Engine mobile cover and engine reverse thrust device

A technology of a thrust reverser and a moving cover, which is applied to machines/engines, jet propulsion devices, etc., can solve the problems of inconvenient maintenance and complex structure, and achieve the effect of using fewer mechanisms.

Active Publication Date: 2015-06-17
AECC COMML AIRCRAFT ENGINE CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0017] One of the objectives of the present invention is to propose a movable engine cover and an engine thrust reverser device provided with the movable cover, which solves the technical problems of complex structure and inconvenient maintenance in the prior art

Method used

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  • Engine mobile cover and engine reverse thrust device
  • Engine mobile cover and engine reverse thrust device
  • Engine mobile cover and engine reverse thrust device

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Embodiment Construction

[0067] Below you can refer to the accompanying drawings Figure 1 to Figure 8 And the content of the text to understand the content of the present invention and the differences between the present invention and the prior art. The technical solution (including the preferred technical solution) of the present invention will be further described in detail below by way of the accompanying drawings and listing some optional embodiments of the present invention. It should be noted that: any technical feature and any technical solution in this embodiment are one or more of a variety of optional technical features or optional technical solutions. Citing all the alternative technical features and alternative technical solutions of the present invention, it is not convenient for the implementation of each technical feature to emphasize that it is one of the optional multiple implementation modes, so those skilled in the art should know that: Replace any technical means provided by the ...

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Abstract

The invention discloses an engine mobile cover and an engine reverse thrust device, relates to the technical field of aero-engines, and solves the technical problems of complex structure and inconvenience for maintenance in the prior art. The engine mobile cover comprises a mobile cover body part, a reset mechanism and at least one blocking door, wherein a blocking surface is arranged on one side surface of the blocking door; the blocking door is movably connected with the mobile cover body part, and can rotate around the movable connection position to an opening position and a closing position relative to the mobile cover body part; and the reset mechanism is arranged between one side surface, opposite the blocking surface, of the blocking door and the mobile cover body part, and can apply enough reset force to the blocking door to rotate the blocking door from the opening position to the closing position. The engine reverse thrust device comprises a core engine hood, a blade grid component, a blade grid support ring, a driving mechanism and the engine mobile cover provided by the invention. According to the invention, the structure of the engine reverse thrust device is simplified and optimized.

Description

technical field [0001] The invention relates to the technical field of aero-engines, in particular to an engine movable cover and an engine thrust reverser provided with the engine movable cover. Background technique [0002] The engine thrust reverser is a device used to change the direction of the engine fan airflow to generate reverse thrust. When the aircraft lands normally, it can shorten the landing run distance of the aircraft on dry and slippery runways. [0003] In high bypass ratio turbofan engines, cold flow thrust reversers are usually used. The cold air flow reverse thrust device is a device that makes the low-temperature air flow that has not passed through the combustion chamber change its direction and sprays out to the side and front by mechanical baffle deflection or other methods, thereby generating backward reverse thrust for the engine or aircraft. . At present, relatively mature cold airflow thrust reversers are mainly divided into baffle door thrust ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K3/02
Inventor 周建强李永国
Owner AECC COMML AIRCRAFT ENGINE CO LTD
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