GB1149367A - Control apparatus for use in a v.t.o.l. aircraft - Google Patents
Control apparatus for use in a v.t.o.l. aircraftInfo
- Publication number
- GB1149367A GB1149367A GB25630/66A GB2563066A GB1149367A GB 1149367 A GB1149367 A GB 1149367A GB 25630/66 A GB25630/66 A GB 25630/66A GB 2563066 A GB2563066 A GB 2563066A GB 1149367 A GB1149367 A GB 1149367A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- units
- controls
- order
- inclination
- 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
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 2
- 229910052799 carbon Inorganic materials 0.000 abstract 2
- 230000004075 alteration Effects 0.000 abstract 1
- 238000012937 correction Methods 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000006247 magnetic powder Substances 0.000 abstract 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
-
- 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
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Preparation Of Clay, And Manufacture Of Mixtures Containing Clay Or Cement (AREA)
- Toys (AREA)
- Mechanical Control Devices (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR20342A FR1458961A (fr) | 1965-06-10 | 1965-06-10 | Dispositif de liaison pour machine volante à décollage et à atterrissage verticaux |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1149367A true GB1149367A (en) | 1969-04-23 |
Family
ID=8581578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB25630/66A Expired GB1149367A (en) | 1965-06-10 | 1966-06-08 | Control apparatus for use in a v.t.o.l. aircraft |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3393882A (enExample) |
| DE (1) | DE1481620A1 (enExample) |
| FR (1) | FR1458961A (enExample) |
| GB (1) | GB1149367A (enExample) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2700734B2 (ja) * | 1991-09-20 | 1998-01-21 | 川崎重工業株式会社 | 垂直離着陸航空機 |
| US5765783A (en) * | 1994-03-04 | 1998-06-16 | The Boeing Company | Vertically launchable and recoverable winged aircraft |
| US5727757A (en) * | 1996-01-17 | 1998-03-17 | Mcdonnell Douglas Helicopter Co. | Slotted cam control system |
| US6896221B1 (en) | 2003-04-16 | 2005-05-24 | Einar Einarsson | Vertical takeoff and landing aircraft |
| FR2864030B1 (fr) * | 2003-12-23 | 2006-02-17 | Eurocopter France | Aeronef convertible pourvu de deux "tilt fan" de part et d'autre du fuselage et d'un troisieme "tilt fan" agence sur la queue de l'aeronef |
| CN100503366C (zh) | 2004-07-29 | 2009-06-24 | 贝尔直升机泰克斯特龙公司 | 用于倾转旋翼飞行器飞行控制的方法和装置 |
| GB0422095D0 (en) * | 2004-10-05 | 2004-11-03 | Hardy Alexander S | Aircraft |
| US7658346B2 (en) * | 2005-02-25 | 2010-02-09 | Honeywell International Inc. | Double ducted hovering air-vehicle |
| US8074940B2 (en) * | 2007-08-08 | 2011-12-13 | Moog Inc. | Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein |
| FR2946318B1 (fr) * | 2009-06-04 | 2012-11-16 | Eurocopter France | Dispositif mecanique pour combiner un premier et un deuxieme ordres de commande,et aeronef muni d'un tel dispositif. |
| US9004393B2 (en) | 2010-10-24 | 2015-04-14 | University Of Kansas | Supersonic hovering air vehicle |
| FR3022217A1 (fr) * | 2014-06-12 | 2015-12-18 | Bermond Gerome | Aeronef convertible a aile basculante |
| US10107196B2 (en) | 2014-08-08 | 2018-10-23 | Thomas International, Inc. | Adjustable size inlet system |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3106369A (en) * | 1960-02-23 | 1963-10-08 | Curtiss Wright Corp | Aircraft and method of operating same |
| FR1292361A (fr) * | 1961-03-23 | 1962-05-04 | Snecma | Dispositif automatique de contrôle de transition pour avions décollant et atterrissant à la verticale |
-
1965
- 1965-06-10 FR FR20342A patent/FR1458961A/fr not_active Expired
-
1966
- 1966-06-06 US US555564A patent/US3393882A/en not_active Expired - Lifetime
- 1966-06-08 GB GB25630/66A patent/GB1149367A/en not_active Expired
- 1966-06-10 DE DE19661481620 patent/DE1481620A1/de active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US3393882A (en) | 1968-07-23 |
| FR1458961A (fr) | 1966-04-29 |
| DE1481620B2 (enExample) | 1969-03-27 |
| DE1481620A1 (de) | 1969-03-27 |
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