EP4724341A1 - Aéronef à réaction - Google Patents
Aéronef à réactionInfo
- Publication number
- EP4724341A1 EP4724341A1 EP23940914.7A EP23940914A EP4724341A1 EP 4724341 A1 EP4724341 A1 EP 4724341A1 EP 23940914 A EP23940914 A EP 23940914A EP 4724341 A1 EP4724341 A1 EP 4724341A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aircraft
- jet engine
- thrust
- engine
- deflector
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
- B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
L'invention concerne un aéronef comprenant un élément de châssis et au moins un moteur à réaction ayant un axe d'évacuation de poussée, une partie de connecteur et une ouverture d'évacuation permettant d'évacuer la poussée le long de l'axe d'évacuation du moteur à réaction. Le moteur à réaction est monté par la partie de connecteur sur l'élément de châssis, et au moins une partie de connecteur du moteur à réaction est montée sur l'élément de châssis de telle sorte que le moteur à réaction est mobile par rapport à l'élément de châssis de telle sorte que l'axe d'évacuation de poussée peut être sélectivement ajusté. Un déflecteur est disposé au niveau ou à proximité de l'ouverture d'évacuation du moteur à réaction, le déflecteur étant sélectivement mobile pour dévier la poussée.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US2023/068118 WO2024253690A1 (fr) | 2023-06-08 | 2023-06-08 | Aéronef à réaction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP4724341A1 true EP4724341A1 (fr) | 2026-04-15 |
Family
ID=93796374
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP23940914.7A Pending EP4724341A1 (fr) | 2023-06-08 | 2023-06-08 | Aéronef à réaction |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP4724341A1 (fr) |
| AU (1) | AU2023452253A1 (fr) |
| IL (1) | IL324930A (fr) |
| WO (1) | WO2024253690A1 (fr) |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5115996A (en) * | 1990-01-31 | 1992-05-26 | Moller International, Inc. | Vtol aircraft |
| GB2366265B (en) * | 1995-05-30 | 2002-06-19 | Rolls Royce Plc | Vtol aircraft nozzle |
| US5666803A (en) * | 1995-08-14 | 1997-09-16 | Windisch; D. Anthony | Vectored thrust compressor for remote controlled aircraft |
| AU2002361854A1 (en) * | 2001-12-26 | 2003-07-24 | Ricardo A. Ducasse | Variably angled propulsion/steering system |
| US8720814B2 (en) * | 2005-10-18 | 2014-05-13 | Frick A. Smith | Aircraft with freewheeling engine |
| US10994838B2 (en) * | 2012-12-07 | 2021-05-04 | Delorean Aerospace, Llc | Vertical takeoff and landing aircraft |
| US10112713B2 (en) * | 2015-06-26 | 2018-10-30 | Nelson Tyler | Back mounted flight machine |
-
2023
- 2023-06-08 IL IL324930A patent/IL324930A/en unknown
- 2023-06-08 AU AU2023452253A patent/AU2023452253A1/en active Pending
- 2023-06-08 WO PCT/US2023/068118 patent/WO2024253690A1/fr not_active Ceased
- 2023-06-08 EP EP23940914.7A patent/EP4724341A1/fr active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| IL324930A (en) | 2026-01-01 |
| WO2024253690A1 (fr) | 2024-12-12 |
| AU2023452253A1 (en) | 2025-12-11 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
| 17P | Request for examination filed |
Effective date: 20251202 |
|
| AK | Designated contracting states |
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