List of aircraft engines
Piston engines
The listed piston engines were or are still being built in a wide variety of variants and outputs. The specification of the engine power refers to the most powerful version.
A-C
D-H
Engine | Type of cooling |
cylinder | Max. Power kW) | Country of origin | Application example | First run | Remarks |
---|---|---|---|---|---|---|---|
Daimler-Benz DB 600 |
V-engine , suspended, liquid-cooled |
12 | 810 | German Empire | 1935 | Version with carburetor | |
Daimler-Benz DB 601 |
V-engine , suspended, liquid-cooled |
12 | 810 | German Empire | 1937 | Further developed version of the DB 600 with gasoline injection | |
Daimler-Benz DB 603 |
V-engine , suspended, liquid-cooled |
12 | 2060 | German Empire | 1942 | Further developed version of the DB 601 with increased cubic capacity | |
Daimler-Benz DB 604 |
X-motor liquid-cooled |
24 | 1922 | German Empire | ? | Development stopped in September 1944 | |
Daimler-Benz DB 605 |
V-engine , suspended, liquid-cooled |
12 | 1470 | German Empire | 1941 | Further developed version of the DB 601 with increased cubic capacity. With over 42,000 units, it is one of the most popular German piston aircraft engines of the Second World War . | |
Daimler-Benz DB 606 |
Double-V-engine , hanging liquid-cooled |
24 | 1985 | German Empire | 1939 | Consists of two DB 601s coupled in a mirror image at an angle of 44 ° via a gearbox | |
Daimler-Benz DB 610 |
Double-V-engine , hanging liquid-cooled |
24 | 2170 | German Empire | ? | Consists of two DB 605 coupled in a mirror image at an angle of 44 ° | |
Daimler-Benz DB 613 |
Double-V-engine , hanging liquid-cooled |
24 | 2794 | German Empire | ? | Consists of two DB 603 coupled in mirror image at an angle of 44 ° via a gearbox | |
De Havilland Gipsy |
In-line engine , standing air-cooled |
4th | 90 | United Kingdom | 1927 | ||
De Havilland Gipsy Major |
In-line engine , hanging air-cooled |
4th | 108 | United Kingdom | 1932 | ||
De Havilland Gipsy Six |
In-line engine , hanging air-cooled |
6th | 149 | United Kingdom | 1935 | ||
De Havilland Gipsy Queen |
In-line engine , hanging air-cooled |
6th | 280 | United Kingdom | 1936 | Military version of the De Havilland Gipsy Six , higher performance by charging | |
De Havilland Gipsy Twelve |
V-engine , hanging air-cooled |
12 | 312 | United Kingdom | 1937 | ||
Dobrynin WD-4K |
Radial engine, 4-fold air-cooled |
24 | 3160 | Soviet Union | 1950 | Turbo compound engine | |
Duesenberg Special A |
In-line engine , vertical, liquid-cooled |
4th | 85 | United States | 1915 | Duesenberg's walking beam valve control , 8 valves | |
Duesenberg Special A-3 |
In-line engine , vertical, liquid-cooled |
4th | 125 | United States | 1915 | Walking beam valve control, 16 valves | |
Duesenberg V-12 |
V-engine , upright liquid-cooled |
12 | 350 | United States | 1916 | Experimental engine; Walking beam valve control, 24 valves | |
