FR1003096A - Perfectionnements aux surfaces alaires à revêtement mobile ou déformable - Google Patents

Perfectionnements aux surfaces alaires à revêtement mobile ou déformable

Info

Publication number
FR1003096A
FR1003096A FR1003096DA FR1003096A FR 1003096 A FR1003096 A FR 1003096A FR 1003096D A FR1003096D A FR 1003096DA FR 1003096 A FR1003096 A FR 1003096A
Authority
FR
France
Prior art keywords
mobile
wing surfaces
deformable coating
deformable
coating
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
English (en)
Inventor
Jacques Gerin
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 FR1003096A publication Critical patent/FR1003096A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/30—Wings comprising inflatable structural components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1003096D 1946-12-04 1946-12-04 Perfectionnements aux surfaces alaires à revêtement mobile ou déformable Expired FR1003096A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1003096T 1946-12-04

Publications (1)

Publication Number Publication Date
FR1003096A true FR1003096A (fr) 1952-03-13

Family

ID=9562676

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1003096D Expired FR1003096A (fr) 1946-12-04 1946-12-04 Perfectionnements aux surfaces alaires à revêtement mobile ou déformable

Country Status (1)

Country Link
FR (1) FR1003096A (fr)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2932470A (en) * 1955-05-24 1960-04-12 Chance Vought Aircraft Inc Variable contour airfoil
US2960281A (en) * 1957-03-20 1960-11-15 Snecma Control device for the air intake of a jet propulsion unit
US3128966A (en) * 1964-04-14 Alvarez-calderon
US3139248A (en) * 1961-06-15 1964-06-30 Alvarez-Calderon Alberto Variable geometry system and apparatus for aircraft
US3188021A (en) * 1963-04-17 1965-06-08 Boeing Co Boundary layer control system utilizing a collapsible duct positioned in a control surface
US3195836A (en) * 1962-04-16 1965-07-20 Alvarez-Calderon Alberto High lift slotted flap
US3203647A (en) * 1961-12-06 1965-08-31 Alvarez-Calderon Alberto High lift fdaps for aircraft wings
US3711039A (en) * 1970-10-26 1973-01-16 Boeing Co Pneumatic leading edge flap for an aircraft wing
US4585192A (en) * 1983-03-30 1986-04-29 British Aerospace Public Limited Company Leading edge arrangements for aircraft wings
US6047923A (en) * 1995-01-13 2000-04-11 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
EP3156323A1 (fr) * 2015-10-15 2017-04-19 Airbus Operations S.L. Profil aérodynamique pour un bord d'attaque

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128966A (en) * 1964-04-14 Alvarez-calderon
US2932470A (en) * 1955-05-24 1960-04-12 Chance Vought Aircraft Inc Variable contour airfoil
US2960281A (en) * 1957-03-20 1960-11-15 Snecma Control device for the air intake of a jet propulsion unit
US3139248A (en) * 1961-06-15 1964-06-30 Alvarez-Calderon Alberto Variable geometry system and apparatus for aircraft
US3203647A (en) * 1961-12-06 1965-08-31 Alvarez-Calderon Alberto High lift fdaps for aircraft wings
US3195836A (en) * 1962-04-16 1965-07-20 Alvarez-Calderon Alberto High lift slotted flap
US3188021A (en) * 1963-04-17 1965-06-08 Boeing Co Boundary layer control system utilizing a collapsible duct positioned in a control surface
US3711039A (en) * 1970-10-26 1973-01-16 Boeing Co Pneumatic leading edge flap for an aircraft wing
US4585192A (en) * 1983-03-30 1986-04-29 British Aerospace Public Limited Company Leading edge arrangements for aircraft wings
US6047923A (en) * 1995-01-13 2000-04-11 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
EP3156323A1 (fr) * 2015-10-15 2017-04-19 Airbus Operations S.L. Profil aérodynamique pour un bord d'attaque
US10322793B2 (en) 2015-10-15 2019-06-18 Airbus Operations S.L. Leading edge for an airfoil

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