CN105620764A - 带火箭推进器的飞机 - Google Patents

带火箭推进器的飞机 Download PDF

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Publication number
CN105620764A
CN105620764A CN201610116601.8A CN201610116601A CN105620764A CN 105620764 A CN105620764 A CN 105620764A CN 201610116601 A CN201610116601 A CN 201610116601A CN 105620764 A CN105620764 A CN 105620764A
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CN
China
Prior art keywords
aircraft
rocket thruster
rocket
rocket propulsion
regulating direction
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Pending
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CN201610116601.8A
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English (en)
Inventor
李和坤
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Individual
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Individual
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Publication date
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Priority to CN201610116601.8A priority Critical patent/CN105620764A/zh
Publication of CN105620764A publication Critical patent/CN105620764A/zh
Pending legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage
    • B64D27/40—
    • B64D27/404—

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

本发明公开了一种带火箭推进器的飞机，属飞行安全技术领域，主要由飞机、调向装置和火箭推进器组成，把火箭推进器通过调响装置装在飞机下方，当飞机因发动机故障和其它原因发生失速时，迅速启动火箭推进器，把飞机推到足够的高度，让飞行员获得更多的时间来取理事故和采取其它错施，减少空难的发生。

Description

带火箭推进器的飞机
技朮领域
本发明涉及航空安全技朮领域，尤其是一种带火箭推进器的飞机。
背景技朮
飞行中的民航机、运输机或者战斗机会遇到突然发动机故障和其它原因引起飞机失速，这时飞行员要有足够的时间耒处理亊故和采取其它错施，这时飞机飞行高度是关键，飞行高度过低极易发生空难，2015年2月4日台湾空难就是在这种情况下发生的，全世界这样的案例不在少数。
发明内容
本发明要解决的问题是提供一种带火箭推进器的飞机，当飞机失速时，迅速启动火箭推进器，把飞机推到足够的高度。
为解决上述问题，本发明采用的方案是：在飞机的下方安一个调向装置，调向装置内装有火箭推进器，当飞机失速后调向装置可根据飞机飞行姿态调整火箭推进器喷气口方向，使飞机获得最佳升力。
由于采用上述方案，本发明与现有技朮相比效有如下有益效果：
当飞机失速后飞行员可获更多时间来处理亊故和采取其它错施，减少空难的发生。
附图说明
说明书附图是本发明的结构示意图。
具体实施方式
以下结合附图实例对本发明的结构作进一步说明：
在附图所示的结构中，飞机3的下方装有调向装置2，调向装置2内装有火箭推进器1，调向装置2可对火箭推进器1进行调向。

Claims (1)

1.一种带火箭推进器的飞机，主要由飞机、调向装置和火箭推进器组成，其特征在于：飞机3的下方装有调向装置2，调向装置2内装有火箭推进器1，调向装置2可对火箭推进器1进行调向。
CN201610116601.8A 2016-02-16 2016-02-16 带火箭推进器的飞机 Pending CN105620764A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610116601.8A CN105620764A (zh) 2016-02-16 2016-02-16 带火箭推进器的飞机

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610116601.8A CN105620764A (zh) 2016-02-16 2016-02-16 带火箭推进器的飞机

Publications (1)

Publication Number Publication Date
CN105620764A true CN105620764A (zh) 2016-06-01

Family

ID=56036192

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610116601.8A Pending CN105620764A (zh) 2016-02-16 2016-02-16 带火箭推进器的飞机

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CN (1) CN105620764A (zh)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106081127A (zh) * 2016-07-27 2016-11-09 冯政尧 空难逃生飞机
CN106379541A (zh) * 2016-08-30 2017-02-08 金嵩 一种飞机起降轮上的驱动部件

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3363861A (en) * 1963-12-11 1968-01-16 Messerschmitt Boelkow Blohm Rocket propelled winged aircraft
US4721271A (en) * 1985-02-14 1988-01-26 The Boeing Company Devices and method for rocket booster vectoring to provide stability augmentation during a booster launch phase
US4817892A (en) * 1986-04-28 1989-04-04 Janeke Charl E Aerospace plane and engine therefor
CN200967562Y (zh) * 2006-11-20 2007-10-31 大连三科航空科技有限公司 高亚音速无人机
CN201101890Y (zh) * 2007-10-05 2008-08-20 石天衡 带搜寻指示器的航模飞机
CN201510749U (zh) * 2009-09-26 2010-06-23 胡吉炜 火箭动力玩具飞机
US7762077B2 (en) * 2006-12-05 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Single-stage hypersonic vehicle featuring advanced swirl combustion
CN102826227A (zh) * 2012-08-22 2012-12-19 冯加伟 无人空天战机

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3363861A (en) * 1963-12-11 1968-01-16 Messerschmitt Boelkow Blohm Rocket propelled winged aircraft
US4721271A (en) * 1985-02-14 1988-01-26 The Boeing Company Devices and method for rocket booster vectoring to provide stability augmentation during a booster launch phase
US4817892A (en) * 1986-04-28 1989-04-04 Janeke Charl E Aerospace plane and engine therefor
CN200967562Y (zh) * 2006-11-20 2007-10-31 大连三科航空科技有限公司 高亚音速无人机
US7762077B2 (en) * 2006-12-05 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Single-stage hypersonic vehicle featuring advanced swirl combustion
CN201101890Y (zh) * 2007-10-05 2008-08-20 石天衡 带搜寻指示器的航模飞机
CN201510749U (zh) * 2009-09-26 2010-06-23 胡吉炜 火箭动力玩具飞机
CN102826227A (zh) * 2012-08-22 2012-12-19 冯加伟 无人空天战机

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106081127A (zh) * 2016-07-27 2016-11-09 冯政尧 空难逃生飞机
CN106379541A (zh) * 2016-08-30 2017-02-08 金嵩 一种飞机起降轮上的驱动部件

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