Duesenberg Model H. |
V-engine , upright liquid-cooled |
16 | 700 | United States | 1918 | Experimental engine; Walking beam valve control, 48 valves | |
Elizalde Beta |
Air- cooled radial engine |
9 | 578 | Spain | ? | Developed on the basis of the Wright R-1820 | |
Fiat A.12 |
In-line engine , vertical, liquid-cooled |
6th | 220 | Italy | 1916 | ||
Fiat A.80 |
Radial engine, 2-fold air-cooled |
18th | 785 | Italy | 1935 | Development based on the Pratt & Whitney R-1690 | |
Fiat AS.3 |
V-engine , upright liquid-cooled |
12 | 736 | Italy | 1927 | ||
Fiat AS.6 |
Double V engine , vertical, liquid-cooled |
24 | 2200 | Italy | 1927 | Motor for racing use | |
Gnome Monosoupape 7 |
Rotary motor air-cooled |
7th | 60 | France | 1916 | ||
Gnome Monosoupape 9B-2 |
Rotary motor air-cooled |
9 | 75 | France | 1916 | ||
Gnome Monosoupape 9N |
Rotary motor air-cooled |
9 | 119 | France | 1916 | ||
Gnome et Rhône 5K titanium |
Air- cooled radial engine |
5 | 190 | France | 1927 | Further development of the Bristol Titan | |
Gnome et Rhône 7K Titan Major |
Air- cooled radial engine |
7th | 270 | France | 1927 | ||
Gnome et Rhône 9K Mistral |
Air- cooled radial engine |
9 | 405 | France | 1927 | ||
Gnome et Rhône 14K Mistral Major |
Radial engine, 2-fold air-cooled |
14th | 750 | France | 1929 | ||
Gnome et Rhône 14M Mars |
Radial engine, 2-fold air-cooled |
14th | 560 | France | 1936 | ||
Gnome et Rhône 14N |
Radial engine, 2-fold air-cooled |
14th | 810 | France | 1936 | ||
Gnome et Rhône 14R |
Radial engine, 2-fold air-cooled |
14th | 1160 | France | 1939 | ||
Green C.4 |
In-line engine , vertical, liquid-cooled |
4th | 39 | United Kingdom | 1908 | ||
Guiberson A-1020 |
Air- cooled radial engine |
9 | 239 | United States | 1940 | Diesel engine , also used as a tank engine | |
Hirth HM 60 |
In-line engine , hanging air-cooled |
4th | 59 | German Empire | 1931 | ||
Hirth HM 500 |
In-line engine , hanging air-cooled |
4th | 77 | German Empire | 1938 | ||
Hirth HM 504 |
In-line engine , hanging air-cooled |
4th | 77 | German Empire | 1935 | ||
Hirth HM 506 |
In-line engine , hanging air-cooled |
6th | 118 | German Empire | 1935 | ||
Hirth HM 508 |
V-engine , hanging air-cooled |
8th | 225 | German Empire | 1937 | ||
Hirth HM 512 |
V-engine , hanging air-cooled |
12 | 335 | German Empire | 1938 | ||
Hirth HM 515 |
In-line engine , hanging air-cooled |
4th | 48 | German Empire | 1938 | ||
Hispano-Suiza 8 |
V-engine, liquid-cooled |
8th | 221 |
Spain Switzerland |
1915 | ||
Hispano-Suiza 12G |
Y-motor, 3-row liquid-cooled |
12 | 294 |
Spain Switzerland |
1920 | ||
Hispano-Suiza 12Y |
V-engine, liquid-cooled |
12 | 1160 |
Spain Switzerland |
1932 |
I-R
S-Z
Shaft power engines
The listed shaft power engines were or are being built in a wide variety of variants and outputs. The specification of the shaft power refers to the most powerful version.
