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Boeing Model 360

The Boeing Model 360 is an American experimental medium-lift tandem rotor cargo helicopter developed privately by Boeing to demonstrate advanced helicopter technology. The aircraft was intended as a technology demonstrator, with no plans to put the type into production, and many of its design features were carried onto other programs including the RAH-66 Comanche and V-22 Osprey. The sole prototype has been preserved and is a static exhibit at the American Helicopter Museum in West Chester, Pennsylvania.

Boeing Model 360
Role Experimental Helicopter
National origin United States
Manufacturer Boeing Helicopters
First flight June 10, 1987
Status Retired
Primary user Boeing Helicopters
Produced 1987
Number built 1

Design and development edit

Boeing Vertol developed its Model 360 in the 1980s as a technology demonstrator with company funds. It was a new design and made significant use of composites.[1]

The Boeing Model 360 differed from its brethren CH-46 and CH-47 tandem rotor helicopters by incorporating extensive amounts of composite materials in structural and dynamic components, namely in advanced rotor heads composed of fiberglass and graphite composites, along with graphite fuselage frames and longerons. The exterior of the craft integrated a Nomex core, surfaced by a Kevlar woven mesh with graphite-strengthened edges. The two tandem four-bladed counter-rotating rotors were each driven by Avco Lycoming AL5512 turboshaft engines mounted on either side of the rear fuselage. In another departure from its military brethren, the Model 360 had no external sponsons containing the landing gear or fuel, the tricycle landing gear instead retracting into the main fuselage. Fuel was contained in three crashworthy cells below the cabin floor.

The Model 360 featured a glass cockpit with six multi-function displays (MFD).[1]

Specifications edit

Data from Jane's All The World's Aircraft 1988–89[2]

General characteristics

  • Length: 51 ft 0 in (15.54 m) fuselage only
  • Cabin width: 6 ft 4 in (2 m) maximum
  • Cabin height: 5 ft 11 in (2 m) maximum
  • Height: 19 ft 4.75 in (5.9119 m)
  • Gross weight: 30,500 lb (13,835 kg)
  • Fuel capacity: 824 US gal (686.1 imp gal; 3,119.2 L) in 1x 238 US gal (198.2 imp gal; 900.9 L) rear fuselage tank and 2x 293 US gal (244.0 imp gal; 1,109.1 L) forward fuselage tanks
  • Powerplant: 2 × Textron Lycoming AL5512 turboshaft engines, 4,200 shp (3,100 kW) each
  • Main rotor diameter: 2 × 50 ft 0 in (15.24 m)
  • Main rotor area: 3,927.5 sq ft (364.88 m2)
  • Blade section: - root: Boeing VR-12; tip: Boeing VR-15[3]

Performance

  • Maximum speed: 200 kn (230 mph, 370 km/h)
  • Cruise speed: 180 kn (210 mph, 330 km/h)
  • Never exceed speed: 235 kn (270 mph, 435 km/h)
  • Disk loading: 7.766 lb/sq ft (37.92 kg/m2)

See also edit

Related development

Aircraft of comparable role, configuration, and era

References edit

  1. ^ a b Norton, Bill (2004). Bell Boeing V-22 Osprey : tiltrotor tactical transport. Leicester: Midland Publishig : Aerofax. p. 20. ISBN 1-85780-165-2.
  2. ^ Taylor, John W.R., ed. (1988). Jane's All the World's Aircraft 1988-89 (79th ed.). London: Jane's Information Group. p. 368. ISBN 0-7106-0867-5.
  3. ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.

External links edit

  • Boeing 360 on Janes Aircraft
  • Ground Shake Test of the Boeing Model 360 Helicopter Airframe, NASA, March 1989, Retrieved Dec 12, 2008

boeing, model, american, experimental, medium, lift, tandem, rotor, cargo, helicopter, developed, privately, boeing, demonstrate, advanced, helicopter, technology, aircraft, intended, technology, demonstrator, with, plans, type, into, production, many, design,. The Boeing Model 360 is an American experimental medium lift tandem rotor cargo helicopter developed privately by Boeing to demonstrate advanced helicopter technology The aircraft was intended as a technology demonstrator with no plans to put the type into production and many of its design features were carried onto other programs including the RAH 66 Comanche and V 22 Osprey The sole prototype has been preserved and is a static exhibit at the American Helicopter Museum in West Chester Pennsylvania Boeing Model 360 Role Experimental Helicopter National origin United States Manufacturer Boeing Helicopters First flight June 10 1987 Status Retired Primary user Boeing Helicopters Produced 1987 Number built 1 Contents 1 Design and development 2 Specifications 3 See also 4 References 5 External linksDesign and development editBoeing Vertol developed its Model 360 in the 1980s as a technology demonstrator with company funds It was a new design and made significant use of composites 1 The Boeing Model 360 differed from its brethren CH 46 and CH 47 tandem rotor helicopters by incorporating extensive amounts of composite materials in structural and dynamic components namely in advanced rotor heads composed of fiberglass and graphite composites along with graphite fuselage frames and longerons The exterior of the craft integrated a Nomex core surfaced by a Kevlar woven mesh with graphite strengthened edges The two tandem four bladed counter rotating rotors were each driven by Avco Lycoming AL5512 turboshaft engines mounted on either side of the rear fuselage In another departure from its military brethren the Model 360 had no external sponsons containing the landing gear or fuel the tricycle landing gear instead retracting into the main fuselage Fuel was contained in three crashworthy cells below the cabin floor The Model 360 featured a glass cockpit with six multi function displays MFD 1 Specifications editData from Jane s All The World s Aircraft 1988 89 2 General characteristicsLength 51 ft 0 in 15 54 m fuselage only Cabin width 6 ft 4 in 2 m maximum Cabin height 5 ft 11 in 2 m maximum Height 19 ft 4 75 in 5 9119 m Gross weight 30 500 lb 13 835 kg Fuel capacity 824 US gal 686 1 imp gal 3 119 2 L in 1x 238 US gal 198 2 imp gal 900 9 L rear fuselage tank and 2x 293 US gal 244 0 imp gal 1 109 1 L forward fuselage tanks Powerplant 2 Textron Lycoming AL5512 turboshaft engines 4 200 shp 3 100 kW each Main rotor diameter 2 50 ft 0 in 15 24 m Main rotor area 3 927 5 sq ft 364 88 m2 Blade section root Boeing VR 12 tip Boeing VR 15 3 Performance Maximum speed 200 kn 230 mph 370 km h Cruise speed 180 kn 210 mph 330 km h Never exceed speed 235 kn 270 mph 435 km h Disk loading 7 766 lb sq ft 37 92 kg m2 See also editRelated development Boeing Vertol CH 46 Sea Knight Boeing CH 47 Chinook Aircraft of comparable role configuration and era Bell D 292 Sikorsky S 75References edit a b Norton Bill 2004 Bell Boeing V 22 Osprey tiltrotor tactical transport Leicester Midland Publishig Aerofax p 20 ISBN 1 85780 165 2 Taylor John W R ed 1988 Jane s All the World s Aircraft 1988 89 79th ed London Jane s Information Group p 368 ISBN 0 7106 0867 5 Lednicer David The Incomplete Guide to Airfoil Usage m selig ae illinois edu Retrieved 16 April 2019 External links editBoeing 360 on Janes Aircraft Ground Shake Test of the Boeing Model 360 Helicopter Airframe NASA March 1989 Retrieved Dec 12 2008 N360BV Prototype on Airliners net Retrieved from https en wikipedia org w index php title Boeing Model 360 amp oldid 1192197190, wikipedia, wiki, book, books, library,

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