DE2226701A1 - Steuersystem für Vtol- oder V/Stol-Flugzeuge - Google Patents
Steuersystem für Vtol- oder V/Stol-FlugzeugeInfo
- Publication number
- DE2226701A1 DE2226701A1 DE19722226701 DE2226701A DE2226701A1 DE 2226701 A1 DE2226701 A1 DE 2226701A1 DE 19722226701 DE19722226701 DE 19722226701 DE 2226701 A DE2226701 A DE 2226701A DE 2226701 A1 DE2226701 A1 DE 2226701A1
- Authority
- DE
- Germany
- Prior art keywords
- control
- control system
- transducers
- pilot
- movements
- 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.)
- Pending
Links
- 230000033001 locomotion Effects 0.000 claims description 37
- 239000003381 stabilizer Substances 0.000 claims description 8
- 241000985905 Candidatus Phytoplasma solani Species 0.000 claims description 6
- 230000005484 gravity Effects 0.000 claims description 3
- 230000008878 coupling Effects 0.000 claims 2
- 238000010168 coupling process Methods 0.000 claims 2
- 238000005859 coupling reaction Methods 0.000 claims 2
- 230000000694 effects Effects 0.000 description 3
- 238000012546 transfer Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 241000239290 Araneae Species 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 230000011664 signaling Effects 0.000 description 1
- 238000012549 training Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0091—Accessories not provided for elsewhere
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Mechanical Control Devices (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1765271 | 1971-05-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE2226701A1 true DE2226701A1 (de) | 1972-12-07 |
Family
ID=10098904
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19722226701 Pending DE2226701A1 (de) | 1971-05-27 | 1972-05-25 | Steuersystem für Vtol- oder V/Stol-Flugzeuge |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3785596A (enExample) |
| DE (1) | DE2226701A1 (enExample) |
| FR (1) | FR2139119A1 (enExample) |
| GB (1) | GB1323997A (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118859975A (zh) * | 2024-09-24 | 2024-10-29 | 成都飞机工业（集团）有限责任公司 | 一种垂直起降无人机水平模态转换垂直模态的控制方法 |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4431149A (en) * | 1982-02-11 | 1984-02-14 | The United States Of America As Represented By The Secretary Of The Air Force | Geared tab |
| US5056742A (en) * | 1987-11-13 | 1991-10-15 | The Boeing Company | Modular rudder pedal and brake control assembly for aircraft |
| FR2678577B1 (fr) * | 1991-07-03 | 1993-10-22 | Aerospatiale Ste Nationale Indle | Dispositif pour le reglage des efforts de manóoeuvre d'organes mobiles d'aeronef. |
| US5527004A (en) * | 1993-02-24 | 1996-06-18 | Helix Air, Inc. | Control system for aircraft |
| SE518099C2 (sv) * | 1997-11-21 | 2002-08-27 | Claes Johansson Automotive Ab | Inställbart pedalställ för ett fordon |
| US6648268B2 (en) * | 2002-02-13 | 2003-11-18 | Dupont Anthony A. | Control system for vertical take off and land (VTOL) aircraft |
| US6776376B2 (en) | 2002-10-18 | 2004-08-17 | Hamilton Sunstrand | Flight control surface actuation system |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3341154A (en) * | 1963-08-01 | 1967-09-12 | Smith & Sons Ltd S | Control systems for aircraft engine installations |
| GB1104721A (en) * | 1963-08-26 | 1968-02-28 | Hawker Siddeley Aviation Ltd | Improvements in aircraft controls |
| US3388878A (en) * | 1965-06-01 | 1968-06-18 | Ryan Aeronautical Co | Vtol aircraft with balanced power, retractible lift fan system |
| US3485463A (en) * | 1968-05-21 | 1969-12-23 | Sperry Rand Corp | Control stick transducer |
-
1971
- 1971-05-27 GB GB1765271A patent/GB1323997A/en not_active Expired
-
1972
- 1972-05-25 DE DE19722226701 patent/DE2226701A1/de active Pending
- 1972-05-26 FR FR7218848A patent/FR2139119A1/fr not_active Withdrawn
- 1972-05-26 US US00257077A patent/US3785596A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118859975A (zh) * | 2024-09-24 | 2024-10-29 | 成都飞机工业（集团）有限责任公司 | 一种垂直起降无人机水平模态转换垂直模态的控制方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1323997A (en) | 1973-07-18 |
| US3785596A (en) | 1974-01-15 |
| FR2139119A1 (enExample) | 1973-01-05 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OHJ | Non-payment of the annual fee |