- "Type" column
- LP : low pressure compressor / turbine
- MD : medium pressure compressor / turbine
- HD : high pressure compressor / turbine
- AT : power turbine
- FT : power
Engine | Type of compressor turbine |
waves | Max. Power kW) | Country of origin | Application example | First run | Remarks |
---|---|---|---|---|---|---|---|
Allison 250 / T63 |
Shaft turbine 7 × HD, 2 × HD, 2 × AT |
2 | 525 | United States | 1960 | ||
Allison 501-D / T56 |
Propeller turbine 14 × HD 4 × HD / AT |
1 | 3860 | United States | 1949 | ||
Armstrong Siddeley Double Mamba |
Double propeller turbine each 10 × HD each 2 × HD / AT |
1 each | 2200 | United Kingdom | 1949 | Twin engine with counter-rotating coaxial propellers | |
Armstrong Siddeley Mamba |
Propeller turbine 10 × HD 2 × HD / AT |
1 | 1100 | United Kingdom | 1946 | ||
Armstrong Siddeley Python |
Propeller turbine 14 × HD 2 × HD / AT |
1 | 3065 | United Kingdom | 1945 | ||
Bristol Proteus |
Propeller turbine 12 × HD, 2 × HD, 2 × AT |
2 | 2515 | United Kingdom | 1947 | ||
Europrop International TP400 |
Propeller turbine 5 × MD, 6 × HD 1 × HD, 1 × MD, 3 × ND / AT |
3 | 8200 |
Germany United Kingdom France Spain |
2005 | Most powerful single propeller engine | |
General Electric T31 |
Propeller turbine 1 × HD 1 × HD / AT |
1 | 1110 | United States | 1943 | First American turboprop -Triebwerk | |
General Electric T58 |
Wave turbine 10 × HD, 2 × HD, 1 × FT |
1 | 1390 | United States | 1955 | ||
General Electric T64 |
Propeller turbine Shaft turbine 14 × HD, 2 × HD, 2 × FT |
1 | 3540 | United States | ? | ||
General Electric T700 |
Wave turbine 1 × LP, 5 × HP, 2 × HP, 2 × LP / AT |
2 | 1491 | United States | 1973 | ||
Honeywell / Garrett TPE331 / T76 |
Propeller turbine 2 × HD 3 × HD / AT |
1 | 1209 | United States | 1960 | ||
Ivchenko Progress D-27 |
Propeller turbine 5 × LP, 3 × HP 1 × HP, 1 × LP, 4 × AT |
3 | 10440 | Russia | 1992 | ||
Ivchenko Progress D-136 |
Shaft turbine ? ? |
? | 9190 | Soviet Union | ? | Most powerful helicopter engine in the world | |
Jendrassik CS-1 |
Propeller turbine 15 × HD 7 × HD / AT |
1 | 295 | Hungary | 1940 | First turboprop engine in the world, projected for 1000 WPS , development discontinued in 1941 | |
Klimow TW3-117 |
Wave turbine 12 × HD, 2 × HD, 2 × FT |
1 | 1765 | Soviet Union | 1974 | So far, more than 25,000 pieces produced, used in 95% of all Russian helicopter, also after their retirement Tractorpulling used | |
Kuznetsov NK-12 |
Propeller turbine 14 × HD 5 × HD / AT |
1 | 11185 | Soviet Union | 1953 | Most powerful turboprop engine ever mass-produced | |
LHTEC T800 |
Wave turbine 2 × HD, 2 × HD, 2xFT |
2 | 1150 | United States | ? | ||
Lycoming T53 |
Propeller turbine Shaft turbine 6 × HD, 2 × HD, 2xFT |
1 | 1343 | United States | ? | Also used in diesel locomotives of the DB class 210 | |
MTR390 |
Shaft turbine 1 × LP, 2 × HP 1 × HP, 2 × LP / AT |
2 | 958 |
