The engine pressure ratio (EPR) is the total pressure ratio across a jet engine, measured as the ratio of the total pressure at the exit of the propelling...
2 KB (204 words) - 17:01, 9 June 2024
turbine engine. The terms compression ratio and pressure ratio are used interchangeably. Overall compression ratio also means the overall cycle pressure ratio...
6 KB (795 words) - 20:09, 7 July 2024
Turbofan (redirect from High-bypass turbofan engine)
of the engine by increasing its pressure ratio or turbine temperature to achieve better combustion causes a corresponding increase in pressure and temperature...
92 KB (11,155 words) - 16:00, 24 September 2024
Pressure ratio may refer to: Compression ratio, for piston engines Overall pressure ratio, for gas turbine engines Pressure ratio, the compression ratio...
211 bytes (58 words) - 16:02, 29 November 2020
described in terms of BPR, which together with engine pressure ratio, turbine inlet temperature and fan pressure ratio are important design parameters. In addition...
28 KB (2,122 words) - 14:40, 26 September 2024
The compression ratio is the ratio between the volume of the cylinder and combustion chamber in an internal combustion engine at their maximum and minimum...
13 KB (1,631 words) - 16:33, 26 September 2024
Afterburner (redirect from Afterburner (engine))
it pays to select an engine cycle with a high specific thrust (i.e. high fan pressure ratio/low bypass ratio). The resulting engine is relatively fuel efficient...
20 KB (2,619 words) - 23:59, 21 August 2024
high pressure ratios (e.g. 10:1), impeller stress considerations limit the pressure ratio that can be employed in high overall pressure ratio engine cycles...
46 KB (6,646 words) - 00:53, 1 October 2024
Compressor stall (redirect from Engine surge)
can occur during the operation of the engine to lower the surge pressure ratio or raise the operating pressure ratio. When the two coincide there is no longer...
16 KB (2,212 words) - 00:04, 19 June 2024
A rotating detonation engine (RDE) uses a form of pressure gain combustion, where one or more detonations continuously travel around an annular channel...
19 KB (1,968 words) - 07:25, 18 July 2024
exit area is the correct value for the nozzle pressure ratio (npr). Since the npr changes with engine thrust setting and flight speed this is seldom...
61 KB (7,824 words) - 03:53, 23 September 2024
Ramjet (redirect from Ramjet engine)
bypass engine can be described as transitioning from turbo to ramjet mode if it can attain a flight speed at which the engine pressure ratio (epr) has...
36 KB (4,882 words) - 14:08, 13 September 2024
Ambient air pressure also imparts a small pressure against the exhaust, helping to keep it moving in the "right" direction as it exits the engine. As the...
23 KB (2,543 words) - 09:24, 27 September 2024
Pulsejet (redirect from Pulse jet engine)
Germany's V-1 flying bomb. Pulsejet engines are a lightweight form of jet propulsion, but usually have a poor compression ratio, and hence give a low specific...
27 KB (3,662 words) - 19:08, 24 August 2024
and fuel consumption) for a pilot is displayed in the cockpit as engine pressure ratio (EPR) and exhaust gas temperature (EGT) or fan speed (N1) and EGT...
118 KB (16,905 words) - 16:41, 22 September 2024
expansion-ratio. The large bell- or cone-shaped nozzle extension beyond the throat gives the rocket engine its characteristic shape. The exit static pressure of...
100 KB (11,709 words) - 16:03, 2 October 2024
Turbojet (redirect from Turbojet engine)
powerplant efficiency (the engine efficiency is increased by the ram pressure rise which adds to the compressor pressure rise, the higher aircraft speed...
28 KB (3,494 words) - 20:14, 30 September 2024
The Coffman engine starter (also known as a "shotgun starter") was a starting system used on many piston engines in aircraft and armored vehicles of the...
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disadvantage. At high overall pressure ratios, the compression system is usually split into two units; a low-pressure (LP) compressor mounted on one...
6 KB (756 words) - 07:12, 25 October 2023
mode the engine acts more like a 'leaky' turbojet (e.g. the F404). In the mixed-flow turbofan with ejector concept, a low bypass ratio engine is mounted...
8 KB (1,053 words) - 06:52, 24 May 2024
Turboshaft (redirect from Turboshaft engine)
multiple-ratio transmissions and clutches. An unusual example of the turboshaft principle is the Pratt & Whitney F135-PW-600 turbofan engine for the STOVL...
7 KB (794 words) - 10:53, 24 October 2023
Rolls-Royce/Snecma Olympus 593 (redirect from Pressure recovery)
included thrust-specific fuel consumption (TSFC or simply SFC), engine pressure ratio, size and weight, and turbine entry temperature. Initial studies...
27 KB (3,080 words) - 04:58, 4 May 2024
an overall engine efficiency of 48.2%, for a burner temperature of 1,700 K (1,430 °C), an overall pressure ratio of 38 and a peak pressure of 30 MPa (300 bar)...
43 KB (5,236 words) - 14:13, 25 September 2024
Air-start system (section Diesel engines)
start large diesel engines and gas turbines. Compared to a gasoline (petrol) engine, a diesel engine has a very high compression ratio, an essential design...
9 KB (1,224 words) - 04:34, 29 February 2024
expansion ratio. For any heat engine the work which can be extracted from it is proportional to the difference between the starting pressure and the ending...
28 KB (3,874 words) - 15:02, 1 October 2024
The pressure-fed engine is a class of rocket engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and...
6 KB (547 words) - 09:20, 27 September 2024
steam engine is a heat engine that performs mechanical work using steam as its working fluid. The steam engine uses the force produced by steam pressure to...
78 KB (9,749 words) - 11:05, 17 September 2024
piston engine gas starting system, used on the Bristol Jupiter engine in 1922. A system used in early Rolls-Royce Kestrel engines ducted high-pressure air...
19 KB (2,353 words) - 21:20, 30 September 2024
Axial compressor (section Axial-flow jet engines)
bleed). Modern jet engines use a series of compressors, running at different speeds; to supply air at around 40:1 pressure ratio for combustion with...
33 KB (5,121 words) - 09:24, 9 July 2024
valve mechanism of a conventional engine, which may reduce mechanical complexity and enable an increased compression ratio by eliminating hotspots that would...
25 KB (3,207 words) - 23:15, 29 September 2024