN 1 875671 26 9 http www aviationweek com aw blogs defense index jsp plckController Blog amp plckScript blogScript amp plckElementId blogDest amp plckBlogPage BlogViewPost amp plckPostId Blog 27ec4a53 dcc8 42d0 bd3a 01329aef79a7Post de32542d 5108 45db b600 be5e7ad5f935 dead link 时事聚焦 俄媒 中国V750型最大无人机是美国B 2B改型 国际观察 天涯社区 Archived from the original on 2011 06 07 Retrieved 2011 09 06 R44 Accident Database Griffin Helicopters Retrieved 30 January 2010 permanent dead link FlyPast November 2009 p 17 Taylor 1976 p 252 Bibliography edit Aircraft Production List 5 The Brantly B 2 Part One Archive No 4 Air Britain 1990 pp 91 92 ISSN 0262 4923 Bridgman Leonard Taylor John W R eds 1958 Jane s All the World s Aircraft 1958 59 London Sampson Low Marston amp Company Ltd Elliott Bryn January February 1999 On the Beat The First 60 Years of Britain s Air Police Air Enthusiast No 79 pp 68 75 ISSN 0143 5450 Elliott Bryn May June 1999 On the Beat The First 60 Years of Britain s Air Police Part Two Air Enthusiast No 81 pp 64 69 ISSN 0143 5450 Frawley Gerard The International Directory of Civil Aircraft Aerospace Publications Pty Ltd 1997 ISBN 1 875671 26 9 Harding Stephen 1990 U S Army Aircraft since 1947 Shrewsbury UK Airlife ISBN 1 85310 102 8 Taylor John W R ed 1976 Jane s All the World s Aircraft 1976 77 London Jane s Yearbooks ISBN 0 354 00538 3 Further reading editThe Illustrated Encyclopedia of Aircraft Part Work 1982 1985 London Orbis Publishing Aviation Week 1965 British built Brantlys FLIGHT 30 January 1959External links edit nbsp Wikimedia Commons has media related to Brantly B 2 Specs amp Photo at Flugzeuginfo net Brantly B 2J10 at Stingray s List of Rotorcraft Retrieved from https en wikipedia org w index php title Brantly B 2 amp oldid 1126374772, wikipedia, wiki, book, books, library,

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