FR675207A - Plane - Google Patents

Plane

Info

Publication number
FR675207A
FR675207A FR675207DA FR675207A FR 675207 A FR675207 A FR 675207A FR 675207D A FR675207D A FR 675207DA FR 675207 A FR675207 A FR 675207A
Authority
FR
France
Prior art keywords
plane
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
Gabriel Miquel
Felix Ladeveze
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 FR675207A publication Critical patent/FR675207A/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
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR675207D 1929-05-15 1929-05-15 Plane Expired FR675207A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR675207T 1929-05-15

Publications (1)

Publication Number Publication Date
FR675207A true FR675207A (en) 1930-02-07

Family

ID=9019247

Family Applications (1)

Application Number Title Priority Date Filing Date
FR675207D Expired FR675207A (en) 1929-05-15 1929-05-15 Plane

Country Status (1)

Country Link
FR (1) FR675207A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4175721A (en) * 1977-06-30 1979-11-27 Lempa Bernard J Jr Trim tab control mechanism
FR2445267A1 (en) * 1978-12-29 1980-07-25 Philippe Marc Aerofoil structure with trailing edge made from flexible material - allows control of fluid flow over section without break in surface
US4386574A (en) * 1981-12-15 1983-06-07 Riolland Pierre L Sail assembly of variable profile, reversible and collapsible

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4175721A (en) * 1977-06-30 1979-11-27 Lempa Bernard J Jr Trim tab control mechanism
FR2445267A1 (en) * 1978-12-29 1980-07-25 Philippe Marc Aerofoil structure with trailing edge made from flexible material - allows control of fluid flow over section without break in surface
US4386574A (en) * 1981-12-15 1983-06-07 Riolland Pierre L Sail assembly of variable profile, reversible and collapsible

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