Germany United Kingdom France Spain |
1989 | ||
Napier Eland |
Propeller turbine 10 × HD 3 × HD / AT |
1 | 2610 | United Kingdom | 1953 | ||
Pratt & Whitney T73 |
Shaft turbine 9 × HD, 2 × HD, 2 × FT |
1 | 3355 | United States | ? | ||
Pratt & Whitney Canada PT6A / T74 |
Propeller turbine 4 × MD, 1 × HD 1 × HD, 2 × AT |
2 | 1175 | Canada | 1959 | ||
Pratt & Whitney Canada PT6B, C / T74 |
Wave turbine 4 × MD, 1 × HD 1 × HD, 2 × AT |
2 | 1252 | Canada | 1959 | ||
Pratt & Whitney Canada PW150 |
Propeller turbine 2 × LP, 2 × HP 1 × HP, 1 × LP, 2 × AT |
3 | 3781 | Canada | 1984 | ||
Pratt & Whitney Canada PW200 |
Wave turbine 1 × HD 1 × HD, 1 × AT |
2 | 570 | Canada | ? | ||
Rolls-Royce AE 1107 |
Wave turbine 14 × HD, 2 × HD, 2 × AT |
2 | 6710 | United States | ? | Originally developed by Allison Engine Company | |
Rolls-Royce AE 2100 |
Propeller turbine 14 × HD, 2 × HD, 2 × AT |
2 | 3410 | United States | ? | Originally developed by Allison Engine Company | |
Rolls Royce Darts |
Propeller turbine 2 × HD 3 × HD / AT |
1 | 2050 | United Kingdom | 1946 | ||
Rolls-Royce RB.50 Trent |
Propeller turbine 1 × HD 1 × HD, 1 × AT |
1 | 550 | United Kingdom |
|
1944 | First Rolls-Royce turboprop engine |
Rolls-Royce Tyne |
Propeller turbine 9 × HP, 6 × LP 1 × HP, 3 × LP / AT |
2 | 4500 | United Kingdom | 1955 | Before the introduction of the EPI TP400, most powerful turboprop engine in the western world | |
Solovyov D-25 |
Shaft turbine 9 × HD 1 × HD, 2 × FT |
1 | 4781 | Soviet Union | 1954 | ||
Turbomeca Arrius |
Wave turbine 1 × HD 1 × HD, 1 × AT |
2 | 530 | France | 1981 | ||
Turbomeca Artouste |
Wave turbine 1 × HD 3 × HD / AT |
1 | 640 | France | 1947 | ||
Turbomeca Astazou |
Propeller turbine Shaft turbine 2 × HD 3 × HD / AT |
1 | 480 | France | 1957 | Information for Astazou II | |
Turbomeca Makila |
Wave turbine 4 × HD, 2 × HD, 2 × AT |
2 | 1236 | France | 1977 | ||
Turbomeca Turmo |
Propeller turbine Shaft turbine 2 × HD, 2 × HD, 2 × AT |
2 | 1200 | France | 1957 | Also used in the railcar SNCF Turbotrain and in the power car of the SNCF TGV 001 |
Jet engines
The jet engines listed were or are being built in a wide variety of variants and outputs. The information for compressor and turbine stages as well as the thrust refer to the most powerful version.
- "Type" column
- LP : low pressure compressor / turbine
- MD : medium pressure compressor / turbine
- HD : high pressure compressor / turbine
Engine | Type of compressor turbine |
waves | Max. Thrust (kN) | Country of origin | Application example | First run | Remarks |
---|---|---|---|---|---|---|---|
Armstrong Siddeley Sapphire |
Turbojet (+ afterburner ) 13 × HD 2 × HD |
1 | 55 | United Kingdom | 1948 | ||
Armstrong Siddeley Viper |
Turbojet 7 × HD 1 × HD |
1 | 17.8 | United Kingdom | 1951 | ||
Avro Canada Orenda |
Turbofan 1 × fan, 9 × HD |
2 | 27 | Canada | 1952 | ||
Awiadwigatel PS-90 |
