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CA2121823A1 - Element de suspension d'aile d'avion - Google Patents

Element de suspension d'aile d'avion

Info

Publication number
CA2121823A1
CA2121823A1 CA002121823A CA2121823A CA2121823A1 CA 2121823 A1 CA2121823 A1 CA 2121823A1 CA 002121823 A CA002121823 A CA 002121823A CA 2121823 A CA2121823 A CA 2121823A CA 2121823 A1 CA2121823 A1 CA 2121823A1
Authority
CA
Canada
Prior art keywords
wing
movement
pivot
loads
flight
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.)
Abandoned
Application number
CA002121823A
Other languages
English (en)
Inventor
Paul Wesley Dawson
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 CA002121823A priority Critical patent/CA2121823A1/fr
Publication of CA2121823A1 publication Critical patent/CA2121823A1/fr
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
CA002121823A 1994-04-21 1994-04-21 Element de suspension d'aile d'avion Abandoned CA2121823A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA002121823A CA2121823A1 (fr) 1994-04-21 1994-04-21 Element de suspension d'aile d'avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA002121823A CA2121823A1 (fr) 1994-04-21 1994-04-21 Element de suspension d'aile d'avion

Publications (1)

Publication Number Publication Date
CA2121823A1 true CA2121823A1 (fr) 1995-10-22

Family

ID=4153422

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002121823A Abandoned CA2121823A1 (fr) 1994-04-21 1994-04-21 Element de suspension d'aile d'avion

Country Status (1)

Country Link
CA (1) CA2121823A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2915173A1 (fr) * 2007-04-17 2008-10-24 Airbus Sa Sa Dispositif de fixation d'un organe de sustentation au fuselage d'un avion.
CN111003142A (zh) * 2019-12-25 2020-04-14 中国航空工业集团公司西安飞机设计研究所 一种翼身柔性连接装置

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2915173A1 (fr) * 2007-04-17 2008-10-24 Airbus Sa Sa Dispositif de fixation d'un organe de sustentation au fuselage d'un avion.
WO2008145892A1 (fr) 2007-04-17 2008-12-04 Airbus Dispositif de fixation d'un organe de sustentation au fuselage d'un avion
JP2010524763A (ja) * 2007-04-17 2010-07-22 エアバス フランス 飛行機の揚力部材を胴体に固定する装置
US8544789B2 (en) 2007-04-17 2013-10-01 Airbus Operations Sas Device for attaching a lift member to the fuselage of an aircraft
CN111003142A (zh) * 2019-12-25 2020-04-14 中国航空工业集团公司西安飞机设计研究所 一种翼身柔性连接装置
CN111003142B (zh) * 2019-12-25 2022-08-19 中国航空工业集团公司西安飞机设计研究所 一种翼身柔性连接装置

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Legal Events

Date Code Title Description
FZDE Discontinued