Армстронг Сиддели Гепарда
| Гепарда | |
|---|---|
| |
| Гепарда х | |
| Тип | Радиальный двигатель |
| Национальное происхождение | Великобритания |
| Производитель | Armstrong Siddeley Motors Ltd. |
| Первый забег | 1935 |
| Основные приложения | Airspeed Oxford |
| Number built | >37,200 |
| Developed from | Armstrong Siddeley Lynx |
Армстронг Сиддели Гепарда семицилиндровым британским воздушным радиальным двигателем охлаждением 834 куб воздушным . является с [ 1 ]
Гепарда использовалась для работы во многих британских самерах тренера во время Второй мировой войны, включая Avro Anson и Airspeed Oxford .
Дизайн и разработка
[ редактировать ]Гепарда была разработана из более ранней рыси с использованием увеличенных цилиндров с отверстиями от Армстронга Сиддели Пантеры, но двигатель сохранил ход рыси. Первоначально были изготовлены только варианты прямого привода, когда были предоставлены более поздние двигатели, доступные с помощью оборудования для уменьшения пропеллера различных соотношений . Нагнетатели были также доступны для последующих вариантов, как ориентированных, так и непосредственно управляемых коленчатым валом . [ 1 ]
The basic design of the Cheetah remained unchanged from its introduction in 1935 to the last examples built in 1948. It was the first engine of its type to be certified for 1,200 hours of operational time between overhauls (TBO), with over 37,200 examples built.[2]
Variants
[edit]- Lynx V (Lynx Major)
- 1930, 230 hp (171 kW).
- Cheetah V
- 1935, 270 hp (201 kW) at 2,100 rpm.
- Cheetah VA
- 1935, 285 hp (212 kW) at 2,425 rpm.
- Cheetah VI
- 1935, 307 hp (229 kW) at 2,425 rpm.
- Cheetah VIA
- 1936, as Mk VI but with Mk IX cylinders.
- Cheetah IX
- 1937, 345 hp (257 kW) at 2,425 rpm.
- Cheetah X
- 1938, 375 hp (280 kW) at 2,300 rpm.
- Cheetah XI
- 345 hp (257 kW) at 2,425 rpm, geared version of Cheetah X.
- Cheetah XII
- Similar to Mk X, adapted for target drone aircraft.
- Cheetah XV
- 420 hp (313 kW) at 2,425 rpm.
- Cheetah XVII
- 1948, 385 hp (287 kW) at 2,425 rpm.
- Cheetah XVIII
- 385 hp (287 kW) at 2,425 rpm, carburettor modified for aerobatics.
- Cheetah XIX
- 355 hp (265 kW) at 2,425 rpm
- Cheetah 25
- 345 hp (257 kW) at 2,425 rpm, Cheetah XV uprated to 475 hp (355 kW) at 2,700 rpm, modified constant-speed unit.
- Cheetah 26
- 385 hp (287 kW).
- Cheetah 27
- 1948, 385 hp (287 kW).
Applications
[edit]
- Airspeed Consul
- Airspeed Courier
- Airspeed Envoy
- Airspeed Oxford
- Airspeed Queen Wasp
- Airspeed Viceroy
- Avro 626
- Avro 652
- Avro Anson
- Blackburn Lincock
- Bristol Bulldog TM (type 124)[5]
- CASA C-201 Alcotán
- de Havilland Hawk Moth
- Handley Page H.P.R.2
- Hispano HS-42
- IAe.22 DL
- Kingsford Smith PL.7
- Koolhoven F.K.51
- Lancashire Aircraft Prospector
- Marinens Flyvebaatfabrikk M.F.8
- Marinens Flyvebaatfabrikk M.F.10
- Percival Provost (prototype)
- SEA.1
- VEF JDA-10M
Survivors
[edit]As of October 2008 at least four Cheetah engines remained airworthy. Two Cheetah 17s power the Anson T21 operated by the Classic Air Force and another pair of Cheetah 17s are fitted to Avro Nineteen, G-AHKX registered to BAE Systems but normally based at the Shuttleworth Collection.[6][7]
Engines on display
[edit]Preserved Armstrong Siddeley Cheetah engines are on public display at the following museums:
- Arkansas Air & Military Museum
- Aviation Heritage Museum (Western Australia)[8]
- Brooklands Museum
- City of Norwich Aviation Museum in Horsham St Faith, Norfolk.[9]
- Fleet Air Arm Museum
- Historical Aircraft Restoration Society Albion Park, New South Wales, Australia
- Malta Aviation Museum
- Port Elizabeth branch of the South African Air Force Museum
- Royal Air Force Museum Cosford
- South Australian Aviation Museum, Adelaide. Two Mk9 Operational Displays
Specifications (Cheetah IX)
[edit]
Data from [10]
General characteristics
- Type: Seven-cylinder single-row supercharged air-cooled radial engine
- Bore: 5.25 in (133 mm)
- Stroke: 5.5 in (140 mm)
- Displacement: 834 cu in (13.65 L)
- Length: 52.8 in (1,342 mm)
- Diameter: 47.6 in (1,210 mm)
- Dry weight: 637 lb (289 kg)
Components
- Valvetrain: Two pushrod-actuated valves per cylinder
- Supercharger: Centrifugal, 5.4:1 reduction
- Fuel system: Claudel-Hobson carburettor
- Fuel type: 87 octane rating petrol
- Cooling system: Air-cooled
- Reduction gear: No
Performance
- Power output:
- 338 hp (252 kW) at 2,100 rpm for takeoff
- 345 hp (257 kW) at 2,425 rpm at 7,875 ft (2,400 m)
- Specific power: 0.41 hp/cu in (18.83 kW/L)
- Compression ratio: 6.35:1
- Specific fuel consumption: 0.45 lb/hp/hr (271 g/kW/hr)
- Oil consumption: 0.24–0.45 oz/hp/hr (9–17 g/kW/hr)
- Power-to-weight ratio: 0.54 hp/lb (0.89 kW/kg)
See also
[edit]Related development
Comparable engines
- Avia Rk.17
- Bristol Neptune
- Gnome-Rhône 7K
- Jacobs R-830
- Piaggio Stella P.VII
- Pratt & Whitney Wasp Junior
- Wright R-760
Related lists
References
[edit]Notes
[edit]- ^ Jump up to: a b Lumsden 2003, p.74.
- ^ Gunston 1989, p.18.
- ^ Lumsden 2003, pp.74-76.
- ^ Cheetah variants start at Mk V.
- ^ Lumsden, Alec (2003). British Piston Engines and their Aircraft. Marlborough, UK: Airlife Publishing. p. 75. ISBN 1-85310-294-6.
- ^ CAA - G-INFO - G-VROE Archived 6 October 2015 at the Wayback Machine Retrieved: 15 February 2009
- ^ CAA - G-INFO - G-AHKX Archived 5 October 2015 at the Wayback Machine Retrieved: 15 February 2009
- ^ "Aviation Heritage Museum | Bull Creek, Perth".
- ^ "Engines List". City of Norwich Aviation Museum. Retrieved 27 August 2023.
- ^ Lumsden 2003, p.75.
Bibliography
[edit]- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
Further reading
[edit]- Bridgman, L, ed. (1998). Jane's fighting aircraft of World War II. Crescent. ISBN 978-0-517-67964-7.
- Gunston, Bill. Development of Piston Aero Engines. Cambridge, England. Patrick Stephens Limited, 2006. ISBN 0-7509-4478-1
Внешние ссылки
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