Turbofan 1 × fan, 2 × LP, 13 × HP, 2 × HP, 4 × LP |
2 | 171 | Russia | 1992 | ||
BMW 003 |
Turbojet 7 × HD 1 × HD |
1 | 7.8 | German Empire | 1940 | First jet engine with an annular combustion chamber | |
CFM International CFM56 |
Turbofan 1 × fan, 3 × LP, 9 × HP 1 × HP, 4 × LP |
2 | 151 |
United States of France |
1974 | Development based on the General Electric F101 | |
CFM International LEAP |
Turbofan 1 × fan, 3 × LP, 7 × HP, 2 × HP, 4 × LP |
2 | 146 |
United States of France |
2013 | Further development of the CFM International CFM56 | |
de Havilland Ghost |
Turbojet 1 × HD 1 × HD |
1 | 22.9 | United Kingdom | 1944 | ||
de Havilland Goblin |
Turbojet 1 × HD 1 × HD |
1 | 16.7 | United Kingdom | 1942 | ||
Engine Alliance GP7200 |
Turbofan 1 × fan, 5 × LP, 9 × HP, 2 × HP, 6 × LP |
2 | 340 | United States | 2004 | ||
Eurojet EJ200 |
Turbofan + afterburner 1 × fan, 3 × HP, 5 × LP 1 × HP, 1 × LP |
2 | 108 |
United Kingdom Germany Italy Spain |
1991 | ||
General Electric CF34 / TF34 |
Turbofan 1 × fan, 3 × LP, 9 × HP 1 × HP, 4 × LP |
2 | 89 | United States | 1982 | ||
General Electric CF6 / TF39 |
Turbofan 1 × fan, 4 × LP, 14 × HP, 2 × HP, 5 × LP |
2 | 305 | United States | 1971 | ||
General Electric F101 |
Turbofan + afterburner 1 × fan, 3 × LP, 9 × HP 1 × HP, 2 × LP |
2 | 137 | United States | 1970 | ||
General Electric F110 |
Turbofan + afterburner 1 × fan, 3 × LP, 9 × HP 1 × HP, 2 × LP |
2 | 142 | United States | 1979 | ||
General Electric F118 |
Turbofan 1 × fan, 2 × LP, 9 × HP 1 × HP, 2 × LP |
2 | 84.5 | United States | 1979 | ||
General Electric GE90 |
Turbofan 1 × fan, 4 × LP, 9 × HP, 2 × HP, 6 × LP |
2 | 489 | United States | 1994 | The GE90-115B variant is the largest and most powerful jet engine in aviation history, with a thrust of 569 kN achieved during a load test. | |
General Electric GEnx |
Turbofan 1 × fan, 4 × LP, 10 × HP, 2 × HP, 7 × LP |
2 | 322 | United States | 2006 | ||
General Electric J79 |
Turbojet + afterburner 17 × HD 3 × HD |
1 | 79.6 | United States | 1955 | ||
Heinkel HeS 3 |
Turbojet 1 × HD 1 × HD |
1 | 4.4 | German Empire | 1937 | The world's first jet flight took place with this engine in a Heinkel He 178 . | |
International Aero Engines V2500 |
Turbofan 1 × fan, 4 × LP, 10 × HP, 2 × HP, 5 × LP |
2 | 146.8 |
United States Germany Japan ( United Kingdom ) ( Italy )
|
1987 | ||
Ivchenko Progress D-36 |
Turbofan 1 × fan, 6 × MD, 7 × HD 1 × HD, 1 × MD, 3 × LP |
3 | 63.75 | Soviet Union | 1971 | Originally also called Lotarjow D-36 | |
Ivchenko Progress D-436 |
Turbofan 1 × fan, 6 × MD, 7 × HD 1 × HD, 1 × MD, 3 × LP |
3 | 92 |
Soviet Union Russia |
1993 | ||
Junkers Jumo 004 |
Turbojet 8 × HD 1 × HD |
1 | 8.7 | German Empire | 1940 | The world's first jet engine ready for series production | |
Klimow RD-33 |
Turbofan + afterburner 4 × fan / LP, 9 × HP 1 × HP, 1 × LP |
2 | 81.3 | Soviet Union | 1974 | ||
Klimow WK-1 |
