AU7987698A - Horizontal stabilizer for rotorcraft - Google Patents

Horizontal stabilizer for rotorcraft

Info

Publication number
AU7987698A
AU7987698A AU79876/98A AU7987698A AU7987698A AU 7987698 A AU7987698 A AU 7987698A AU 79876/98 A AU79876/98 A AU 79876/98A AU 7987698 A AU7987698 A AU 7987698A AU 7987698 A AU7987698 A AU 7987698A
Authority
AU
Australia
Prior art keywords
rotorcraft
horizontal stabilizer
stabilizer
horizontal
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.)
Abandoned
Application number
AU79876/98A
Inventor
James Richard Lamb
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.)
Sikorsky Aircraft Corp
Original Assignee
Sikorsky 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 Sikorsky Aircraft Corp filed Critical Sikorsky Aircraft Corp
Publication of AU7987698A publication Critical patent/AU7987698A/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
    • B64C2027/8281—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
AU79876/98A 1998-06-25 1998-06-25 Horizontal stabilizer for rotorcraft Abandoned AU7987698A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1998/013192 WO1999067130A1 (en) 1998-06-25 1998-06-25 Horizontal stabilizer for rotorcraft

Publications (1)

Publication Number Publication Date
AU7987698A true AU7987698A (en) 2000-01-10

Family

ID=22267367

Family Applications (1)

Application Number Title Priority Date Filing Date
AU79876/98A Abandoned AU7987698A (en) 1998-06-25 1998-06-25 Horizontal stabilizer for rotorcraft

Country Status (2)

Country Link
AU (1) AU7987698A (en)
WO (1) WO1999067130A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108100231B (en) * 2017-12-01 2021-05-11 中国直升机设计研究所 Horizontal tail joint of helicopter
CN108839814B (en) * 2018-06-13 2021-07-02 江西昌河航空工业有限公司 Device for dismounting and replacing tail beam joint of helicopter
PL3730403T3 (en) 2019-04-26 2022-09-05 Airbus Helicopters Deutschland GmbH A helicopter with a stabilizer wing
RU2743306C1 (en) * 2020-10-19 2021-02-16 Эйрбас Хеликоптерс Дойчланд Гмбх Rotary-winged aircraft with stabilizer wing

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2167249B1 (en) * 1972-01-11 1974-06-21 Aerospatiale
US4103848A (en) 1977-03-08 1978-08-01 United Technologies Corporation Variable incidence helicopter stabilator and fail safe actuator
US4247061A (en) 1978-07-12 1981-01-27 United Technologies Corporation Helicopter with stabilator detuned in antisymmetric vibration modes from main rotor wake excitation frequency
FR2600036B1 (en) * 1986-06-16 1988-09-16 Aerospatiale DIRECTIONAL DEVICE AND STABILIZER WITH ANTI-TORQUE HULL AND INCLINED ROTOR AND WITH A “V” DIFFERENTIAL TAKING, AND HELICOPTER EQUIPPED WITH SUCH A DEVICE.
US5102067A (en) 1991-04-11 1992-04-07 United Technologies Corporation Integrated helicopter empennage structure

Also Published As

Publication number Publication date
WO1999067130A1 (en) 1999-12-29

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase