JPH11510127A - 回転翼航空機の回転運動の制御及び自動安定用のシステム - Google Patents
回転翼航空機の回転運動の制御及び自動安定用のシステムInfo
- Publication number
- JPH11510127A JPH11510127A JP9507788A JP50778897A JPH11510127A JP H11510127 A JPH11510127 A JP H11510127A JP 9507788 A JP9507788 A JP 9507788A JP 50778897 A JP50778897 A JP 50778897A JP H11510127 A JPH11510127 A JP H11510127A
- Authority
- JP
- Japan
- Prior art keywords
- gyro
- rotor
- thrust
- rotation
- axis
- 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.)
- Ceased
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 |
---|---|---|---|
US155895P | 1995-07-27 | 1995-07-27 | |
US60/001,558 | 1995-07-27 | ||
US707995P | 1995-10-24 | 1995-10-24 | |
US60/007,079 | 1995-10-24 | ||
PCT/US1996/012322 WO1997005017A1 (fr) | 1995-07-27 | 1996-07-26 | Systeme de regulation et de stabilisation automatique du mouvement de giration d'un aeronef a voilure tournante |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH11510127A true JPH11510127A (ja) | 1999-09-07 |
Family
ID=26669193
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9507788A Ceased JPH11510127A (ja) | 1995-07-27 | 1996-07-26 | 回転翼航空機の回転運動の制御及び自動安定用のシステム |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0869901A4 (fr) |
JP (1) | JPH11510127A (fr) |
AU (1) | AU6763296A (fr) |
WO (1) | WO1997005017A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2022173053A (ja) * | 2021-05-05 | 2022-11-17 | エアバス ヘリコプターズ ドイチェランド ゲーエムベーハー | 周期的ピッチ角調整装置 |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2562938C1 (ru) * | 2014-04-29 | 2015-09-10 | Акционерное общество "Московский вертолетный завод им. М.Л. Миля" | Одновинтовой вертолет и способ управления им |
WO2016109004A2 (fr) * | 2014-12-19 | 2016-07-07 | Sikorsky Aircraft Corporation | Liaison en ciseaux réglable |
US11040785B2 (en) * | 2018-04-16 | 2021-06-22 | Bell Helicopter Textron Inc. | Devices and methods to verify tail rotor cross-head positioning |
CN111470033B (zh) * | 2020-05-14 | 2023-05-16 | 芜湖丽勤光电技术有限公司 | 一种小型飞机尾部平衡装置 |
CN112594131B (zh) * | 2020-11-26 | 2022-04-26 | 中国船舶重工集团海装风电股份有限公司 | 一种风力发电机组侧风偏航控制方法、系统及相关组件 |
CN113815854B (zh) * | 2021-10-29 | 2024-06-11 | 湖南韬讯航空科技有限公司 | 一种飞行器旋翼系统及控制方法 |
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 (ja) * | 1977-09-06 | 1983-01-18 | マブチモ−タ−株式会社 | ヘリコプタ模型装置 |
US4759514A (en) | 1986-09-30 | 1988-07-26 | The Boeing Company | Tail rotor yaw position control for a helicopter |
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 |
US5597138A (en) | 1991-09-30 | 1997-01-28 | Arlton; Paul E. | Yaw control and stabilization system for helicopters |
-
1996
- 1996-07-26 EP EP96928019A patent/EP0869901A4/fr not_active Ceased
- 1996-07-26 AU AU67632/96A patent/AU6763296A/en not_active Abandoned
- 1996-07-26 WO PCT/US1996/012322 patent/WO1997005017A1/fr not_active Application Discontinuation
- 1996-07-26 JP JP9507788A patent/JPH11510127A/ja not_active Ceased
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2022173053A (ja) * | 2021-05-05 | 2022-11-17 | エアバス ヘリコプターズ ドイチェランド ゲーエムベーハー | 周期的ピッチ角調整装置 |
Also Published As
Publication number | Publication date |
---|---|
EP0869901A4 (fr) | 2000-10-04 |
AU6763296A (en) | 1997-02-26 |
WO1997005017A1 (fr) | 1997-02-13 |
EP0869901A1 (fr) | 1998-10-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20041026 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20050126 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20050328 |
|
A313 | Final decision of rejection without a dissenting response from the applicant |
Free format text: JAPANESE INTERMEDIATE CODE: A313 Effective date: 20050606 |
|
A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20050712 |