Examples of 'aircraft turbojet' in a sentence
Meaning of "aircraft turbojet"
Aircraft turbojet: An air-breathing jet engine used in aircraft propulsion. It works by compressing air, mixing it with fuel, igniting the mixture, and expelling the hot exhaust gases to produce thrust
How to use "aircraft turbojet" in a sentence
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Advanced
aircraft turbojet
Noise reduction assembly for aircraft turbojet.
Aircraft turbojet engines generate significant noise pollution.
Test bench for an aircraft turbojet engine is provided.
The invention relates to thrust reversers for aircraft turbojet engines.
Assembly for an aircraft turbojet engine comprising a thrust reversal cowl.
The invention applies in particular to aircraft turbojet engines.
An aircraft turbojet comprising a fan according to claim 5.
The invention preferably applies to an aircraft turbojet engine.
An aircraft turbojet comprising a structure according to claim 1.
The following example relates more particularly to an aircraft turbojet engine.
Intermediate casing hub for an aircraft turbojet engine including a composite outlet pipe.
The present invention relates to an assembly for an aircraft turbojet engine.
Nacelle for an aircraft turbojet engine comprising,.
The present application also relates to a compressor and an aircraft turbojet.
Structure for an aircraft turbojet comprising,.
See also
The invention notably relates to an actuation system for an aircraft turbojet engine.
An aircraft turbojet engine comprising an afterbody as claimed in claim 1.
System for deicing the nose cone of an aircraft turbojet with oil.
An aircraft turbojet engine nacelle, comprising at least one arrangement according to claim 1.
Composite materials are being used increasingly frequently in the field of aircraft turbojet engines.
Thrust reverser for an aircraft turbojet engine nacelle comprising,.
The disclosed embodiments relate to a nacelle cowling for an aircraft turbojet engine.
Nacelle of an aircraft turbojet engine equipped with a thrust reverser according to claim 1.
The present disclosure relates to gas ejection cones for aircraft turbojet engines.
An aircraft turbojet low-pressure compressor includes a sealing device for a turbine engine.
The present disclosure relates to a cascade thrust reverser for aircraft turbojet engine.
An aircraft turbojet fan wherein said aircraft turbojet fan comprises a rotor including,.
The invention concerns gas turbines and in particular gas turbines of aircraft turbojet engines.
Thrust reverser for a nacelle of an aircraft turbojet engine, the thrust reverser comprising,.
The turbine engine 4 in this case is an aircraft turbojet.
In the case of aircraft turbojet engines, the compressor receives the intake air flow.
The present invention relates to a maintenance trolley for an aircraft turbojet engine nacelle air intake.
Aircraft turbojet engine, comprising an intermediate casing according to claim 12.
FIELD The invention concerns tests on aircraft turbojet engines.
An aircraft turbojet engine generally comprises a fan, a compressor, a combustion chamber, and a turbine.
Thrust reverser for a nacelle of an aircraft turbojet engine comprising,.
An aircraft turbojet engine 15 with an ejector 16 may be used as a low-pressure source.
The present invention relates to a fan of a turbomachine, such as an aircraft turbojet.
Moreover, another subject of the invention is an aircraft turbojet engine comprising such an afterbody.
FIG . 1 illustrates schematically the upstream section, partly shown, of a nacelle 1 for an aircraft turbojet engine.
The invention in particular applies to aircraft turbojet engines, preferably bypass and twin-spool turbojet engines.
The invention relates to the field of turbine engines, in particular to aircraft turbojet engines.
Maintenance trolley for an air intake of an aircraft turbojet engine nacelle, comprising,.
To accomplish this, one object of the invention is a structure for an aircraft turbojet including,.
Hub of intermediate casing for aircraft turbojet engine, comprising,.
The present invention relates to the field of multi-spool and multi-flow aircraft turbojet engines.
Noise reduction sandwich panel, notably for aircraft turbojet engine.
Said rectifier 2 forms part of a turbomachine compressor 3, in particular an aircraft turbojet engine.
More particularly, a ground test bench for an aircraft turbojet engine . BACKGROUND.
FIGS . 1 and 2, previously described, represent a fan of an aircraft turbojet known from the prior art ;.
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