FR839422A - Rudder device for flat descent aircraft - Google Patents

Rudder device for flat descent aircraft

Info

Publication number
FR839422A
FR839422A FR839422DA FR839422A FR 839422 A FR839422 A FR 839422A FR 839422D A FR839422D A FR 839422DA FR 839422 A FR839422 A FR 839422A
Authority
FR
France
Prior art keywords
rudder device
flat
aircraft
descent aircraft
flat descent
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
Elie Jean Henri Billioque
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 FR839422A publication Critical patent/FR839422A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
FR839422D 1937-12-09 1937-12-09 Rudder device for flat descent aircraft Expired FR839422A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR839422T 1937-12-09

Publications (1)

Publication Number Publication Date
FR839422A true FR839422A (en) 1939-04-04

Family

ID=9299519

Family Applications (1)

Application Number Title Priority Date Filing Date
FR839422D Expired FR839422A (en) 1937-12-09 1937-12-09 Rudder device for flat descent aircraft

Country Status (1)

Country Link
FR (1) FR839422A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2500689A (en) * 1945-02-05 1950-03-14 Lockheed Aircraft Corp Coupled control surface for aircraft
US2940693A (en) * 1954-09-20 1960-06-14 Fairey Aviat Ltd Aircraft fins
DE3030728A1 (en) * 1980-08-14 1982-02-18 Dornier Gmbh, 7990 Friedrichshafen Steering gear, partic. rudders, for aircraft or missiles - use delta-wing fins outboard on elevator rotatable about two perpendicular axes

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2500689A (en) * 1945-02-05 1950-03-14 Lockheed Aircraft Corp Coupled control surface for aircraft
US2940693A (en) * 1954-09-20 1960-06-14 Fairey Aviat Ltd Aircraft fins
DE3030728A1 (en) * 1980-08-14 1982-02-18 Dornier Gmbh, 7990 Friedrichshafen Steering gear, partic. rudders, for aircraft or missiles - use delta-wing fins outboard on elevator rotatable about two perpendicular axes

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