Examples of 'turbojet engines' in a sentence
Meaning of "turbojet engines"
Turbojet engines are a type of aircraft propulsion system that operate by drawing in air, compressing it, and then combusting it with fuel to generate forward thrust. They use a continuous flow of intake air and are known for their high-speed capabilities and relatively simple design
How to use "turbojet engines" in a sentence
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turbojet engines
Turbojet engines generate significant noise pollution.
A turbojet train is a train powered by turbojet engines.
The aircraft turbojet engines generate significant noise pollution.
The invention applies in particular to aircraft turbojet engines.
An aircraft is moved by several turbojet engines each housed in a nacelle.
The present invention relates to the field of turbojet engines.
Most supersonic turbojet engines are equipped with an afterburner arrangement.
It will be equipped with turbojet engines.
Turbojet engines have tubular compartments in which different pressures prevail.
An airplane is propelled by a number of turbojet engines each housed in a nacelle.
It is intended for the control of an emergency feed regulator of turbojet engines.
An aircraft is driven by several turbojet engines each housed in a nacelle.
The invention relates to thrust reversers for aircraft turbojet engines.
The company also produces turbojet engines for aircraft and missiles.
The field of the present invention is that of bypass turbojet engines.
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Double flow turbojet engines constitute one propulsion engine type for aircraft.
The invention preferably applies to turbojet engines and turboprop engines.
It is already known to use catalytic ignition devices in the art of turbojet engines.
An airplane is propelled by one or more turbojet engines each housed in a nacelle.
Composite materials are being used increasingly frequently in the field of aircraft turbojet engines.
Variable section exhaust nozzles are used in turbojet engines whether with or without reheat.
New lightweight turbojet engines that were being developed enabled the concept to take shape.
Military fighters and fast business jets use turbojet engines.
Early jet aircraft used turbojet engines which were relatively inefficient for subsonic flight.
The present disclosure relates to gas ejection cones for aircraft turbojet engines.
The power plant consists of four turbojet engines suspended on pylons under the wing.
The power of the starter is transmitted to the utility shaft of the turbojet engines.
Rotating stall is a phenomenon which affects all turbojet engines under various operating conditions.
The arm can also be calibrated for various applications or for different turbojet engines.
Father of Soviet turbojet engines can be called AA bassinet.
The invention concerns gas turbines and in particular gas turbines of aircraft turbojet engines.
Other comparable turbojet engines are developed at the same time including the Canadian Orenda Iroquois.
Method and device for reversing the thrust of very high bypass ratio turbojet engines.
Turbojet engines have a high fuel consumption, and afterburning even more so.
Each one is equipped with VTOL capability and five turbojet engines.
In order to optimize their thrust, turbojet engines work with several annular airflows.
Field The disclosed embodiments relate to the field of aircraft propelled by turbojet engines.
Inter-shaft bearing for multibody turbojet engines with damping by a film of oil.
FIELD The invention concerns tests on aircraft turbojet engines.
Aircraft, notably jet aircraft, have turbojet engines which are significant sources of noise emissions.
The combustor, or burner, was primitive by the standards of modern turbojet engines.
The combustion chambers of conventional turbojet engines typically operate at sub-stoichiometric fuel ratios.
As a result, turbo-compound aero engines were soon supplanted by turboprop and turbojet engines.
Yet, such an architecture is unsuitable for turbojet engines with high bypass ratio.
The invention relates to the field of turbine engines, in particular to aircraft turbojet engines.
Even four turbojet engines could not provide the required power during take-off.
The present invention relates to the field of turbomachines, particularly bypass turbojet engines.
Current turbojet engines generate more and more heat, particularly for the following reasons,.
The invention applies to all types of aircraft turbomachines, in particular turbojet engines and turbochargers.
The term " jet engine " includes turbojet engines and turbofan engines, for example.
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Examples of using Turbojet
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Turbojet and turbofan engines including turbocompound
Single baffle turbojet engine thrust reverser
Turbojet engines generate significant noise pollution
Examples of using Engines
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The engines can be investigated in two modes
For positiveignition engines fuelled with petrol
The engines are down but can be restarted
