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Aerial propulsion equipment

A technology for propulsion equipment and aviation, applied in the field of aviation, can solve problems such as heat dissipation and gear transmission lubrication, and achieve the effects of improving work coordination, improving technical level, and being easy to use

Inactive Publication Date: 2018-08-21
赵婷婷 +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Aviation propulsion equipment is widely used in the aerospace field. It mainly provides power for aerospace flight equipment. However, traditional aviation propulsion equipment has certain problems with heat dissipation and lubrication in gear transmission during operation. This equipment effectively solves this problem. question

Method used

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  • Aerial propulsion equipment
  • Aerial propulsion equipment
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Embodiment Construction

[0019] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.

[0020] Any feature disclosed in this specification (including any appended claims, abstract and drawings), unless expressly stated otherwise, may be replaced by alternative features which are equivalent or serve a similar purpose. That is, unless expressly stated otherwise, each feature is one example only of a series of equivalent or similar features.

[0021] Such as Figure 1-3As shown, an aviation propulsion device of the present invention includes a casing 100, a first hollow 114 is fixed in the casing 100, and a second hollow 114 is fixed in the end wall of the first hollow 114. 119, the upper and lower end walls of the second empty groove 119 are fixed with an annular groove 118 with the mouth facing inward, and the end wall of the second empty groove 119 away from the first empty groo...

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Abstract

The invention discloses aerial propulsion equipment, comprising an enclosure, wherein a first hollow groove is fixedly formed in the enclosure, a second hollow groove is fixedly formed in an end wallof the first hollow groove, ring slots with inward opening parts are fixedly formed in upper and lower end walls of the second hollow groove, a first switching cavity is formed in an end wall, away from the first hollow groove, of the second hollow groove in a communicating way, a plurality of push blocks are arranged in the first switching cavity by sliding connection, a first fixed connection rod is fixedly arranged on an end face, facing the first hollow groove, of each push block, the ring slots in sliding fit connection with a first closed pad is fixedly formed in an end face, facing thefirst hollow groove, of the first fixed connection rod, and close the first closed pad, and a first connecting arm is fixedly arranged on an end face, facing the first hollow groove, of each ring slot, penetrates through the second hollow groove, and extends into the first hollow groove.

Description

technical field [0001] The invention relates to the field of aviation technology, in particular to an aviation propulsion device. Background technique [0002] Aviation propulsion equipment is widely used in the aerospace field. It mainly provides power for aerospace flight equipment. However, traditional aviation propulsion equipment has certain problems with heat dissipation and lubrication in gear transmission during operation. This equipment effectively solves this problem. question. Contents of the invention [0003] The object of the present invention is to provide an aeropropulsion device capable of overcoming the above-mentioned defects of the prior art. [0004] According to the present invention, the aeronautical propulsion equipment of the present invention comprises a casing, a first hollow slot is fixedly provided in the casing, a second hollow slot is fixedly provided in the end wall of the first hollow slot, and the The upper and lower end walls of the sec...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/40
CPCB64G1/40
Inventor 赵婷婷黎庆李小华
Owner 赵婷婷