Examples of 'turbofan engine' in a sentence

Meaning of "turbofan engine"

A turbofan engine is a type of aircraft engine that consists of a fan and a core engine. The fan provides most of the thrust and is powered by the core engine, which includes a gas turbine. Turbofan engines are commonly used in commercial and military aircraft due to their efficiency and quiet operation

How to use "turbofan engine" in a sentence

Basic
Advanced
turbofan engine
Turbofan engine with a floating pod.
The propulsion unit is a turbofan engine.
The turbofan engine comprises of a fan and a core engine.
The engine in this particular case is a turbofan engine.
Its powerful turbofan engine has the largest diameter of any commercial aircraft.
Thrust reverser for a turbofan engine.
Conventional diesel turbofan engine propulsion during high altitude and outside cities cruise.
Air inlet for a turbofan engine.
This engineering leads to additional costs and increases the mass of the turbofan engine.
The two shaft unmixed turbofan engine is one of several possible designs of a turbofan engine.
The turbomachine in question in this particular case is a turbofan engine.
The invention also relates to a turbofan engine nacelle including a thrust reverser according to the invention.
The turbo machine in this particular case is a turbofan engine.
Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing.
The fan is the first component of the turbofan engine.

See also

Various lightweight and low cost turbofan engine configurations have been proposed in the prior art.
The invention relates to a thrust reverser for a turbofan engine nacelle.
Nacelle of a turbofan engine comprising a thrust reverser device according to claim 1.
Sealing device between an air inlet and a fan frame of a turbofan engine.
The inlet air that passes through a turbofan engine is usually divided into two separate.
Improvements in gear performance are mainly driven by continuous demands of geared turbofan engine operators.
The invention also relates to the front-fan turbofan engine comprising a fan rotor thus defined.
The description below relates to an example installation for a typical single shaft turbofan engine.
Fig . 7b shows washing of the core engine of a turbofan engine according to the invention.
The invention relates to a chevron-type primary exhaust nozzle for an aircraft turbofan engine.
High-bypass turbofan engine.
More preferentially, the invention can be applied to a twin-spool turbofan engine.
Turbofan engine nacelle, comprising a thrust reverser according claim 1.
In this exemplary case, it is a turbofan engine.
Turbofan engine comprising a nacelle with an air inlet-according to claim 1.
In this specific case, it is a turbofan engine.
Turbofan engine according to claim 12, wherein the links have a regulatable length.
The fan is therefore no longer expelled from the turbofan engine 1.
The geared turbofan engine 20 enables relatively high bypass flow ratios.
Air-to-oil heat exchangers are an integral feature of advanced turbofan engine designs.
Turbofan engine according to claim 2, wherein the flexible member is a segmented, circular ring.
Fig.2 shows an example of a prior art manifold when installed in a turbofan engine inlet.
Primary exhaust nozzle for a turbofan engine of the double, separated air-flow type for aircraft comprising,.
Another portion of the air is channelled around the turbofan engine as ' bypass ' air.
Known turbofan engine 10 with its various major components is schematically illustrated in FIG . 1.
Then the stubby wings and control surfaces are deployed, and the turbofan engine takes over.
The JT8D is an axial-flow front turbofan engine incorporating dual-spool design.
The joint venture was formed to build and support the CFM56 series of turbofan engine.
A cross section view of a two shaft turbofan engine is shown in Fig.1.
NSM utilizes a rocket booster for initial launch, after which it transits to a turbofan engine.
The TF39 was the first high-bypass turbofan engine to enter production.
During development, Saab had opted to power the type using a single large turbofan engine.
Its utilization in CFM LEAP high-bypass turbofan engine has reduced fuel consumption by 16 %.
A separate partnership was formed between Rolls-Royce and Turbomeca to develop the Adour afterburning turbofan engine.
A cross section view of a single shaft turbofan engine is shown in Fig.1.

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