FR421352A - Airplane with shock-absorbing device - Google Patents

Airplane with shock-absorbing device

Info

Publication number
FR421352A
FR421352A FR421352A FR421352DA FR421352A FR 421352 A FR421352 A FR 421352A FR 421352 A FR421352 A FR 421352A FR 421352D A FR421352D A FR 421352DA FR 421352 A FR421352 A FR 421352A
Authority
FR
France
Prior art keywords
airplane
shock
absorbing device
absorbing
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.)
Expired
Application number
FR421352A
Other languages
French (fr)
Inventor
Georges Nadig
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
Application granted granted Critical
Publication of FR421352A publication Critical patent/FR421352A/en
Expired legal-status Critical Current

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
    • B64C3/385—Variable incidence wings
    • 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)
FR421352A 1910-10-12 1910-10-12 Airplane with shock-absorbing device Expired FR421352A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR421352T 1910-10-12

Publications (1)

Publication Number Publication Date
FR421352A true FR421352A (en) 1911-02-21

Family

ID=1464411

Family Applications (1)

Application Number Title Priority Date Filing Date
FR421352A Expired FR421352A (en) 1910-10-12 1910-10-12 Airplane with shock-absorbing device

Country Status (1)

Country Link
FR (1) FR421352A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2860100A1 (en) * 2013-10-09 2015-04-15 The Boeing Company Aircraft wing-to-fuselage joint with active suspension and method
WO2016038097A1 (en) * 2014-09-12 2016-03-17 Airbus Operations Gmbh Aircraft having hydraulic support struts between fuselage and wings

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2860100A1 (en) * 2013-10-09 2015-04-15 The Boeing Company Aircraft wing-to-fuselage joint with active suspension and method
US9399508B2 (en) 2013-10-09 2016-07-26 The Boeing Company Aircraft wing-to-fuselage joint with active suspension and method
WO2016038097A1 (en) * 2014-09-12 2016-03-17 Airbus Operations Gmbh Aircraft having hydraulic support struts between fuselage and wings
CN106715262A (en) * 2014-09-12 2017-05-24 空中客车运作有限责任公司 Aircraft having hydraulic support struts between fuselage and wings
US10988234B2 (en) 2014-09-12 2021-04-27 Airbus Operations Gmbh Aircraft having hydraulic support struts between fuselage and wings

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