Turbojet (+ afterburner ) 1 × HD 1 × HD |
1 | 33.2 | Soviet Union | 1947 | Based on the Rolls-Royce Nene , built in series without a license agreement | |
Lyulka AL-21 |
Turbojet (+ afterburner ) 14 × HD 3 × HD |
1 | 110 | Soviet Union | ? | ||
Mikulin AM-3 |
Turbojet 1 × blower, 8 × HD 2 × HD |
1 | 91.6 | Soviet Union | ? | ||
Pirna 014 |
Turbojet 12 × HD 2 × HD |
1 | 32.3 | German Democratic Republic | 1959 | ||
Pratt & Whitney F135 |
Turbofan + afterburner 3 × fan / LP, 6 × HP 1 × HP, 2 × LP |
2 | 191 | United States | ? | Development based on the Pratt & Whitney F119 | |
Pratt & Whitney J57 |
Turbojet (+ afterburner ) 9 × LP, 7 × HP 1 × HP, 2 × LP |
2 | 80 | United States | 1952 | Increased performance through water injection | |
Pratt & Whitney J58 |
Turbojet + afterburner 9 × HD 2 × HD |
1 | 151.3 | United States | 1957 | Combination of turbojet and ramjet engine for speeds> Mach 3 | |
Pratt & Whitney JT3D / TF33 |
Turbofan 2 × fan, 6 × MD, 7 × HP 1 × HP, 3 × LP |
2 | 75.6 | United States | 1958 | Developed on the basis of the Pratt & Whitney J57 | |
Pratt & Whitney JT8D |
Turbofan 2 × fan, 6 × LP, 7 × HP 1 × HP, 2 × LP |
2 | 96.5 | United States | 1960 | Developed on the basis of the Pratt & Whitney J52 | |
Pratt & Whitney JT9D |
Turbofan 1 × fan, 3 × LP, 11 × HP, 2 × HP, 4 × LP |
2 | 249 | United States | 1966 | ||
Pratt & Whitney PW1000G |
Geared turbofan 1 × G-Fan, 3 × LP, 8 × HP, 2 × HP, 3 × LP |
2 | 147 | United States | 2008 | ||
Pratt & Whitney PW2000 / F117 |
Turbofan 1 × fan,? × ND,? × HD ? × HD,? × ND |
2 | 191 | United States | ? | ||
Pratt & Whitney PW4000 |
Turbofan 1 × fan, 7 × LP, 11 × HP, 2 × HP, 7 × LP |
2 | 440 | United States | 1984 | ||
Pratt & Whitney PW5000 / F119 |
Turbofan + afterburner 3 × fan / LP, 6 × HP 1 × HP, 1 × LP |
2 | 155 | United States | 1988 | ||
Pratt & Whitney PW6000 |
Turbofan 1 × fan, 4 × LP, 6 × HP 1 × HP, 3 × LP |
2 | 106 | United States | 2000 | ||
Rolls-Royce Avon |
Turbojet (+ afterburner ) 16 × HD 3 × HD |
1 | 73 | United Kingdom | 1946 | First jet engine from Rolls-Royce with axial compressor | |
Rolls-Royce BR700 |
Turbofan 1 × fan, 10 × HP, 2 × HP, 3 × LP |
2 | 95 | Germany | 1994 | Joint development by Rolls-Royce and BMW | |
Rolls-Royce Conway |
Turbofan 7 × Fan / LP, 9 × HP 1 × HP, 2 × LP |
2 | 97.8 | United Kingdom | 1952 | World's first turbofan used in aviation | |
Rolls-Royce Derwent |
Turbojet 1 × HD 1 × HD |
1 | 16 | United Kingdom | 1943 | Development based on the Rolls-Royce Welland | |
Rolls-Royce Nene |
Turbojet 1 × HD 1 × HD |
1 | 22.2 | United Kingdom | 1944 | Development based on the Rolls-Royce Welland | |
Rolls-Royce Pegasus |
Turbofan 3 × fan / LP, 8 × HP, 2 × HP, 2 × LP |
2 | 106 | United Kingdom | 1959 | Engine with thrust vector control by means of four swiveling nozzles | |
Rolls-Royce RB.183 Tay |
Turbofan 1 × fan, 3 × LP, 21 × HP, 2 × HP, 3 × LP |
