FR1536412A - Tail rotor pivot control mechanism of a convertiplane - Google Patents

Tail rotor pivot control mechanism of a convertiplane

Info

Publication number
FR1536412A
FR1536412A FR113314A FR113314A FR1536412A FR 1536412 A FR1536412 A FR 1536412A FR 113314 A FR113314 A FR 113314A FR 113314 A FR113314 A FR 113314A FR 1536412 A FR1536412 A FR 1536412A
Authority
FR
France
Prior art keywords
convertiplane
control mechanism
tail rotor
pivot control
rotor pivot
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
FR113314A
Other languages
French (fr)
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Priority to FR113314A priority Critical patent/FR1536412A/en
Application granted granted Critical
Publication of FR1536412A publication Critical patent/FR1536412A/en
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
    • B64C29/0091—Accessories not provided for elsewhere
    • 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
    • B64C13/02—Initiating means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
FR113314A 1967-07-06 1967-07-06 Tail rotor pivot control mechanism of a convertiplane Expired FR1536412A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR113314A FR1536412A (en) 1967-07-06 1967-07-06 Tail rotor pivot control mechanism of a convertiplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR113314A FR1536412A (en) 1967-07-06 1967-07-06 Tail rotor pivot control mechanism of a convertiplane

Publications (1)

Publication Number Publication Date
FR1536412A true FR1536412A (en) 1968-08-16

Family

ID=8634597

Family Applications (1)

Application Number Title Priority Date Filing Date
FR113314A Expired FR1536412A (en) 1967-07-06 1967-07-06 Tail rotor pivot control mechanism of a convertiplane

Country Status (1)

Country Link
FR (1) FR1536412A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2407377A1 (en) 2010-07-13 2012-01-18 Eurocopter Method and aircraft equipped with a tiltable rear rotor
EP2468627A1 (en) 2010-12-22 2012-06-27 Eurocopter Aircraft provided with a tilting rear rotor and associated method

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2407377A1 (en) 2010-07-13 2012-01-18 Eurocopter Method and aircraft equipped with a tiltable rear rotor
FR2962713A1 (en) * 2010-07-13 2012-01-20 Eurocopter France METHOD AND AIRCRAFT PROVIDED WITH A BACK-UP ROTOR
US8777152B2 (en) 2010-07-13 2014-07-15 Airbus Helicopters Method and an aircraft provided with a swiveling tail rotor
EP2468627A1 (en) 2010-12-22 2012-06-27 Eurocopter Aircraft provided with a tilting rear rotor and associated method
US8763949B2 (en) 2010-12-22 2014-07-01 Airbus Helicopters Aircraft provided with a swiveling tail rotor, and an associated method

Similar Documents

Publication Publication Date Title
FR1507701A (en) Control mechanism for vanes
FR1505127A (en) Helicopter rotor control device
FR1536412A (en) Tail rotor pivot control mechanism of a convertiplane
FR1449045A (en) Position control device of a phonographic arm
CH440203A (en) Control device of a dryer
CH473504A (en) Control device of a static converter
FR1414040A (en) Aircraft tail horizontal plane control mechanism
FR1320786A (en) Elevator control
FR1467144A (en) Hydro-electronic notcher divider control device
CH487358A (en) Stepping mechanism
FR1460643A (en) Elevator control device
FR1545170A (en) Control mechanism of a switch
FR1539389A (en) Control device for the slow rotation of a shaft
CA755896A (en) Speed control mechanism
FR89040E (en) Elevator control device
FR1526264A (en) Mechanism for positioning a sample
FR1541241A (en) Winding control
FR1542247A (en) Control mechanism of an advancing device
FR1481917A (en) Servo-mechanism for controlling a movement
FR1523341A (en) Automatic watering control
FR1505375A (en) Shaft position digital control mechanism
FR1536772A (en) Drive mechanism
FR1468087A (en) Attitude control by radiation
AU286774B2 (en) A photographic shutter having fast and slow speed escapement mechanism
FR1409614A (en) Device for flexible assembly of control rods