MX368612B - Mecanismo de plegado manual de ala. - Google Patents

Mecanismo de plegado manual de ala.

Info

Publication number
MX368612B
MX368612B MX2016001061A MX2016001061A MX368612B MX 368612 B MX368612 B MX 368612B MX 2016001061 A MX2016001061 A MX 2016001061A MX 2016001061 A MX2016001061 A MX 2016001061A MX 368612 B MX368612 B MX 368612B
Authority
MX
Mexico
Prior art keywords
wing
fold mechanism
aircraft
provides
outboard
Prior art date
Application number
MX2016001061A
Other languages
English (en)
Other versions
MX2016001061A (es
Inventor
Karkow Jon
Gionta Matthew
Wilding Joseph
Jagemann Michael
Original Assignee
Icon Aircraft Inc
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 Icon Aircraft Inc filed Critical Icon Aircraft Inc
Publication of MX2016001061A publication Critical patent/MX2016001061A/es
Publication of MX368612B publication Critical patent/MX368612B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/008—Amphibious sea planes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)

Abstract

Un mecanismo de plegado de ala manual provee medios por medios de los cuales se reconfigura el ala de una aeronave entre una configuración de vuelo y una que puede fácilmente guardarse y transportarse. El mecanismo de plegado incluye un tubo de extensión que permite que la porción exterior del ala se extienda lejos de la sección interior del ala, gire alrededor del eje lateral de la aeronave y después pivotee hacia atrás de tal forma que se almea con el eje longitudinal de la aeronave a lo largo del fuselaje. El mecanismo de plegado del ala es independiente de los componentes estructurales del ala usados para transportar las cargas aerodinámicas durante el vuelo y proveer medios al usuario para llevar a la sección de ala exterior en una posición casi de alineación mientras el mecanismo de plegado del ala a continuación ayuda a refinar la alineación a su configuración de vuelo final.
MX2016001061A 2013-07-26 2014-07-21 Mecanismo de plegado manual de ala. MX368612B (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201361858825P 2013-07-26 2013-07-26
US14/335,083 US10099770B2 (en) 2013-07-26 2014-07-18 Manuel wing-fold mechanism
PCT/US2014/047433 WO2015057286A1 (en) 2013-07-26 2014-07-21 Manual wing-fold mechanism

Publications (2)

Publication Number Publication Date
MX2016001061A MX2016001061A (es) 2016-04-20
MX368612B true MX368612B (es) 2019-10-09

Family

ID=52828535

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2016001061A MX368612B (es) 2013-07-26 2014-07-21 Mecanismo de plegado manual de ala.

Country Status (10)

Country Link
US (2) US10099770B2 (es)
EP (2) EP3013684B1 (es)
CN (2) CN105593116B (es)
AU (2) AU2014334927B2 (es)
BR (1) BR112016001299B1 (es)
CA (2) CA3124045A1 (es)
ES (2) ES2908687T3 (es)
MX (1) MX368612B (es)
RU (1) RU2674387C2 (es)
WO (1) WO2015057286A1 (es)

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RU2727896C1 (ru) * 2019-12-02 2020-07-24 Общество с ограниченной ответственностью "Научно Инженерная Компания" Самолет со складываемым крылом и устройство складывания крыла
CN112046730B (zh) * 2020-09-17 2022-01-04 江苏云博智能科技有限公司 一种无人机的机翼折叠结构
CN114194378A (zh) * 2021-12-31 2022-03-18 中国航天空气动力技术研究院 一种无人机伸缩机翼结构
CN114735197A (zh) * 2022-04-19 2022-07-12 清华大学 可折叠机翼的固定锁定机构
CN115056967B (zh) * 2022-06-29 2023-04-25 浙江大学 一种双轴旋转折叠的刚性机翼及使用方法
US20240262489A1 (en) * 2023-02-08 2024-08-08 Anduril Industries, Inc. Dual engine vertical take off and landing collapsible fixed wing aircraft
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Also Published As

Publication number Publication date
US20160185444A1 (en) 2016-06-30
WO2015057286A1 (en) 2015-04-23
RU2674387C2 (ru) 2018-12-07
ES2704702T3 (es) 2019-03-19
AU2014334927A1 (en) 2016-02-11
EP3013684B1 (en) 2018-10-31
EP3466809B1 (en) 2021-12-22
ES2908687T3 (es) 2022-05-03
RU2016102195A (ru) 2017-08-29
EP3013684A4 (en) 2017-03-29
AU2018203074B2 (en) 2020-04-09
EP3466809A1 (en) 2019-04-10
AU2014334927B2 (en) 2018-04-19
US10435138B2 (en) 2019-10-08
CN109703738A (zh) 2019-05-03
BR112016001299B1 (pt) 2022-02-22
CN105593116B (zh) 2019-02-01
US20180370612A1 (en) 2018-12-27
CA3124045A1 (en) 2015-04-23
CN109703738B (zh) 2022-05-17
MX2016001061A (es) 2016-04-20
CA2918749A1 (en) 2015-04-23
CN105593116A (zh) 2016-05-18
US10099770B2 (en) 2018-10-16
RU2016102195A3 (es) 2018-06-25
AU2018203074A1 (en) 2018-05-24
EP3013684A1 (en) 2016-05-04
CA2918749C (en) 2021-08-31
BR112016001299A2 (es) 2017-07-25

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