ES2008200A6 - Disposicion sustentadora por accion directa del flujo de los motores para aeronaves de despegue vertical. - Google Patents
Disposicion sustentadora por accion directa del flujo de los motores para aeronaves de despegue vertical.Info
- Publication number
- ES2008200A6 ES2008200A6 ES8702544A ES8702544A ES2008200A6 ES 2008200 A6 ES2008200 A6 ES 2008200A6 ES 8702544 A ES8702544 A ES 8702544A ES 8702544 A ES8702544 A ES 8702544A ES 2008200 A6 ES2008200 A6 ES 2008200A6
- Authority
- ES
- Spain
- Prior art keywords
- aircraft
- aeroplane
- counteract
- flight
- engine
- 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
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
- B64C29/0075—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 tiltable relative to the fuselage
Abstract
DISPOSICION SUSTENTADORA POR ACCION DIRECTA DEL FLUJO DE LOS MOTORES PARA AERONAVES DE DESPEGUE VERTICAL, QUE APLICA DIRECTAMENTE LA TRACCION DE LOS MOTORES SIN LA INTERVENCION DE LAS ALAS. EL EJE O VECTOR DE FUERZA APLICADO TIENE LA MISMA INTENSIDAD, DIRECCION Y SENTIDO QUE LA RESULTANTE SUMA VECTORIAL DE LAS FUERZAS NECESARIAS PARA MOVER LA AERONAVE Y ES IGUAL Y OPUESTO A LA RESULTANTE DE LA SUMA DE LAS RESISTENCIAS QUE HAY QUE VENCER Y QUE SON EL PESO Y LA RESISTENCIA TOTAL AL AVANCE EN EL AIRE; ASIMISMO, SE PUEDE APLICAR LAS FUERZAS POR SEPARADO UNA PARA CONTRARRESTAR EL PESO Y LA OTRA LA RESISTENCIA TOTAL AL AVANCE. LOS MOTORES GIRARAN ALREDEDOR DEL EJE TRANSVERSAL DEL AVION MOVIDOS POR MEDIO DE UNOS MARTINETES HIDRAULICOS O BIEN POR MEDIO DE MOTORES ELECTRICOS O HIDRAULICOS Y UN SISTEMA DE ENGRANAJES.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES8702544A ES2008200A6 (es) | 1987-09-02 | 1987-09-02 | Disposicion sustentadora por accion directa del flujo de los motores para aeronaves de despegue vertical. |
DE19883829329 DE3829329A1 (de) | 1987-09-02 | 1988-08-30 | Tragvorrichtung fuer senkrecht startende luftfahrzeuge auf grund der direkten wirkung des stroms der motoren |
FR8811410A FR2619786A1 (fr) | 1987-09-02 | 1988-08-31 | Disposition de sustentation par action directe du flux des moteurs pour aeronefs a decollage vertical |
GB8820733A GB2209314A (en) | 1987-09-02 | 1988-09-02 | Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES8702544A ES2008200A6 (es) | 1987-09-02 | 1987-09-02 | Disposicion sustentadora por accion directa del flujo de los motores para aeronaves de despegue vertical. |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2008200A6 true ES2008200A6 (es) | 1989-07-16 |
Family
ID=8252374
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES8702544A Expired ES2008200A6 (es) | 1987-09-02 | 1987-09-02 | Disposicion sustentadora por accion directa del flujo de los motores para aeronaves de despegue vertical. |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE3829329A1 (es) |
ES (1) | ES2008200A6 (es) |
FR (1) | FR2619786A1 (es) |
GB (1) | GB2209314A (es) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2119603A1 (es) * | 1994-11-03 | 1998-10-01 | Saiz Manuel Munoz | Sistema de propulsion y estabilizacion para aviones de despegue vertical. |
ES2293818A1 (es) * | 2006-02-09 | 2008-03-16 | Manuel Muñoz Saiz | Sistema sustentador y propulsor para aeronaves de despegue y aterrizaje vertical. |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2332892A (en) * | 1997-08-08 | 1999-07-07 | Mark Alexander Roberts | Hovering craft with ducted fans |
US6254032B1 (en) | 1999-10-26 | 2001-07-03 | Franz Bucher | Aircraft and method for operating an aircraft |
GB2359052B (en) * | 2000-02-09 | 2003-09-17 | Rolls Royce Plc | Engine arrangement |
US6886776B2 (en) | 2001-10-02 | 2005-05-03 | Karl F. Milde, Jr. | VTOL personal aircraft |
GB2389826B (en) * | 2002-06-22 | 2006-08-23 | John Edward Randell | Craft propulsion |
GB2409845A (en) * | 2004-01-08 | 2005-07-13 | Robert Graham Burrage | Tilt-rotor aircraft changeable between vertical lift and forward flight modes |
