• A combustor is a component or area of a gas turbine, ramjet, or scramjet engine where combustion takes place. It is also known as a burner, burner can...
    32 KB (4,515 words) - 03:29, 4 November 2024
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    Ramjet (section Combustor)
    the combustor raises the air temperature by burning fuel. This takes place with a small pressure loss. The air velocity entering the combustor has to...
    37 KB (4,929 words) - 12:26, 9 November 2024
  • Thumbnail for Fluidized bed combustion
    gas in addition to the vitiated air from the PFB combustor. This mixture is burned in a topping combustor to provide higher inlet temperatures for greater...
    8 KB (1,093 words) - 13:53, 5 August 2024
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    (GE) of the United States. GE produces the high-pressure compressor, combustor, and high-pressure turbine, Safran manufactures the fan, gearbox, exhaust...
    86 KB (8,721 words) - 17:42, 10 November 2024
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    engine management developments. William C. Pfefferle developed a catalytic combustor for gas turbines in the early 1970s, allowing combustion without significant...
    56 KB (6,707 words) - 19:35, 6 November 2024
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    mixed with the compressed air and burns in the combustor. The combustion products leave the combustor and expand through the turbine where power is extracted...
    28 KB (3,537 words) - 01:57, 30 October 2024
  • Thumbnail for General Electric GE9X
    third-generation, twin-annular pre-swirl (TAPS) combustor instead of the previous dual annular combustor. Able to endure hotter temperatures, ceramic matrix...
    26 KB (2,619 words) - 19:46, 7 November 2024
  • combustor, can annular combustors have discrete combustion zones contained in separate liners with their own fuel injectors. Unlike the can combustor...
    9 KB (997 words) - 17:47, 3 June 2024
  • Thumbnail for Air turborocket
    to combust, the turboramjet combustor may use hydrogen and oxygen, carried on the aircraft, as its fuel for the combustor. The air compressed by the compressor...
    9 KB (1,175 words) - 02:52, 25 August 2024
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    propeller. A turboprop consists of an intake, reduction gearbox, compressor, combustor, turbine, and a propelling nozzle. Air enters the intake and is compressed...
    34 KB (3,061 words) - 01:23, 12 October 2024
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    and combat. The afterburning process injects additional fuel into a combustor in the jet pipe behind (i.e., "after") the turbine, "reheating" the exhaust...
    20 KB (2,619 words) - 23:59, 21 August 2024
  • Thumbnail for Williams FJ44
    high pressure (HP) turbine. The combustor is an impingement cooled annular design. Fuel is delivered to the combustor through an unusual rotating fuel...
    11 KB (783 words) - 16:12, 20 October 2024
  • Thumbnail for GE Aerospace
    designated the X101). The GE1 was a basic gas generator (compressor, combustor and turbine) onto which a variety of components such as fans, afterburners...
    30 KB (2,586 words) - 15:48, 4 November 2024
  • Thumbnail for Components of jet engines
    diffuser slows down the compressor delivery air to reduce flow losses in the combustor. Slower air is also required to help stabilize the combustion flame and...
    46 KB (6,760 words) - 01:48, 10 October 2024
  • Thumbnail for Volcanic ash and aviation safety
    creates a ceramic mass that sticks to turbine blades, fuel nozzles, and combustors, which can quickly lead to total engine failure. Ash can also contaminate...
    14 KB (1,650 words) - 17:58, 6 November 2024
  • Thumbnail for Combustion instability
    region to avoid in the operation of the combustor. This graphical representation of a hypothetical combustor allows to group three methods to prevent...
    17 KB (2,133 words) - 10:48, 16 August 2024
  • hollow titanium like those of Rolls-Royce Plc., and its single annular combustor uses 3D printed fuel nozzles. A model of the CJ-1000Al was exhibited at...
    10 KB (1,000 words) - 21:20, 16 June 2024
  • Thumbnail for JEA Northside Generating Station
    2, formerly the largest circulating fluidized-bed combustors, (CFBs), in the world. These combustors, completed in 2002 and rated at 297.5 megawatts each...
    15 KB (1,564 words) - 13:55, 5 August 2024
  • radiative emissions via photovoltaic and thermionic generators. Heterogeneous combustors may be utilized for small-scale heating purposes, and as oxidizers of...
    6 KB (708 words) - 13:11, 28 May 2021
  • offshore. A DLE combustor uses the principle of lean premixed combustion, and is similar to the SAC combustor (Single Annular Combustor) with some exceptions...
    12 KB (1,267 words) - 02:50, 15 February 2024
  • engine geometry is simple and similar to scramjet, varying only in the combustor design. The engine includes a supersonic inlet followed by a combustion...
    6 KB (722 words) - 06:18, 5 November 2024
  • Thumbnail for Pratt & Whitney PW1000G
    military ATEGG program's low aspect-ratio airfoils. A floatwall/TALON combustor was followed by a single stage HP turbine and a counter rotating 3-stage...
    74 KB (7,302 words) - 10:27, 19 September 2024
  • the combustor can be as high as approximately 30 MPa. The combustion feedstock consists of approximately 95% recycled CO2 by mass. The combustor provides...
    28 KB (1,632 words) - 08:05, 14 October 2024
  • HP compressor, while a 2-stage LP turbine drives the 3 stage fan. The combustor is annular. In 1998, the USAF's Lockheed U-2S fleet was fitted with a...
    4 KB (254 words) - 11:04, 16 October 2024
  • or other turbine engine due to the extinguishment of the flame in its combustor. The loss of flame can have a variety of causes, such as fuel starvation...
    4 KB (474 words) - 22:42, 1 March 2024
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    Relationship between Chlorine in Waste Streams and Dioxin Emissions from Waste Combustor Stacks (PDF). Vol. 36. New York, NY: American Society of Mechanical Engineers...
    56 KB (5,174 words) - 22:28, 13 October 2024
  • Thumbnail for Pratt & Whitney Canada PW300
    high-pressure compressor, driven by a two-stage high-pressure turbine. An annular combustor is used. There is no forced mixing before the bypass and core streams...
    9 KB (828 words) - 16:59, 13 August 2024
  • with care-free throttle handling without compressor stall or surge or combustor flame-out. There must be no unacceptable loss of power or handling deterioration...
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  • ratio. As the surface to volume ratio increases heat loss to walls of combustor increases which leads to flame quenching. The development of miniaturized...
    8 KB (993 words) - 04:44, 28 December 2023
  • afterburning turbofan Length: Diameter: Dry weight: Compressor: axial Combustors: annular Maximum thrust: 10,000 kgf (98 kN; 22,046 lbf) with afterburner...
    3 KB (236 words) - 10:54, 15 May 2024