CN104648649A - Airship for vertical take-off and landing of aircraft - Google Patents

Airship for vertical take-off and landing of aircraft Download PDF

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Publication number
CN104648649A
CN104648649A CN201310579434.7A CN201310579434A CN104648649A CN 104648649 A CN104648649 A CN 104648649A CN 201310579434 A CN201310579434 A CN 201310579434A CN 104648649 A CN104648649 A CN 104648649A
Authority
CN
China
Prior art keywords
aircraft
landing
airship
dirigible
vertical take
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201310579434.7A
Other languages
Chinese (zh)
Inventor
武泽馨
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xiangzhou No 4 Middle School
Original Assignee
Xiangzhou No 4 Middle School
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Xiangzhou No 4 Middle School filed Critical Xiangzhou No 4 Middle School
Priority to CN201310579434.7A priority Critical patent/CN104648649A/en
Publication of CN104648649A publication Critical patent/CN104648649A/en
Pending legal-status Critical Current

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Abstract

The invention relates to an airship for vertical take-off and landing of an aircraft. The airship consists of a rigid airship and a guide rail and can be used for realizing vertical take-off and landing of the aircraft. A take-off mode of a fixed wing aircraft is changed to vertical take-off and landing, so that energy-saving and environment-friendly take-off operation is realized.

Description

Can for the dirigible of aircraft vertical landing
Technical field
The present invention relates to a kind of rigid airship, be specifically related to a kind of dirigible for aircraft vertical landing, fixed wing aircraft can be promoted to high aerial, horizontal for fixed wing aircraft impelling is gone out by recycling dirigible own level flying speed and guide rail, make aircraft obtain certain initial velocity in the horizontal direction, thus can accelerate to realize high-altitude flight.
Background technology
Current fixed wing aircraft takes off, and must carry out accelerated slip on the runway of land, when coasting speed reaches certain critical value, aircraft will take off.This pattern Problems existing that takes off is: 1, take off and need airstrips that is professional, long distance; 2, slide acceleration and need lot of energy.These 2 quite obvious when developing intercity short distance blimp aircraft industry.
Summary of the invention
The present invention is exactly to solve the problem, a kind of dirigible for aircraft vertical landing can be provided, be specifically related to a kind of load-carrying ability large, fixed wing aircraft can be promoted to high aerial, horizontal for fixed wing aircraft impelling is gone out by recycling dirigible own level flying speed and guide rail, make aircraft obtain certain initial velocity in the horizontal direction, thus can accelerate to realize high-altitude flight.The dirigible that this kind of second-mission aircraft takes off, is applicable to develop intercity short distance blimp air traffic.Utilizing dirigible buoyant lift aircraft, consuming less energy by gliding to take off than aircraft self.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described.
Fig. 1 is structural representation of the present invention.
Detailed description of the invention
Shown in Fig. 1: be provided with the length slide rail roughly the same with dirigible 2 in dirigible 1 belly lower end.

Claims (1)

1. for a dirigible for aircraft vertical landing, can it is characterized in that, be provided with the length slide rail roughly the same with dirigible (2) in dirigible (1) belly lower end.
CN201310579434.7A 2013-11-19 2013-11-19 Airship for vertical take-off and landing of aircraft Pending CN104648649A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310579434.7A CN104648649A (en) 2013-11-19 2013-11-19 Airship for vertical take-off and landing of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310579434.7A CN104648649A (en) 2013-11-19 2013-11-19 Airship for vertical take-off and landing of aircraft

Publications (1)

Publication Number Publication Date
CN104648649A true CN104648649A (en) 2015-05-27

Family

ID=53240387

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310579434.7A Pending CN104648649A (en) 2013-11-19 2013-11-19 Airship for vertical take-off and landing of aircraft

Country Status (1)

Country Link
CN (1) CN104648649A (en)

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20150527

WD01 Invention patent application deemed withdrawn after publication