JPS5951479B2 - 双反転式ヒンジ無し回転翼を有する航空機の制御方法及び航空機 - Google Patents
双反転式ヒンジ無し回転翼を有する航空機の制御方法及び航空機Info
- Publication number
- JPS5951479B2 JPS5951479B2 JP51136816A JP13681676A JPS5951479B2 JP S5951479 B2 JPS5951479 B2 JP S5951479B2 JP 51136816 A JP51136816 A JP 51136816A JP 13681676 A JP13681676 A JP 13681676A JP S5951479 B2 JPS5951479 B2 JP S5951479B2
- Authority
- JP
- Japan
- Prior art keywords
- rotor
- aircraft
- axis
- moment
- tilting
- 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
Links
- 238000000034 method Methods 0.000 title claims description 8
- 230000033001 locomotion Effects 0.000 claims description 35
- 230000004044 response Effects 0.000 claims description 9
- 230000009471 action Effects 0.000 claims description 3
- 239000011295 pitch Substances 0.000 description 60
- 230000000737 periodic effect Effects 0.000 description 54
- 230000007246 mechanism Effects 0.000 description 18
- 239000013598 vector Substances 0.000 description 15
- 230000008859 change Effects 0.000 description 13
- 238000005452 bending Methods 0.000 description 9
- 230000008878 coupling Effects 0.000 description 6
- 238000010168 coupling process Methods 0.000 description 6
- 238000005859 coupling reaction Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 230000001133 acceleration Effects 0.000 description 4
- 238000001514 detection method Methods 0.000 description 4
- 206010034719 Personality change Diseases 0.000 description 3
- 125000004122 cyclic group Chemical group 0.000 description 3
- 238000011161 development Methods 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
- 201000009482 yaws Diseases 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/80—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement for differential adjustment of blade pitch between two or more lifting rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/631,599 US4027999A (en) | 1975-11-13 | 1975-11-13 | Analog mixer to vary helicopter rotor phase angle in flight |
| US05/631,600 US4008979A (en) | 1975-11-13 | 1975-11-13 | Control for helicopter having dual rigid rotors |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5262898A JPS5262898A (en) | 1977-05-24 |
| JPS5951479B2 true JPS5951479B2 (ja) | 1984-12-14 |
Family
ID=27091437
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP51136816A Expired JPS5951479B2 (ja) | 1975-11-13 | 1976-11-12 | 双反転式ヒンジ無し回転翼を有する航空機の制御方法及び航空機 |
Country Status (7)
| Country | Link |
|---|---|
| JP (1) | JPS5951479B2 (fa) |
| BR (1) | BR7607626A (fa) |
| DE (1) | DE2651577C2 (fa) |
| FR (1) | FR2331479A1 (fa) |
| GB (1) | GB1519380A (fa) |
| IL (1) | IL50878A (fa) |
| IT (1) | IT1064383B (fa) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6369482U (fa) * | 1986-10-24 | 1988-05-10 |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19627869A1 (de) * | 1996-07-11 | 1998-01-15 | Zf Luftfahrttechnik Gmbh | Hubschrauber |
| DE102007002586A1 (de) | 2007-01-12 | 2008-07-24 | Rotorfly Ltd. | Rotorsystem |
| US9315265B2 (en) | 2013-07-29 | 2016-04-19 | Sikorsky Aircraft Corporation | Adjustable scissor control link |
| WO2015152912A1 (en) * | 2014-04-02 | 2015-10-08 | Sikorsky Aircraft Corporation | Rotor phasing control |
| CN117419885B (zh) * | 2023-12-19 | 2024-03-19 | 中国空气动力研究与发展中心低速空气动力研究所 | 一种剪刀式尾桨风洞试验台 |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2427936A (en) * | 1943-09-18 | 1947-09-23 | Jr Nathaniel B Wales | Control mechanism for helicopters having coaxial counterrotating rotors |
| FR995459A (fr) * | 1945-03-06 | 1951-12-03 | Procédé et dispositif permettant d'améliorer la maniabilité des appareils d'aviation à voilures tournantes articulées | |
| US2748876A (en) * | 1951-01-12 | 1956-06-05 | Vertol Aircraft Corp | Means for controlling tip-path of rotors |
| US3409248A (en) * | 1965-10-22 | 1968-11-05 | Harvard J. Bryan | Rotary winged aircraft with drag propelling rotors and controls |
| US3409249A (en) * | 1966-06-29 | 1968-11-05 | United Aircraft Corp | Coaxial rigid rotor helicopter and method of flying same |
| FR1534974A (fr) * | 1967-06-28 | 1968-08-02 | United Aircraft Corp | Perfectionnements apportés aux hélicoptères à rotors coaxiaux rigides et aux méthodes de pilotage de tels hélicoptères |
| US3521971A (en) * | 1968-07-17 | 1970-07-28 | United Aircraft Corp | Method and apparatus for controlling aircraft |
| US3570786A (en) * | 1969-08-07 | 1971-03-16 | United Aircraft Corp | Control apparatus and method for operating an aircraft |
| JPS5614519B1 (fa) * | 1971-04-06 | 1981-04-04 |
-
1976
- 1976-10-26 GB GB44425/76A patent/GB1519380A/en not_active Expired
- 1976-11-10 IL IL50878A patent/IL50878A/xx unknown
- 1976-11-11 BR BR7607626A patent/BR7607626A/pt unknown
- 1976-11-12 JP JP51136816A patent/JPS5951479B2/ja not_active Expired
- 1976-11-12 FR FR7634098A patent/FR2331479A1/fr active Granted
- 1976-11-12 IT IT29285/76A patent/IT1064383B/it active
- 1976-11-12 DE DE2651577A patent/DE2651577C2/de not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6369482U (fa) * | 1986-10-24 | 1988-05-10 |
Also Published As
| Publication number | Publication date |
|---|---|
| IL50878A (en) | 1980-01-31 |
| GB1519380A (en) | 1978-07-26 |
| JPS5262898A (en) | 1977-05-24 |
| IT1064383B (it) | 1985-02-18 |
| DE2651577C2 (de) | 1986-07-31 |
| FR2331479A1 (fr) | 1977-06-10 |
| DE2651577A1 (de) | 1977-05-26 |
| FR2331479B1 (fa) | 1983-02-11 |
| BR7607626A (pt) | 1977-09-27 |
| IL50878A0 (en) | 1977-01-31 |
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