2 | 67 | United Kingdom | 1984 | Development based on the Rolls-Royce Spey | |
Rolls-Royce RB.203 Trent |
Turbofan 1 × fan, 4 × MD, 5 × HD 1 × HD, 1 × MD, 2 × LP |
3 | 71.4 | United Kingdom | 1967 | ||
Rolls-Royce RB211 |
Turbofan 1 × fan, 7 × MD, 6 × HD 1 × HD, 2 × MD, 3 × LP |
3 | 270 | United Kingdom | 1969 | ||
Rolls-Royce RB211 Trent |
Turbofan 1 × fan, 8 × MD, 6 × HD 1 × HD, 2 × MD, 6 × LP |
3 | 423 | United Kingdom |
|
1990 | The Trent 800 version is the basis for the MT 30 marine gas turbine . |
Rolls-Royce RB.44 Tay |
Turbojet + afterburner 1 × HD 1 × HD |
1 | 27.8 | United Kingdom | ? | Development based on the Rolls-Royce Nene | |
Rolls-Royce Spey |
Turbofan (+ afterburner ) 5 × fan / LP, 12 × HP 2 × HP, 2 × LP |
2 | 120 | United Kingdom | 1964 | ||
Rolls-Royce Welland |
Turbojet 1 × HD 1 × HD |
1 | 7.7 | United Kingdom | 1942 | First series-produced jet engine from Rolls-Royce | |
Rolls-Royce / SNECMA Olympus 593 |
Turbojet + afterburner 7 × LP, 7 × HP 1 × HP, 1 × LP |
2 | 169.2 |
United Kingdom of France |
1965 | Developed on the basis of the Rolls-Royce Olympus | |
Rolls-Royce Turboméca Adour |
Turbofan (+ afterburner ) 2 × fan / LP, 5 × HP 1 × HP, 1 × LP |
2 | 37.5 |
United Kingdom of France |
1968 | ||
Saturn AL-31 |
Turbofan + afterburner 4 × fan / LP, 9 × HP 1 × HP, 1 × LP |
2 | 144.5 | Soviet Union | ? | ||
Saturn AL-55 |
Turbofan 3 × fan / LP, 5 × HP 1 × HP, 1 × LP |
2 | 17.3 | Russia | 1999 | ||
SNECMA Atar |
Turbojet + afterburner 9 × HD 2 × HD |
1 | 70.6 | France | 1948 | Developed on the basis of the BMW 018 | |
SNECMA-Turbomeca Larzac |
Turbofan 2 × Fan / LP, 4 × HP 1 × HP, 1 × LP |
2 | 14.12 | France | 1969 | ||
Solovyov D-30 |
Turbofan (+ afterburner ) 3 × fan / LP, 11 × HP 2 × HP, 4 × LP |
2 | 152.1 | Soviet Union | ? | ||
Tumanski RD-9 |
Turbojet (+ afterburner ) 9 × HD 2 × HD |
1 | 31.9 | Soviet Union | 1953 | Developed on the basis of the Mikulin AM-3 | |
Turbo-Union RB199 |
Turbofan + afterburner 3 × Fan / LP, 3 × MD, 6 × HP 1 × HP, 1 × MD, 2 × LP |
3 | 74.3 |
United Kingdom Germany Italy |
1972 | ||
Westinghouse J40 |
Turbojet (+ afterburner ) 10 × HD 1 × HD |
1 | 48.5 | United States | 1948 | Development due to techn. Problems ceased in 1955, no series production |
literature
- Bill Gunston: Lexicon of the aircraft engines. Motorbuch Verlag, 1991, ISBN 3-1301-4229-0 .
- Kyrill von Gersdorff, Kurt Grasmann: aircraft engines and jet engines. Bernard & Graefe Verlag, 1981, ISBN 3-7637-5272-2 .
Web links
Commons : Aircraft engine imagery by manufacturer - collection of images, videos and audio files
Individual evidence
- ↑ Limbach aircraft engines: aircraft engines from 56 kW to 75 kW. Retrieved July 3, 2015 .
- ↑ Limbach aircraft engines: aircraft engines from 76 kW to 125 kW. Retrieved July 3, 2015 .
- ^ Avco Corp .: Lycoming 235 Series. Retrieved July 3, 2015 .
- ^ Avco Corp .: Lycoming 320 Series. Retrieved July 3, 2015 .
