Examples of 'aeroengine' in a sentence
Meaning of "aeroengine"
aeroengine (noun) - An aeroengine is a type of engine specifically designed for use in aircraft, such as airplanes or helicopters
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- Alternative spelling of aero engine
How to use "aeroengine" in a sentence
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aeroengine
Aeroengine fitted with heat exchanger means.
The part may constitute an aeroengine casing.
Russian aeroengine manufacturers.
Standardizing data used for monitoring an aeroengine.
The turbomachine is advantageously an aeroengine and more particularly a turbojet.
System for real time simulation of the environment of an aeroengine.
The invention also provides an aeroengine including a plurality of blades of the invention.
The present invention relates to the field of monitoring an aeroengine.
The present invention relates to an aeroengine fitted with heat exchanger means.
An aeroengine comprising a power supply circuit according to claim 1.
Identifying failures in an aeroengine.
The invention also provides an aeroengine including a casing structure as specified above.
The project includes the transfer of technology from a leading aeroengine manufacturer.
The invention also provides an aeroengine afterbody including an exhaust cone of the invention.
The invention also provides an aircraft including at least one aeroengine of the invention.
See also
The invention also provides an aeroengine including a system in accordance with the invention.
In particular, the part may constitute an aeroengine blade.
Turboprop comprising an aeroengine casing according to claim 7.
An aeroengine including the casing structure according to claim 1.
The invention also provides a turboprop including an aeroengine casing of the invention.
An aeroengine comprising a fan according claim 1.
The invention also provides a gas turbine aeroengine including such a fan retention casing.
An aeroengine having a plurality of aircraft propeller blades according to claim 1.
An aircraft including at least one aeroengine according to claim 3.
An aeroengine comprising a gas turbine and an electronic unit according to claim 9.
An aircraft fitted with at least one aeroengine according to claim 7.
Gas turbine aeroengine having a gas turbine casing according to claim 1.
In an aspect of the invention, the part constitutes an aeroengine casing.
Gas turbine aeroengine including a fan retention casing according to claim 7.
Part according to claim 5, constituting an afterbody part of a gas turbine aeroengine.
The invention also relates to an aeroengine including an after-body assembly of the invention.
By way of example, the part may be a blade or a casing for an aeroengine.
Thus, aeroengine monitoring may take place identically, regardless of external acquisition conditions.
In particular, the invention relates to detecting anomalies in control means of the aeroengine.
Template, Russian aeroengine manufacturers.
Advantageously, said time-series measurements are collected during normal operation of said aeroengine.
To achieve this object, the aeroengine of the invention comprises,.
In particular, the invention relates to standardizing data used for monitoring the aeroengine.
The aeroengine including the after-body assembly according to claim 1.
Method according to claim 1, wherein the part constitutes an afterbody part of a gas turbine aeroengine.
An aeroengine comprising,.
Sensors for collecting time-series measurements from said aeroengine and its environment ;.
To achieve this object, the aeroengine of the invention comprises, primary air circuit ;.
The invention relates to operating safety for electrically-driven accessories of a turboengine, in particular an aeroengine.
FIG . 2 shows a system including a fan 11 for an aeroengine in a second embodiment of the invention.
The above-described method is particularly suitable for making fan casings for a gas turbine aeroengine.
Leitz Reference BX is purpose-built for aeroengine blade and 3D glass inspection, combining optical and….
Abstract, Soot has become an important issue in the design of aeroengine combustors.
Charlie Taylor built an inline aeroengine for the Wright Flyer 12 horsepower.
Step E 5 relates to selecting reference signatures corresponding to listed failures of the aeroengine.