DE102011015780A1 (de) * | 2011-04-01 | 2012-10-04 | Lfk-Lenkflugkörpersysteme Gmbh | Kleinflugkörper |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB383494A (es) * | ||||
GB383497A (en) * | 1931-09-24 | 1932-11-17 | Louis Marmonier | Flight device evolved from the ordinary aeroplane and the helicopter |
GB788314A (en) * | 1954-09-27 | 1957-12-23 | Harold Arthur Howard | Improvements in jet-propelled aircraft |
GB828884A (en) * | 1954-12-21 | 1960-02-24 | Boulton Aircraft Ltd | Improvements in or relating to aircraft |
GB860497A (en) * | 1958-05-02 | 1961-02-08 | Daimler Benz Ag | Improvements relating to turbo-jet propulsion units in aircraft |
GB984955A (en) * | 1964-01-22 | 1965-03-03 | Rolls Royce | Nozzle for a jet engine |
GB1085459A (en) * | 1966-03-03 | 1967-10-04 | Arthur Paul Pedrick | Improvements in gas turbine jet engines particularly for vertical take off and landing delta wing sub and supersonic aircraft |
GB1111845A (en) * | 1967-04-14 | 1968-05-01 | Arthur Paul Pedrick | Improvements in hypersonic vtol aircraft |
GB1335771A (en) * | 1972-06-12 | 1973-10-31 | Pedrick A P | Vertical take off and landing wingless aircraft |
DE2527497A1 (de) * | 1975-06-20 | 1976-12-30 | Ver Flugtechnische Werke | Vtol-fluggeraet |
SE450480B (sv) * | 1982-08-30 | 1987-06-29 | Tech Gerete Und Entwicklungsge | Styvvingad flygkropp |
-
1987
- 1987-09-02 ES ES8702544A patent/ES2008200A6/es not_active Expired
-
1988
- 1988-08-30 DE DE19883829329 patent/DE3829329A1/de not_active Withdrawn
- 1988-08-31 FR FR8811410A patent/FR2619786A1/fr not_active Withdrawn
- 1988-09-02 GB GB8820733A patent/GB2209314A/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2119603A1 (es) * | 1994-11-03 | 1998-10-01 | Saiz Manuel Munoz | Sistema de propulsion y estabilizacion para aviones de despegue vertical. |
ES2293818A1 (es) * | 2006-02-09 | 2008-03-16 | Manuel Muñoz Saiz | Sistema sustentador y propulsor para aeronaves de despegue y aterrizaje vertical. |
Also Published As
Publication number | Publication date |
---|---|
DE3829329A1 (de) | 1989-03-16 |
GB8820733D0 (en) | 1988-10-05 |
FR2619786A1 (fr) | 1989-03-03 |
GB2209314A (en) | 1989-05-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5178344A (en) | VTOL aircraft | |
NO934831L (no) | Ubemannet luftfartöy som kan foreta vertikal letting og landing og som kan ha horisontal flyvebane | |
Anderson | Historical overview of V/STOL aircraft technology | |
CA2075043A1 (en) | Vtol aircraft | |
CA2335954A1 (en) | Balloon trajectory control system | |
ES2008200A6 (es) | Disposicion sustentadora por accion directa del flujo de los motores para aeronaves de despegue vertical. | |
US4085911A (en) | Vertical takeoff and landing aircraft | |
PL308911A1 (en) | Flying device | |
US4804156A (en) | Circular aircraft | |
RU2135393C1 (ru) | Индивидуальный летательный аппарат | |
US3633847A (en) | Aircraft with lift-and-cruise fans | |
US3823897A (en) | Vertical take-off and landing aircraft | |
GB900095A (en) | Air-craft having an annular wing and a propulsion means fitted into the latter | |
US3847368A (en) | Lift cell | |
US3081965A (en) | Channel winged aircraft | |
JPS6474200A (en) | Simple flight device | |
FR2349495A1 (fr) | Aile circulaire | |
RU2067064C1 (ru) | Планирующий управляемый парашют | |
CZ346292A3 (cs) | Konstrukce pro závěsný kluzák nebo klouzavý padák | |
JPH02114094A (ja) | 超軽量動力機および推進装置 | |
THOMAS et al. | Powered low-aspect-ratio Wing In Ground effect(WIG) aerodynamic characteristics(conducted in Langley V/STOL tunnel) | |
DE3832157A1 (de) | Flugkoerper als erntegeraet, sowie verfahren zum stabilisieren des flugkoerpers | |
Krobusek | Aircrew aspects of United Stated future fighter aircraft | |
RU92007811A (ru) | Способ аэродинамической компенсации реактивного момента несущего винта вертолета одновинтовой или многовинтовой соосной схемы | |
CN107176292A (zh) | 一种飞行器用空气推进器 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FD1A | Patent lapsed |
Effective date: 20020318 |