FR1212967A - Système de contrôle de vol - Google Patents

Système de contrôle de vol

Info

Publication number
FR1212967A
FR1212967A FR1212967DA FR1212967A FR 1212967 A FR1212967 A FR 1212967A FR 1212967D A FR1212967D A FR 1212967DA FR 1212967 A FR1212967 A FR 1212967A
Authority
FR
France
Prior art keywords
control system
flight control
flight
control
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)
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.)
Doak Aircraft Co Inc
Original Assignee
Doak Aircraft Co Inc
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 Doak Aircraft Co Inc filed Critical Doak Aircraft Co Inc
Application granted granted Critical
Publication of FR1212967A publication Critical patent/FR1212967A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1212967D 1958-10-18 1958-10-18 Système de contrôle de vol Expired FR1212967A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1212967T 1958-10-18

Publications (1)

Publication Number Publication Date
FR1212967A true FR1212967A (fr) 1960-03-28

Family

ID=9676323

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1212967D Expired FR1212967A (fr) 1958-10-18 1958-10-18 Système de contrôle de vol

Country Status (1)

Country Link
FR (1) FR1212967A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1220740B (de) * 1962-02-03 1966-07-07 Ver Flugtechnische Werke Ges M Steuergestaenge zum gleichsinnigen und zum gegensinnigen Verstellen zweier Glieder, insbesondere fuer ein in der Flachlage senkrecht starendes und landendes Flugzeug
DE1238340B (de) * 1961-04-20 1967-04-06 Gen Electric Senkrecht startendes Flugzeug mit zwei Turbinengeblaesen seitlich des Rumpfes

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1238340B (de) * 1961-04-20 1967-04-06 Gen Electric Senkrecht startendes Flugzeug mit zwei Turbinengeblaesen seitlich des Rumpfes
DE1238340C2 (de) * 1961-04-20 1967-10-19 Gen Electric Senkrecht startendes Flugzeug mit zwei Turbinengeblaesen seitlich des Rumpfes
DE1220740B (de) * 1962-02-03 1966-07-07 Ver Flugtechnische Werke Ges M Steuergestaenge zum gleichsinnigen und zum gegensinnigen Verstellen zweier Glieder, insbesondere fuer ein in der Flachlage senkrecht starendes und landendes Flugzeug

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