CN103950542A - 减阻风头 - Google Patents

减阻风头 Download PDF

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Publication number
CN103950542A
CN103950542A CN201410133634.4A CN201410133634A CN103950542A CN 103950542 A CN103950542 A CN 103950542A CN 201410133634 A CN201410133634 A CN 201410133634A CN 103950542 A CN103950542 A CN 103950542A
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inlet channel
air
drag
driving engine
inlet
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CN201410133634.4A
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CN103950542B (zh
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张鑫宇
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Abstract

本发明涉及一种减阻风头。此设计适用于大型民航飞机。利用发动机的引气减小飞机在飞行中所受到的气动阻力。用于减小飞机在飞行中说受的气动阻力。

Description

减阻风头
技术领域
本发明是一种飞机飞行中减小阻力的设计。 
背景技术
利用发动机巨大的吸引力，吸引气流，减小飞机飞行时的空气阻力。 
发明内容
本设计主要是有小风头，主风头，小通风管，主通风管，空气流量主控制门以及发动机组成。小通风头吸引来自前方的气流通过小通风管汇聚到主通风头里，空气流量主控制门控制气流流量经过第二进气道进入发动机。动力来源为发动机的内部动力。整个管路的排布要达到空气在管道内流动时阻力最小。可以通过调节第一进气道内的内进气环来调节第一进气道与第二进气道的空气流量的比例。发动机在机翼下吊装的位置要与通风管的排布一致。
附图说明 
图1是小通风头及通风管的排布演示图。
图2是飞机减阻风头图。

Claims (4)

1.一种减小飞机在飞行中空气阻力的设计主要有小通风头，小通风管，主通风头，主通风管，空气流量主控制门，第一进气道，第二进气道，内进气环以及发动机组成。
2.各种通风头和通风管负责吸引气流并引入发动机。
3.空气流量主控制门控制空气流量。
4.如权利要求一所诉第一进气道与第二进气道通过内进气环的调节，实现控制第一进气道与第二进气道空气流量的比例，并引进发动机。
CN201410133634.4A 2014-04-04 2014-04-04 用于减小飞机在飞行中空气阻力的装置 Expired - Fee Related CN103950542B (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410133634.4A CN103950542B (zh) 2014-04-04 2014-04-04 用于减小飞机在飞行中空气阻力的装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410133634.4A CN103950542B (zh) 2014-04-04 2014-04-04 用于减小飞机在飞行中空气阻力的装置

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CN103950542A true CN103950542A (zh) 2014-07-30
CN103950542B CN103950542B (zh) 2017-01-04

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112173111A (zh) * 2020-11-05 2021-01-05 娄底市速尔成科技有限公司 一种基于互联网的载物无人机

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4611616A (en) * 1984-01-10 1986-09-16 Messerschmitt-Bolkow-Blohm Gmbh Axially semisymmetrical supersonic air intake for reaction engines, particularly solid fuel ram jet rocket engines
EP1243782A2 (en) * 2001-03-23 2002-09-25 The Boeing Company Double jet engine inlet
CN101224790A (zh) * 2008-01-25 2008-07-23 朱晓义 具有气流通道的飞行器
CN101531251A (zh) * 2009-04-22 2009-09-16 黄建芳 一种用于飞行器的安全保护装置
CN101857085A (zh) * 2010-06-03 2010-10-13 刘春� 一种飞行器

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4611616A (en) * 1984-01-10 1986-09-16 Messerschmitt-Bolkow-Blohm Gmbh Axially semisymmetrical supersonic air intake for reaction engines, particularly solid fuel ram jet rocket engines
EP1243782A2 (en) * 2001-03-23 2002-09-25 The Boeing Company Double jet engine inlet
CN101224790A (zh) * 2008-01-25 2008-07-23 朱晓义 具有气流通道的飞行器
CN101531251A (zh) * 2009-04-22 2009-09-16 黄建芳 一种用于飞行器的安全保护装置
CN101857085A (zh) * 2010-06-03 2010-10-13 刘春� 一种飞行器

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112173111A (zh) * 2020-11-05 2021-01-05 娄底市速尔成科技有限公司 一种基于互联网的载物无人机
CN112173111B (zh) * 2020-11-05 2022-05-06 娄底市速尔成科技有限公司 一种基于互联网的载物无人机

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Termination date: 20170404