CN105857572A - Inflatable aircraft wing - Google Patents

Inflatable aircraft wing Download PDF

Info

Publication number
CN105857572A
CN105857572A CN201610169767.6A CN201610169767A CN105857572A CN 105857572 A CN105857572 A CN 105857572A CN 201610169767 A CN201610169767 A CN 201610169767A CN 105857572 A CN105857572 A CN 105857572A
Authority
CN
China
Prior art keywords
aircraft wing
inflatable
wing
cab
inflatable aircraft
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
CN201610169767.6A
Other languages
Chinese (zh)
Inventor
任宝全
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201610169767.6A priority Critical patent/CN105857572A/en
Publication of CN105857572A publication Critical patent/CN105857572A/en
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/30—Wings comprising inflatable structural components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

The invention provides an inflatable aircraft wing. The inflatable aircraft wing (105 in figure 1) is mounted on an aircraft cab (101 in figure 1); an airscrew support (104 in figure 1) is arranged on the top of the cab; an airscrew (102 in figure 1) is mounted on the top of the support; and walking wheels (103 in figure 1) are arranged at the bottom of the cab. The shape of the aircraft wing is formed by cutting a flexible airtight material, and the aircraft wing is an enclosed structure with hollow interior; after inflation, the inflatable aircraft wing functions as the wing; and after deflation, the inflatable aircraft wing only occupies small space.

Description

A kind of inflated type aircraft wing
Technical field
Aircraft mechanical manufactures field.
Background technology
Existing aircraft wing is mostly with fixed in the majority, then to have be exactly folding.
Summary of the invention
The invention discloses the manufacture method of a kind of inflated type aircraft wing, the shape of aircraft wing profile it is tailored into a kind of flexible hermetic high intensity thin property material, require that inner hollow is airtight bears certain pressure, charge gas and can play the effect of aircraft wing, deflated take little space.
Accompanying drawing explanation
The present invention is further described below in conjunction with the accompanying drawings.
Fig. 1 is the aircraft wing of the present invention overall schematic when charging gas.
Fig. 2 be aircraft wing of the present invention deflated time overall schematic.

Claims (2)

1. the aircraft wing of flexible hollow closed structure is advanced.
2.High-strength ultra-thin advance.
CN201610169767.6A 2016-03-23 2016-03-23 Inflatable aircraft wing Pending CN105857572A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610169767.6A CN105857572A (en) 2016-03-23 2016-03-23 Inflatable aircraft wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610169767.6A CN105857572A (en) 2016-03-23 2016-03-23 Inflatable aircraft wing

Publications (1)

Publication Number Publication Date
CN105857572A true CN105857572A (en) 2016-08-17

Family

ID=56624778

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610169767.6A Pending CN105857572A (en) 2016-03-23 2016-03-23 Inflatable aircraft wing

Country Status (1)

Country Link
CN (1) CN105857572A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107458600A (en) * 2017-08-10 2017-12-12 北京航空航天大学 A kind of flapping wing that folding and unfolding is driven using inflation/deflation

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0768238A1 (en) * 1995-10-11 1997-04-16 Tokuzo Hirose Aircraft and method of flying the same
CN2335888Y (en) * 1996-11-05 1999-09-01 雷良榆 Inflated flexible wing aircraft
CN102923298A (en) * 2012-11-22 2013-02-13 哈尔滨工业大学 Wire falling array type inflatable unfolding wing
CN103963960A (en) * 2014-05-14 2014-08-06 北京航空航天大学 Semi-rigid inflatable automatically-unfolded-folded wing
CN104925243A (en) * 2015-06-26 2015-09-23 西北工业大学 Wingspan-changeable inflatable floating and rising integrated stratospheric airship

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0768238A1 (en) * 1995-10-11 1997-04-16 Tokuzo Hirose Aircraft and method of flying the same
CN2335888Y (en) * 1996-11-05 1999-09-01 雷良榆 Inflated flexible wing aircraft
CN102923298A (en) * 2012-11-22 2013-02-13 哈尔滨工业大学 Wire falling array type inflatable unfolding wing
CN103963960A (en) * 2014-05-14 2014-08-06 北京航空航天大学 Semi-rigid inflatable automatically-unfolded-folded wing
CN104925243A (en) * 2015-06-26 2015-09-23 西北工业大学 Wingspan-changeable inflatable floating and rising integrated stratospheric airship

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107458600A (en) * 2017-08-10 2017-12-12 北京航空航天大学 A kind of flapping wing that folding and unfolding is driven using inflation/deflation

Similar Documents

Publication Publication Date Title
GB2534791A (en) Inflatable play structure with integrated inflation mechanism
CN209977129U (en) Inflatable airbag based on pressure sensor
CO2018008682A2 (en) Improved device for sealing and inflating damaged inflatable items, such as punctured tires
CN105857572A (en) Inflatable aircraft wing
WO2014186046A3 (en) Helicopter external life raft pod
CN202098233U (en) Outer tire of graphene tire
MX360628B (en) Self-actuating flow restrictor for a vehicle airbag assembly.
CN106697251B (en) A kind of pneumatic muscles variant stratospheric airship
ES2539967T3 (en) Procedure and control and / or pressure adjustment device for a mounted assembly
CN104590539B (en) Formula airship envelope superpressure and deformation controller in hole is opened for umbrella
CN203818596U (en) Cooling setter for tire production
CN202056366U (en) Safety air valve and inflatable pool with same
CN105270581A (en) Lifesaving airbag
CN200978004Y (en) Storage mobile multi-gasbag aerostat
CN105988280A (en) Easily-foldable and unfoldable inflating and suction soft ball screen
CN207023617U (en) The bag of campaign-styled pneumatic decorative
CN205714646U (en) Can automatic inflating or the air compressor machine of venting
CN105077877A (en) Automatically inflatable sunshade
CN105988279A (en) Easily-foldable, unfoldable and inflatable soft ball screen
CN204296376U (en) Runflat, puncture-proof tire structure-improved
CN207409169U (en) Atmospheric pressure demonstration teaching aid
CN204433043U (en) A kind of micro-balloon device for filling
CN202525625U (en) Portable sofa
RU2500573C1 (en) Disc-shape aircraft driven by air
CN203126488U (en) Novel automobile cover

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160817