- ^ Avco Corp .: Lycoming 360 Series. Retrieved July 3, 2015 .
- ^ Avco Corp .: Lycoming 540 Series. Retrieved July 3, 2015 .
- ^ Avco Corp .: Lycoming 580 Series. Retrieved July 3, 2015 .
- ^ Avco Corp .: Lycoming 720 Series. Retrieved July 3, 2015 .
- ↑ a b c d e f g h i j k Pratt & Whitney: Classic Engines. Retrieved July 3, 2015 .
- ↑ a b c Michael Zoche drive technology: zoche aero-diesels specifications. Retrieved July 3, 2015 .
- ^ Europrop International: The TP400-D6. (No longer available online.) Archived from the original on May 14, 2010 ; Retrieved July 3, 2015 . Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice.
- ^ Smithsonian National Air and Space Museum: General Electric T31 (TG-100) Turboprop Engine. Retrieved July 3, 2015 .
- ↑ General Electric: T58 Turboshaft Engines. (No longer available online.) Archived from the original on March 26, 2015 ; Retrieved July 3, 2015 . Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice.
- ↑ General Electric: T64 Turboshaft / Turboprop Engines. (No longer available online.) Archived from the original on March 27, 2015 ; Retrieved July 3, 2015 . Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice.
- ↑ General Electric: T700-701D Turboshaft / Turboprop Engines. (No longer available online.) Formerly in the original ; Retrieved July 5, 2015 . ( Page no longer available , search in web archives ) Info: The link was automatically marked as defective. Please check the link according to the instructions and then remove this notice.
- ↑ SE Ivchenko Progress: D-136, D-136 Series 1 gas turbine turboshaft Aero Engine. Retrieved July 7, 2015 .
- ^ JSC "Klimov": TV3-117. Retrieved July 3, 2015 .
- ^ Rolls-Royce: UAV. (No longer available online.) Formerly in the original ; Retrieved July 9, 2015 . ( Page no longer available , search in web archives ) Info: The link was automatically marked as defective. Please check the link according to the instructions and then remove this notice.
- ↑ MTU Turbomeca Rolls-Royce GmbH: mtr390. Retrieved July 7, 2015 .
- ^ A b Rolls-Royce: Tactical Aircraft. (No longer available online.) Formerly in the original ; Retrieved July 6, 2015 . ( Page no longer available , search in web archives ) Info: The link was automatically marked as defective. Please check the link according to the instructions and then remove this notice.
- ^ Turbomeca: Arrius. (No longer available online.) Archived from the original on June 17, 2015 ; Retrieved July 6, 2015 . Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice.
- ↑ Turbomeca: Makila. (No longer available online.) Archived from the original on June 17, 2015 ; Retrieved July 6, 2015 . Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice.
- ↑ a b CFM International: The CFM56 Turbofan Engine Product Line. Retrieved July 8, 2015 .
- ↑ General Electric: The CF34 Engine. Retrieved July 12, 2015 .
- ^ General Electric: The CF6 Engine. Retrieved July 8, 2015 .
- ↑ General Electric: The F110 Engine. Retrieved July 8, 2015 .
- ↑ General Electric: The GE90 Engine Family. Retrieved July 8, 2015 .
- ↑ General Electric: The GEn × Engine. Retrieved July 8, 2015 .
- ↑ International Aero Engines: Engine Facts. (No longer available online.) Archived from the original on March 14, 2016 ; Retrieved July 9, 2015 . Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice.
- ↑ a b c d MTU Aero Engines: Narrowbody and Regional Jets. Retrieved July 7, 2015 .
- ^ A b c d e f Pratt & Whitney: Commercial Engines. Retrieved July 7, 2015 .
- ^ Pratt & Whitney: Military Engines. Retrieved July 7, 2015 .
- ^ A b Rolls-Royce: Small Aircraft Engines. Retrieved July 9, 2015 .
- ^ A b Rolls-Royce: Civil Large Engines. Retrieved July 9, 2015 .