Westland Widgeon (helicopter)

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Widgeon
FileWestlandwidgeon560 (cropped).jpg
Westland WS-51A Widgeon
General information
Type Helicopter
Manufacturer Westland Aircraft
Number built12 new built plus 3 conversions [1]
History
First flight23 August 1955
Developed from Westland WS-51 Dragonfly

The Westland Widgeon was a helicopter developed by Westland Aircraft as a private venture improvement on the Westland WS-51 Dragonfly.

Contents

Design and development

Westland Aircraft decided to make a private venture improvement on the Westland WS-51 Dragonfly helicopter, which was a licensed Sikorsky Aircraft design, by increasing the cabin capacity and replacing the Dragonfly's rotor head, blades and gearbox with the units used in the Westland Whirlwind. Three Dragonfly Series 1As were converted to WS-51 Series 2 Widgeon specifications and the first one flew on 23 August 1955. One of these conversions, registration G-ANLW, was the first helicopter to land at the London Heliport on 8 April 1959, and later appeared in the 1971 film, When Eight Bells Toll . [2]

In 1957, there was a plan to take up to 24 existing Fleet Air Arm Dragonflies to Dragonfly HC.7 standard (as the Naval Widgeon was to become) but this was abandoned and it contributed to the decision to stop progress. [3]

Variants

WS-51 Series 2 Widgeon
12 new aircraft and three conversions from Series 1A Dragonflies. [1]
Dragonfly HC.7
Proposed conversion of Fleet Air Arm Dragonflies to Widgeon standard. 24 conversions planned but never carried out. [3]
UH-1
Brazilian Navy designation for the Widgeon. Originally designated HUW. [4]

Operators

Flag of Brazil.svg  Brazil
Flag of Sri Lanka.svg Ceylon
Flag of Hong Kong 1959.svg  Hong Kong
Flag of Jordan.svg  Jordan
Flag of Nigeria.svg  Nigeria
Flag of the United Kingdom.svg  United Kingdom

Surviving aircraft

Brazil

United Kingdom

Specifications (Widgeon)

Data from Westland Aircraft since 1915, [1] Jane's all the World's Aircraft 1957-58 [15]

General characteristics

One-hour rating: 470 hp (350 kW) at 38 inHg (130 kPa) at 6,000 ft (1,800 m) at 2,900 rpm [16]
Maximum continuous power: 375 hp (280 kW) at 2,800 rpm
Maximum weak mixture power: 305 hp (227 kW) at 31 inHg (100 kPa) at 2,800 rpm [16]

Performance

See also

Related development

Aircraft of comparable role, configuration, and era

References

Notes

  1. 1 2 3 James 1991, p. 320.
  2. "G-ANLW Westland Dragonfly". www.helis.com. Retrieved 1 July 2021.
  3. 1 2 Beaver, Paul (1987). Encyclopaedia of the Fleet Air Arm Since 1945. Yeovil, Somerset: Patrick Stephens Ltd. p. 176. ISBN   978-0850597608.
  4. "Brazilian Military Aircraft Designations". designation-systems.net. Retrieved 16 March 2025.
  5. "WORLD HELICOPTER MARKET 1967 pg. 58". flightglobal. Retrieved 18 October 2014.
  6. "WORLD HELICOPTER MARKET 1967 pg. 60". flightglobal. Retrieved 18 October 2014.
  7. Iliffe-Moon, Peter (17 May 1973). "The unarmed air force". Flight International . Vol. 103, no. 3349. p. 759.
  8. "WORLD HELICOPTER MARKET 1967 pg. 62". flightglobal. Retrieved 18 October 2014.
  9. Draper 1999 , pp. 80–82
  10. Flight International 11 July 1968, p. 55.
  11. "Museu da Aviação Naval | ComForAerNav". www.marinha.mil.br. Retrieved 12 July 2024.
  12. "New life for-historic Widgeon helicopter, G-ANLW". 15 October 2021. Retrieved 4 January 2025.
  13. "Restoration of Westland WS.51A Widgeon, G-AOZE" . Retrieved 4 January 2025.
  14. "Westland Widgeon: G-APTW" . Retrieved 25 April 2025.
  15. Bridgman, Leonard, ed. (1957). Jane's all the World's Aircraft 1957-58. London: Sampson Low, Marston & Company, Ltd. pp. 81–82.
  16. 1 2 3 4 5 6 7 8 "WIDGEON AND WHIRLWIND —with Power by Alvis: A Report on Two Current Westland Developments". Flight and Aircraft Engineer. 68 (2449): 976–977. 30 December 1955. Retrieved 9 April 2019.

Bibliography