AU7987698A - Horizontal stabilizer for rotorcraft - Google Patents

Horizontal stabilizer for rotorcraft

Info

Publication number: AU7987698A
Authority: AU; Australia
Prior art keywords: rotorcraft; horizontal stabilizer; stabilizer; horizontal
Prior art date: 1998-06-25
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.)

1998-06-25

Filing date

1998-06-25

Publication date

2000-01-10

1998-06-25 Application filed by Sikorsky Aircraft Corp filed Critical Sikorsky Aircraft Corp

2000-01-10 Publication of AU7987698A publication Critical patent/AU7987698A/en

Status Abandoned legal-status Critical Current

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

1998
- 1998-06-25 AU AU79876/98A patent/AU7987698A/en not_active Abandoned
- 1998-06-25 WO PCT/US1998/013192 patent/WO1999067130A1/en active Application Filing

Also Published As

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

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Legal Events

Date	Code	Title	Description
2001-03-15	MK6	Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase