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Bell D-292

The Bell D-292 was an American experimental helicopter developed by Bell Helicopters for the United States Army Advanced Composite Airframe Program (ACAP), as part of the studies involved in the Light Helicopter Experimental (LHX) program.

D-292
The U.S. Army Bell D-292 conducting a flight test
Role Experimental helicopter
National origin United States
Manufacturer Bell Helicopter
First flight 30 August 1985
Number built 1
Developed from Bell 222

Design and development edit

The Bell D-292 was developed under the US Army's Advanced Composite Airframe Program (ACAP), which was a project to develop an all-composite helicopter fuselage, considerably lighter and less costly to build than predominantly metal airframes, in support of the LHX program.[1][2] In February 1981, contracts were awarded to Sikorsky and Bell Helicopters, with Sikorsky submitting the S-75.[3] Both companies were to build three airframes, one tool-proof version, one static-test version and a flight-test vehicle.[3]

The Bell D-292 used the Avco Lycoming engines, transmission, two-bladed main and tail rotors, tailboom, vertical fin, and rotor pylon from the Bell 222. The new airframe replaced metal with composites for greater strength, reduced weight and both lower manufacturing and maintenance costs.

The D-292 serial number 85-24371 flew for the first time on 30 August 1985[4] following delays due to funding and industrial problems.[3]

Specifications edit

General characteristics

  • Crew: four
  • Length: 40 ft 5 in (12.32 m)
  • Height: 11 ft 2 in (3.40 m)
  • Empty weight: 5,765 lb (2,615 kg)
  • Max takeoff weight: 7,485 lb (3,395 kg)
  • Powerplant: 2 × Avco Lycoming LTS 101-750C-1 turboshaft, 684 hp (510 kW) each
  • Main rotor diameter: 42 ft 0 in (12.80 m)

See also edit

Related development

Aircraft of comparable role, configuration, and era

Related lists

References edit

Notes edit

  1. ^ Harding 1997
  2. ^ Historic US Army Helicopters 2007-02-24 at the Wayback Machine
  3. ^ a b c "Bell admits ACAP delays". Flight International. 1985-01-12.
  4. ^ "Bell ACAP takes off". Flight International: 9. 1985-09-21.

Bibliography edit

  • Harding, Stephen (1997). U.S. Army Aircraft Since 1947. Atglen, PA, USA: Schiffer Publishing Ltd. ISBN 978-0-933424-53-1.

bell, american, experimental, helicopter, developed, bell, helicopters, united, states, army, advanced, composite, airframe, program, acap, part, studies, involved, light, helicopter, experimental, program, 292the, army, conducting, flight, testrole, experimen. The Bell D 292 was an American experimental helicopter developed by Bell Helicopters for the United States Army Advanced Composite Airframe Program ACAP as part of the studies involved in the Light Helicopter Experimental LHX program D 292The U S Army Bell D 292 conducting a flight testRole Experimental helicopterNational origin United StatesManufacturer Bell HelicopterFirst flight 30 August 1985Number built 1Developed from Bell 222 Contents 1 Design and development 2 Specifications 3 See also 4 References 4 1 Notes 4 2 BibliographyDesign and development editThis section needs expansion with information on later D 292 history You can help by adding to it September 2010 The Bell D 292 was developed under the US Army s Advanced Composite Airframe Program ACAP which was a project to develop an all composite helicopter fuselage considerably lighter and less costly to build than predominantly metal airframes in support of the LHX program 1 2 In February 1981 contracts were awarded to Sikorsky and Bell Helicopters with Sikorsky submitting the S 75 3 Both companies were to build three airframes one tool proof version one static test version and a flight test vehicle 3 The Bell D 292 used the Avco Lycoming engines transmission two bladed main and tail rotors tailboom vertical fin and rotor pylon from the Bell 222 The new airframe replaced metal with composites for greater strength reduced weight and both lower manufacturing and maintenance costs The D 292 serial number 85 24371 flew for the first time on 30 August 1985 4 following delays due to funding and industrial problems 3 Specifications editGeneral characteristics Crew four Length 40 ft 5 in 12 32 m Height 11 ft 2 in 3 40 m Empty weight 5 765 lb 2 615 kg Max takeoff weight 7 485 lb 3 395 kg Powerplant 2 Avco Lycoming LTS 101 750C 1 turboshaft 684 hp 510 kW each Main rotor diameter 42 ft 0 in 12 80 m See also editRelated development Bell 222Aircraft of comparable role configuration and era Boeing Model 360 Sikorsky S 75Related lists List of helicoptersReferences editNotes edit Harding 1997 Historic US Army Helicopters Archived 2007 02 24 at the Wayback Machine a b c Bell admits ACAP delays Flight International 1985 01 12 Bell ACAP takes off Flight International 9 1985 09 21 Bibliography edit Harding Stephen 1997 U S Army Aircraft Since 1947 Atglen PA USA Schiffer Publishing Ltd ISBN 978 0 933424 53 1 Retrieved from https en wikipedia org w index php title Bell D 292 amp oldid 1149351290, wikipedia, wiki, book, books, library,

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