CH489390A - Aéronef comprenant un dispositif de propulsion et de sustentation par réaction combiné - Google Patents
Aéronef comprenant un dispositif de propulsion et de sustentation par réaction combinéInfo
- Publication number
- CH489390A CH489390A CH776268A CH776268A CH489390A CH 489390 A CH489390 A CH 489390A CH 776268 A CH776268 A CH 776268A CH 776268 A CH776268 A CH 776268A CH 489390 A CH489390 A CH 489390A
- Authority
- CH
- Switzerland
- Prior art keywords
- aircraft
- lift device
- combined reaction
- reaction propulsion
- propulsion
- Prior art date
Links
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
- B64C29/0008—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
- B64C29/0041—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 jet motors
- B64C29/005—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 jet motors the motors being fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- 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
- B64C29/0041—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 jet motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR107669A FR1548297A (fr) | 1967-05-24 | 1967-05-24 | |
FR141237A FR94023E (fr) | 1967-05-24 | 1968-02-26 | Systeme sustentateur ou propulso sustentateur pour aéronefs. |
Publications (1)
Publication Number | Publication Date |
---|---|
CH489390A true CH489390A (fr) | 1970-04-30 |
Family
ID=26176744
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH776268A CH489390A (fr) | 1967-05-24 | 1968-05-24 | Aéronef comprenant un dispositif de propulsion et de sustentation par réaction combiné |
Country Status (6)
Country | Link |
---|---|
US (1) | US3545701A (fr) |
BE (1) | BE715615A (fr) |
CH (1) | CH489390A (fr) |
DE (1) | DE1756465C3 (fr) |
FR (1) | FR94023E (fr) |
GB (1) | GB1212743A (fr) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3666209A (en) * | 1970-02-24 | 1972-05-30 | Boeing Co | V/stol aircraft with variable tilt wing |
US3770227A (en) * | 1971-09-10 | 1973-11-06 | Us Air Force | Jet wing with multiple thrust augmentors |
US3830451A (en) * | 1973-06-28 | 1974-08-20 | Rockwell International Corp | Aircraft control system |
US3860200A (en) * | 1973-09-05 | 1975-01-14 | Rockwell International Corp | Airfoil |
US4017041A (en) * | 1976-01-12 | 1977-04-12 | Nelson Wilbur C | Airfoil tip vortex control |
US4442986A (en) * | 1982-08-30 | 1984-04-17 | The United States Of America As Represented By The Secretary Of The Navy | Leading edge augmentor wing-in-ground effect vehicle |
US5076512A (en) * | 1989-02-08 | 1991-12-31 | Boeing Canada Ltd. | Ventral segmented nozzles for promoting rapid temperature and pressure decay |
US5062588A (en) * | 1989-02-08 | 1991-11-05 | Boeing Of Canada Ltd. | Segmented rotatable nozzles |
GB0301370D0 (en) * | 2003-01-22 | 2003-02-19 | Secr Defence | A wing for a compound helicopter |
DE10313729B4 (de) * | 2003-03-27 | 2007-11-29 | Airbus Deutschland Gmbh | Luftauslaßventil für ein Flugzeug |
US20050116087A1 (en) * | 2003-06-11 | 2005-06-02 | Page John S.Jr. | Aircraft converts drag to lift |
US20080230656A1 (en) * | 2006-04-11 | 2008-09-25 | Moshe Kretchmer | Aircraft wings having hinged vanes and aircraft having said wings |
FR2911116B1 (fr) * | 2007-01-05 | 2009-02-06 | Airbus France Sas | Dispositif de sortie d'air pour un aeronef |
FR2915733B1 (fr) * | 2007-05-04 | 2009-06-05 | Airbus France Sas | Dispositif de sortie d'air mobile pour un aeronef |
US8336828B2 (en) * | 2009-11-12 | 2012-12-25 | The Boeing Company | Traversing jet actuator |
FR2990926B1 (fr) * | 2012-05-22 | 2014-11-28 | Eurocopter France | Moyen de stabilisation en tangage et aeronef a voilure tournante muni d'un tel moyen |
US10370100B2 (en) * | 2015-03-24 | 2019-08-06 | United States Of America As Represented By The Administrator Of Nasa | Aerodynamically actuated thrust vectoring devices |
USD868627S1 (en) | 2018-04-27 | 2019-12-03 | Jetoptera, Inc. | Flying car |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
CA3216288A1 (fr) | 2015-09-02 | 2017-04-20 | Jetoptera, Inc. | Configurations d'ejecteur et de profil areodynamique |
US10669026B2 (en) * | 2016-04-01 | 2020-06-02 | Albert Aguilar | Lift cell modules and lift pods |
US10315754B2 (en) | 2016-06-10 | 2019-06-11 | Coflow Jet, LLC | Fluid systems that include a co-flow jet |
US10106246B2 (en) | 2016-06-10 | 2018-10-23 | Coflow Jet, LLC | Fluid systems that include a co-flow jet |
CN106628171A (zh) * | 2016-12-01 | 2017-05-10 | 向仲宇 | 一种分割式可改变扑翼面积的扑翼飞行器 |
EP3684687B1 (fr) * | 2017-09-22 | 2023-05-24 | AMSL Innovations Pty Ltd | Système d'actionnement d'inclinaison pour aéronef à décollage et atterrissage verticaux (adav) |
US10683076B2 (en) | 2017-10-31 | 2020-06-16 | Coflow Jet, LLC | Fluid systems that include a co-flow jet |
US11293293B2 (en) | 2018-01-22 | 2022-04-05 | Coflow Jet, LLC | Turbomachines that include a casing treatment |
US11111025B2 (en) | 2018-06-22 | 2021-09-07 | Coflow Jet, LLC | Fluid systems that prevent the formation of ice |
GB2600584B (en) | 2019-07-23 | 2024-03-06 | Coflow Jet Llc | Fluid systems and methods that address flow separation |
KR20220090243A (ko) * | 2020-12-22 | 2022-06-29 | 현대자동차주식회사 | 에어 모빌리티 |
-
1968
- 1968-02-26 FR FR141237A patent/FR94023E/fr not_active Expired
- 1968-05-24 CH CH776268A patent/CH489390A/fr not_active IP Right Cessation
- 1968-05-24 BE BE715615D patent/BE715615A/xx unknown
- 1968-05-24 US US731869A patent/US3545701A/en not_active Expired - Lifetime
- 1968-05-24 GB GB25023/68A patent/GB1212743A/en not_active Expired
- 1968-05-24 DE DE1756465A patent/DE1756465C3/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR94023E (fr) | 1969-06-20 |
DE1756465B2 (de) | 1973-03-29 |
DE1756465C3 (de) | 1973-10-18 |
BE715615A (fr) | 1968-11-25 |
US3545701A (en) | 1970-12-08 |
DE1756465A1 (de) | 1970-04-02 |
GB1212743A (en) | 1970-11-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PL | Patent ceased |