ADC (de "Aircraft Disposal Company") [3] compró 35.000 motores excedentes de guerra en 1920. Inicialmente produjo motores a partir de repuestos Renault de 70 hp .
División de Bristol Aeroplane Company formada cuando Cosmos Engineering fue adquirida en 1920. Se convirtió en Bristol Aero Engines en 1956. Se fusionó con Armstrong Siddeley en 1958 para formar Bristol Siddeley. Fuentes: Motores de pistón, Lumsden, [3] turbinas de gas y motores de cohetes, Gunston. [14]
Estatorreactor Bristol BRJ.1 de 6 pulgadas, modelo de desarrollo inicial utilizando cámara de combustión Boeing.
Estatorreactor Bristol BRJ.2 de 16 pulgadas. BRJ1 a mayor escala con cámara de combustión Boeing.
Estatorreactor Bristol BRJ.2/5 M2 de 16 pulgadas. Utilizado en los primeros Red Duster. Conocido por el Ministerio de Ciencia como BT.1 Thor
Estatorreactor Bristol BRJ.3 M2 de 16 pulgadas. Equipado con cámara de combustión NGTE y utilizado en difracción de rayos X. Capacidad nominal de 100 000 lbf (440 kN) en M3, Ø = 16 pulgadas (41 cm)
Estatorreactor Bristol BRJ.4/1 M2 de 16 pulgadas. Utilizado en los primeros Red Duster y Bloodhound I. Conocido por el Ministerio de Defensa como BT.2 Thor
Estatorreactor Bristol BRJ.5/1 M2 de 16 pulgadas. Utilizado en el Bloodhound II. Se convirtió en el BT.3 Thor
Estatorreactor Bristol BRJ.601 M3 de 16 pulgadas. Probado en bobina.
Estudio del proyecto Bristol BRJ.701 23in M3 ramjet.
Bristol BRJ.801 [21]
Estatorreactor Bristol BRJ.801 M3 de 18 pulgadas. Estatorreactor M3 inicial desarrollado para la etapa 1 3 ⁄ 4 del Blue Envoy .
Bristol BRJ.811 estatorreactor M3 de 18 pulgadas. Ramjet M3 desarrollado para la etapa 1 3 ⁄ 4 Blue Envoy.
Estatorreactor Bristol BRJ.824 M3 de 18 pulgadas. Cancelado con Blue Steel Mk2.
Bristol Siddeley
Bristol Siddeley se formó cuando Bristol adquirió Armstrong Siddeley y cambió la marca de varios de los motores. Adquirió los motores de Havilland y, a su vez, se convirtió en una división de Rolls-Royce Limited .
Bristol Siddeley BS.1009 Bristol Siddeley M3 Ramjet. BT.3 Thor modificado destinado al Bloodhound III propuesto. Tobera, admisión y difusor modificados. [10]
Licenciatura en Bristol Siddeley, 1010
Bristol Siddeley BS.1011 Clasificado en 40000 lb (177,9 KN).
Bristol Siddeley BS.1012 Central eléctrica combinada Bristol Siddeley para APD 1019 y P.42. Turbomáquinas Olympus o BS.100 utilizadas, combustión en conductos de derivación y estatorreactores.
Bristol Siddeley BS.1013 Estudio de estatorreactor Bristol Siddeley para misiles de largo alcance. Posiblemente para Pandora.
Farcot 65 hp 8cyl radial 105 mm × 120 mm (4.13 in × 4.72 in)[2]
Farcot 100 hp 8cyl radial[18][2]
Farina
(S.A. Stabilimenti Farina)
Farina Algol[42]
Farina Aligoth[42]
Farina T.58[15]
Farman
Source:Liron[95][96]Note: Farman engine designations differ from other French manufacturers in using the attributes as the basis of the designation, thus; Farman 7E (7-cyl radial E – Etoile / Star / Radial) or Farman 12We (W-12 fifth type – the e is not a variant or sub-variant it is the type designator). As usual there are exceptions such as the 12Gvi, 12B, 12C and 18T.
Gnome et Rhône[14][18] except where noted
Im French engine designations —even— sub-series numbers (for example Gnome-Rhône 14N-68) rotated anti-clockwise (LH rotation) and were generally fitted on the starboard side, —odd numbers— (for example Gnome-Rhône 14N-69) rotated clockwise (RH rotation) and were fitted on the port side.
Gnome Monosoupape rotary engine of 1917
Gnome
Gnome 1906 25 hp rotary – prototype Gnome rotary engine
Gnome 34 hp 5-cyl rotary 100 mm × 100 mm (3.9 in × 3.9 in)[18][2]
Gnome 123 hp 14-cyl rotary 110 mm × 120 mm (4.33 in × 4.73 in)[18]
Gnome 1907 50 hp
Gnome 7 Gamma 70 hp 130 mm × 120 mm (5.1 in × 4.7 in)[2][3]
Orenda Engines, formed by Avro Canada taking over publicly funded jet engine development by Turbo Research.[14] Later became Orenda Aerospace under Magellan.
Société nationale d'études et de construction de moteurs d'aviation formed by nationalisation of Gnome et Rhône in 1945. On French engine designations even sub-series numbers (for example Gnome-Rhône 14N-68) rotated anti-clockwise (LH rotation) and were generally fitted on the starboard side, odd numbers (for example Gnome-Rhône 14N-69) rotated clockwise (RH rotation) and were fitted on the port side.
Tips 480 hp 250 hp 4.5 in × 6 in (110 mm × 150 mm)[2] (18 cyl., 1717.67 ci, air- and water-cooled rotary engine. At rated RPM the crankshaft rotated at 1800 rpm, propeller shaft at 1080 rpm and the engine body at 60 rpm. Cooling was by direct air flow and tubular radiators between the cylinders, with water circulating without hoses or pumps.)[2]
Tips & Smith Super-Rhône
Tomonoo
(Tomon Naoji)
Tomono 90 hp 6-cyl in-line 4.5 in × 4.375 in (114.3 mm × 111.1 mm)[2]
Tone
Tone 2V9 180 hp 4.5 in × 4.375 in (114.3 mm × 111.1 mm)[2]
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