FR1536732A - Perfectionnements aux aéronefs combinés - Google Patents

Perfectionnements aux aéronefs combinés

Info

Publication number
FR1536732A
FR1536732A FR120814A FR120814A FR1536732A FR 1536732 A FR1536732 A FR 1536732A FR 120814 A FR120814 A FR 120814A FR 120814 A FR120814 A FR 120814A FR 1536732 A FR1536732 A FR 1536732A
Authority
FR
France
Prior art keywords
combined aircraft
aircraft
combined
aircraft improvements
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
FR120814A
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.)
Westland Group PLC
Original Assignee
Westland Aircraft Ltd
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 Westland Aircraft Ltd filed Critical Westland Aircraft Ltd
Priority to FR120814A priority Critical patent/FR1536732A/fr
Application granted granted Critical
Publication of FR1536732A publication Critical patent/FR1536732A/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/003Variable-diameter propellers; Mechanisms therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • B64C29/0033Aircraft 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)
  • Mechanical Engineering (AREA)
FR120814A 1967-09-13 1967-09-13 Perfectionnements aux aéronefs combinés Expired FR1536732A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR120814A FR1536732A (fr) 1967-09-13 1967-09-13 Perfectionnements aux aéronefs combinés

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR120814A FR1536732A (fr) 1967-09-13 1967-09-13 Perfectionnements aux aéronefs combinés

Publications (1)

Publication Number Publication Date
FR1536732A true FR1536732A (fr) 1968-08-16

Family

ID=8638221

Family Applications (1)

Application Number Title Priority Date Filing Date
FR120814A Expired FR1536732A (fr) 1967-09-13 1967-09-13 Perfectionnements aux aéronefs combinés

Country Status (1)

Country Link
FR (1) FR1536732A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993024365A1 (fr) * 1992-06-01 1993-12-09 United Technologies Corp. Rotor a diametre variable a torsion decalee

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993024365A1 (fr) * 1992-06-01 1993-12-09 United Technologies Corp. Rotor a diametre variable a torsion decalee

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