Information om | Engelska ordet COMBUSTOR

Exempel på hur man kan använda COMBUSTOR i en mening

• A turboprop consists of an intake, reduction gearbox, compressor, combustor, turbine, and a propelling nozzle.
• E family introduced new technologies such as the triple-shaft architecture, an annular combustor and a structurally integrated power-plant (nacelle).
• Furthermore, single-crystal alloys allows higher temperature capability and PW's Floatwall combustor liners improve durability and maintainability.
• GE produces the high-pressure compressor, combustor, and high-pressure turbine, Safran manufactures the fan, gearbox, exhaust and the low-pressure turbine, and some components are made by Avio of Italy and Honeywell from the US.
• The combustion chamber in gas turbines and jet engines (including ramjets and scramjets) is called the combustor.
• As a result of the temperature rise in the afterburner combustor, the gas is accelerated, firstly by the heat addition, known as Rayleigh flow, then by the nozzle to a higher exit velocity than that which occurs without the afterburner.
• As an RTM322 variant, the Aneto is a two spool turboshaft with a three stage axial compressor and a single stage centrifugal compressor turning at 36,300rpm, a reverse flow annular combustor, a two stage gas generator axial turbine and a two stage axial power turbine with a forward transmission shaft turning at 21,000rpm.
• The BR715 inspired combustor yields a longer life and lower emissions: 80% lower smoke and unburned hydrocarbons and 35% lower NOx than CAEP 6 limits.
• The initial workshare was as follows: Turbomeca produced the compressor, gearbox, accessories and control system, Rolls-Royce manufactured the power turbine stage, while MTU was responsible for the combustor, high-pressure turbine, along with the final assembly of the entire first batch of engines.
• The GE1 was a basic gas generator (compressor, combustor and turbine) onto which a variety of components such as fans, afterburners or other thrust vectoring devices could be added later.
• By the late 1990s, Volvo Aero's component range included fan cases, fan-compressor structures, compressor rotors, shafts, combustor structures, vanes, low-pressure turbine (LPT) cases, turbine structures, rocket nozzles, combustion chambers, and rocket engine turbines for both civilian and military purposes.
• The engine failure was later traced to an incorrectly repaired combustor, causing the turbine disc to shatter and puncture the wing fuel tanks.
• As the HP spool accelerates and the fuel:air mixture in the combustor lights up, at some point there is sufficient energy in the turbine gas stream to start to rotate the LP spool, which accelerates, albeit more sluggishly.
• CAS' core focus is the overhaul, repair, and modification of aircraft jet turbine engine components such as combustor, fuel nozzles, tube repair, and ducting, for various engines, namely: PW4000, PW2000, V2500, and CFM56.
• GE has several option packages for industrial LM6000s, including SPRINT (Spray Inter-Cooled Turbine), water injection (widely known as "NOx water"), STIG (Steam Injected Gas Turbine) technology and DLE (Dry Low Emissions) which utilizes a combustor with premixers to maximize combustion efficiency.
• A combustor is a component or area of a gas turbine, ramjet, or scramjet engine where combustion takes place.
• This initial version of the CF6 has a single-stage fan with one core booster stage, driven by a 5-stage LP (low pressure) turbine, turbocharging a 16-stage HP (high pressure) axial compressor driven by a 2-stage HP turbine; the combustor is annular; separate exhaust nozzles are used for the fan and core airflows.
• On jetliners, air is supplied to the ECS by being bled from a compressor stage of each gas turbine engine, upstream of the combustor.
• In aviation, a flameout (or flame-out) is the run-down of a jet engine or other turbine engine due to the extinguishment of the flame in its combustor.
• The engine featured an electronically controlled afterburner, a system that dumped additional fuel into the combustor pipe 'behind' the engine, reheating the exhaust and producing significantly more thrust, although with greatly reduced efficiency and high fuel burn rates.

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