CN202348443U - 喷气式发动机进气口可调式防护罩 - Google Patents

喷气式发动机进气口可调式防护罩 Download PDF

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Publication number
CN202348443U
CN202348443U CN201120547474XU CN201120547474U CN202348443U CN 202348443 U CN202348443 U CN 202348443U CN 201120547474X U CN201120547474X U CN 201120547474XU CN 201120547474 U CN201120547474 U CN 201120547474U CN 202348443 U CN202348443 U CN 202348443U
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protective cover
jet engine
air inlet
adjustable protective
suction port
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Expired - Fee Related
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CN201120547474XU
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王玉臣
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Abstract

本实用新型的喷气式发动机进气口可调式防护罩涉及一种防护罩，在发动机进气口的边壁上设有插入式活动连杆，插入式活动连杆的另一端固接有防护罩。本实用新型喷气式发动机进气口可调式防护罩，结构简单，实施容易，成本低，同时可以有效的防止飞鸟撞进吸气孔，同时起到和风作用有利于空中二次启动发动机。

Description

喷气式发动机进气口可调式防护罩
技术领域
本实用新型涉及一种防护罩，尤其涉及一种喷气式发动机进气口可调式防护罩。
背景技术
目前，现有的喷气式发动机的吸气孔都完全裸露于外部，极易造成飞禽误入的事故，同时使得空中停车之后的二次启动带来困难。
发明内容
本实用新型旨在针对背景技术中存在的不足，而提供的一种喷气式发动机进气口可调式防护罩。
本实用新型的喷气式发动机进气口可调式防护罩，是在发动机进气口的边壁上设有插入式活动连杆，插入式活动连杆的另一端固接有防护罩。
作为本实用新型的进一步改进，在进气口的边壁上设有三个以上的插入式活动连杆。
本实用新型喷气式发动机进气口可调式防护罩，结构简单，实施容易，成本低，同时可以有效的防止飞鸟撞进吸气孔，同时起到和风作用有利于空中二次启动发动机。
附图说明
图1为本实用新型喷气式发动机进气口可调式防护罩的结构示意图。
具体实施方式
本实用新型的喷气式发动机进气口可调式防护罩，是在发动机进气口1的边壁上设有插入式活动连杆2，插入式活动连杆2的另一端固接有防护罩3，插入式连杆可以调节防护罩与进气孔的距离。在进气口1的边壁上设有三个以上的插入式活动连杆2。

Claims (2)

1.喷气式发动机进气口可调式防护罩，其特征是在发动机进气口（1）的边壁上设有插入式活动连杆（2），插入式活动连杆（2）的另一端固接有防护罩（3）。
2.如权利要求1所述的喷气式发动机进气口可调式防护罩，其特征是在进气口（1）的边壁上设有三个以上的插入式活动连杆（2）。
CN201120547474XU 2011-12-24 2011-12-24 喷气式发动机进气口可调式防护罩 Expired - Fee Related CN202348443U (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201120547474XU CN202348443U (zh) 2011-12-24 2011-12-24 喷气式发动机进气口可调式防护罩

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201120547474XU CN202348443U (zh) 2011-12-24 2011-12-24 喷气式发动机进气口可调式防护罩

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CN202348443U true CN202348443U (zh) 2012-07-25

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103979111A (zh) * 2014-04-24 2014-08-13 马同金 飞机碎鸟网罩刀
CN106864759A (zh) * 2017-02-20 2017-06-20 张延林 飞机发动机防护装置及防护方法
CN106965944A (zh) * 2016-01-13 2017-07-21 王振牛 一种喷气式飞机进气道多级缓冲防鸟撞罩的方法
CN109026438A (zh) * 2018-10-10 2018-12-18 吴拥军 高效喷气推进器

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103979111A (zh) * 2014-04-24 2014-08-13 马同金 飞机碎鸟网罩刀
CN103979111B (zh) * 2014-04-24 2016-10-26 马同金 飞机碎鸟网罩刀
CN106965944A (zh) * 2016-01-13 2017-07-21 王振牛 一种喷气式飞机进气道多级缓冲防鸟撞罩的方法
CN106864759A (zh) * 2017-02-20 2017-06-20 张延林 飞机发动机防护装置及防护方法
CN109026438A (zh) * 2018-10-10 2018-12-18 吴拥军 高效喷气推进器

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C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20120725

Termination date: 20121224