AU6763296A - System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft - Google Patents
System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraftInfo
- Publication number
- AU6763296A AU6763296A AU67632/96A AU6763296A AU6763296A AU 6763296 A AU6763296 A AU 6763296A AU 67632/96 A AU67632/96 A AU 67632/96A AU 6763296 A AU6763296 A AU 6763296A AU 6763296 A AU6763296 A AU 6763296A
- Authority
- AU
- Australia
- Prior art keywords
- controlling
- rotational motion
- wing aircraft
- rotary wing
- automatically stabilizing
- 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
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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US007079 | 1987-01-27 | ||
US155895P | 1995-07-27 | 1995-07-27 | |
US001558 | 1995-07-27 | ||
US707995P | 1995-10-24 | 1995-10-24 | |
PCT/US1996/012322 WO1997005017A1 (en) | 1995-07-27 | 1996-07-26 | System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
AU6763296A true AU6763296A (en) | 1997-02-26 |
Family
ID=26669193
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU67632/96A Abandoned AU6763296A (en) | 1995-07-27 | 1996-07-26 | System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0869901A4 (en) |
JP (1) | JPH11510127A (en) |
AU (1) | AU6763296A (en) |
WO (1) | WO1997005017A1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2562938C1 (en) * | 2014-04-29 | 2015-09-10 | Акционерное общество "Московский вертолетный завод им. М.Л. Миля" | Single-rotor helicopter and method of its control |
US10752348B2 (en) | 2014-12-19 | 2020-08-25 | Sikorsky Aircraft Corporation | Adjustable scissor link |
US11040785B2 (en) * | 2018-04-16 | 2021-06-22 | Bell Helicopter Textron Inc. | Devices and methods to verify tail rotor cross-head positioning |
CN111470033B (en) * | 2020-05-14 | 2023-05-16 | 芜湖丽勤光电技术有限公司 | Small aircraft tail balancing device |
CN112594131B (en) * | 2020-11-26 | 2022-04-26 | 中国船舶重工集团海装风电股份有限公司 | Method and system for controlling yaw of wind generating set during crosswind and related components |
EP4086171B1 (en) * | 2021-05-05 | 2023-11-22 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A cyclic pitch angle adjustment apparatus |
CN113815854B (en) * | 2021-10-29 | 2024-06-11 | 湖南韬讯航空科技有限公司 | Aircraft rotor system and control method |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2689099A (en) * | 1951-09-20 | 1954-09-14 | United Aircraft Corp | Triangular stabilizer for rotary wing aircraft |
GB751837A (en) * | 1954-02-01 | 1956-07-04 | Carlo Lualdi | Gyroscopic device for stabilizing the rotors of helicopters |
US3027948A (en) * | 1958-01-24 | 1962-04-03 | Kellett Aircraft Corp | Stabilization of rotary wing aircraft |
US3004736A (en) | 1959-10-06 | 1961-10-17 | Lockheed Aircraft Corp | Tail rotor for helicopter |
US3211235A (en) * | 1964-02-17 | 1965-10-12 | Enstrom Corp | Control system for yaw control rotors of helicopters |
US3528633A (en) * | 1967-11-14 | 1970-09-15 | Siegfried Knemeyer | System for controlling and stabilizing an aircraft in yaw |
JPS582706B2 (en) * | 1977-09-06 | 1983-01-18 | マブチモ−タ−株式会社 | helicopter model equipment |
US4759514A (en) | 1986-09-30 | 1988-07-26 | The Boeing Company | Tail rotor yaw position control for a helicopter |
US5597138A (en) | 1991-09-30 | 1997-01-28 | Arlton; Paul E. | Yaw control and stabilization system for helicopters |
US5609312A (en) | 1991-09-30 | 1997-03-11 | Arlton; Paul E. | Model helicopter |
US5628620A (en) | 1991-09-30 | 1997-05-13 | Arlton; Paul E. | Main rotor system for helicopters |
US5305968A (en) | 1991-09-30 | 1994-04-26 | Arlton Paul E | Device for automatically stabilizing the yaw motion of a helicopter |
-
1996
- 1996-07-26 JP JP9507788A patent/JPH11510127A/en not_active Ceased
- 1996-07-26 EP EP96928019A patent/EP0869901A4/en not_active Ceased
- 1996-07-26 AU AU67632/96A patent/AU6763296A/en not_active Abandoned
- 1996-07-26 WO PCT/US1996/012322 patent/WO1997005017A1/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP0869901A1 (en) | 1998-10-14 |
JPH11510127A (en) | 1999-09-07 |
EP0869901A4 (en) | 2000-10-04 |
WO1997005017A1 (en) | 1997-02-13 |
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