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Protective cover for turbofan engine of aeroplane

A turbofan and protective cover technology, applied in the field of protective cover, can solve problems such as abnormal engine operation, engine damage, and stop operation

Inactive Publication Date: 2006-12-20
韩英
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

From the perspective of aircraft structure, the front protection of the engine is the weakest, and the impactor can directly enter the engine, damage the components of the engine, and cause the engine to run abnormally or stop running.

Method used

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  • Protective cover for turbofan engine of aeroplane
  • Protective cover for turbofan engine of aeroplane
  • Protective cover for turbofan engine of aeroplane

Examples

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Embodiment Construction

[0020] see first figure 1 , figure 2 , image 3 , the protective cover used to protect the safety of the aircraft turbofan engine, it includes a casing (1) installed on the front end of the engine (A) to protect the safety of the engine, and a casing (1) arranged on the top of the casing (1) to conduct air The air guide hole (2), a fixing belt (3) arranged at the end of the housing (1) to fix the housing (1) and a bolt hole (4) arranged on the fixing belt (3), are arranged in the housing It is connected with the inner wall of the shell and is radial, and is used to support the support frame (5) of the shell (see Figure 4 ). The air guide holes (2) include air guide holes (2A) and (2B).

[0021] The shell (1): a. It is made of metal alloy material or carbon fiber composite material with light material and high mechanical strength.

[0022] B, housing (1) profile front end is garden arc, and the middle part is garden cone, and the end is garden cylinder.

[0023] c, the ...

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Abstract

The invention relates to a protective cover for protecting the worm fan engine of plane, which comprises a frame (1) at the front of engine (A), a gas hole (2) on the frame (1) to guide air, a fixing belt (3) at the end of frame 91) to fix the frame (1), a bolt hole on the fixing belt (3), and a support (5) inside the frame (1) to connect the inner wall and support the frame, wherein there are two gas holes (2A, 2B). The frame (1) can reduce the air resistance and improve the anti-impact ability; the gas hole (2) can supply air to the engine (A); the fixing belt (3) and bolt hole (4) can fix and connect the protective cover and engine (A); and the support (5) can strengthen the frame.

Description

Technical field: [0001] The invention relates to a protective cover for protecting the safety of an aircraft turbofan engine, which comprises a casing installed on the front end of the engine to block impact objects, an air guide hole arranged on the casing to conduct air, and a casing arranged on the casing The end of the body is used to connect the fixing belt with the engine, the bolt hole is arranged on the fixing belt, and the support frame used to support the casing is arranged in the casing. Background technique: [0002] The engine is an important part of the aircraft, it provides flight power for the aircraft, and its operating status is crucial to the safety of the aircraft and people. Over the years, accidents of engine damage due to the impact of air impactors have occurred from time to time, such as flying birds, hail, etc., and its consequences are very serious. From the perspective of aircraft structure, the front protection of the engine is the weakest, and ...

Claims

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Application Information

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IPC IPC(8): F02C7/055
Inventor 韩英
Owner 韩英
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