FR1122894A - wall element for a hollow body of aerodynamic shape usable in particular in aeronautics and its manufacturing process - Google Patents

wall element for a hollow body of aerodynamic shape usable in particular in aeronautics and its manufacturing process

Info

Publication number
FR1122894A
FR1122894A FR1122894DA FR1122894A FR 1122894 A FR1122894 A FR 1122894A FR 1122894D A FR1122894D A FR 1122894DA FR 1122894 A FR1122894 A FR 1122894A
Authority
FR
France
Prior art keywords
aeronautics
manufacturing process
hollow body
wall element
aerodynamic shape
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
Other languages
French (fr)
Inventor
Lionel-Charles Heal
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 filed Critical
Application granted granted Critical
Publication of FR1122894A publication Critical patent/FR1122894A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1122894D 1955-04-22 1955-04-22 wall element for a hollow body of aerodynamic shape usable in particular in aeronautics and its manufacturing process Expired FR1122894A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1122894T 1955-04-22

Publications (1)

Publication Number Publication Date
FR1122894A true FR1122894A (en) 1956-09-13

Family

ID=9632875

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1122894D Expired FR1122894A (en) 1955-04-22 1955-04-22 wall element for a hollow body of aerodynamic shape usable in particular in aeronautics and its manufacturing process

Country Status (1)

Country Link
FR (1) FR1122894A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3070369A1 (en) * 2017-08-30 2019-03-01 Airbus Operations METHOD FOR MANUFACTURING AN AIRCRAFT ATTACK EDGE PANEL FOR OBTAINING EXTENDED LAMINAR FLOW, ATTACHING EDGE COMPRISING AT LEAST ONE PANEL OBTAINED FROM SAID METHOD

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3070369A1 (en) * 2017-08-30 2019-03-01 Airbus Operations METHOD FOR MANUFACTURING AN AIRCRAFT ATTACK EDGE PANEL FOR OBTAINING EXTENDED LAMINAR FLOW, ATTACHING EDGE COMPRISING AT LEAST ONE PANEL OBTAINED FROM SAID METHOD
EP3450303A1 (en) * 2017-08-30 2019-03-06 Airbus Operations S.A.S. Method for manufacturing a panel of an aircraft leading edge for providing an extended laminar flow, leading edge comprising at least one panel obtained by the method
US11027818B2 (en) 2017-08-30 2021-06-08 Airbus Operations S.A.S. Method for manufacturing an aircraft leading edge panel that allows extensive laminar flow to be obtained, and leading edge comprising at least one panel obtained using the said method

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