FR2906222B1 - VEHICLE WITH A FIXED VEHICLE WITH TAKE-OFF AND VERTICAL LANDING - Google Patents
VEHICLE WITH A FIXED VEHICLE WITH TAKE-OFF AND VERTICAL LANDINGInfo
- Publication number
- FR2906222B1 FR2906222B1 FR0608353A FR0608353A FR2906222B1 FR 2906222 B1 FR2906222 B1 FR 2906222B1 FR 0608353 A FR0608353 A FR 0608353A FR 0608353 A FR0608353 A FR 0608353A FR 2906222 B1 FR2906222 B1 FR 2906222B1
- Authority
- FR
- France
- Prior art keywords
- vehicle
- take
- wing
- vertical landing
- compressor
- 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 - Fee Related
Links
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 abstract 1
- 239000003546 flue gas 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
- B64C29/0008—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
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/01—Boundary layer ingestion [BLI] propulsion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/385—Variable incidence wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/48—Varying camber by relatively-movable parts of wing structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/04—Boundary layer controls by actively generating fluid flow
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The vehicle has a turbine (3) that generates air stream on an upper surface of a front wing (1) that is positioned in an inlet of a compressor. The wing (1) is constituted of the upper surface that is adjustable for providing air lift in takeoff phase, and a rigid lower surface. A rear wing (2) is positioned on an outlet of a pipe (11) and has another upper surface on which flue gas stream is applied for producing air lift force to allow takeoff and landing. The wings are arranged around the turbomachine. Injectors (7, 8) take air from the compressor.
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0608353A FR2906222B1 (en) | 2006-09-25 | 2006-09-25 | VEHICLE WITH A FIXED VEHICLE WITH TAKE-OFF AND VERTICAL LANDING |
EP07823490A EP2066564B1 (en) | 2006-09-25 | 2007-09-10 | Vertical take-off and landing vehicle which does not have a rotary wing |
JP2009529729A JP2010504249A (en) | 2006-09-25 | 2007-09-10 | Vertical take-off and landing aircraft without rotor blades |
US12/442,778 US20100006695A1 (en) | 2006-09-25 | 2007-09-10 | Vertical take-off and landing vehicle which does not have a rotary wing |
ES07823490T ES2353029T3 (en) | 2006-09-25 | 2007-09-10 | VERTICAL TAKE-OFF AND LANDING VEHICLE WITHOUT ROTATING SUSTAINATION PLANS. |
AT07823490T ATE481318T1 (en) | 2006-09-25 | 2007-09-10 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITHOUT ROTARY WINGS |
CA002664424A CA2664424A1 (en) | 2006-09-25 | 2007-09-10 | Vertical take-off and landing vehicle which does not have a rotary wing |
PCT/FR2007/001452 WO2008037865A1 (en) | 2006-09-25 | 2007-09-10 | Vertical take-off and landing vehicle which does not have a rotary wing |
DE602007009270T DE602007009270D1 (en) | 2006-09-25 | 2007-09-10 | SENKRECHT STARTING AND LANDING AIRPLANE WITHOUT ROTATING WINGS |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0608353A FR2906222B1 (en) | 2006-09-25 | 2006-09-25 | VEHICLE WITH A FIXED VEHICLE WITH TAKE-OFF AND VERTICAL LANDING |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2906222A1 FR2906222A1 (en) | 2008-03-28 |
FR2906222B1 true FR2906222B1 (en) | 2009-08-21 |
Family
ID=38022830
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0608353A Expired - Fee Related FR2906222B1 (en) | 2006-09-25 | 2006-09-25 | VEHICLE WITH A FIXED VEHICLE WITH TAKE-OFF AND VERTICAL LANDING |
Country Status (2)
Country | Link |
---|---|
ES (1) | ES2353029T3 (en) |
FR (1) | FR2906222B1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2953808B1 (en) * | 2009-12-11 | 2016-09-09 | li jing Chen | AN AIRCRAFT WHOSE PUSH-WEIGHT RATIO IS LESS THAN 1 ARRIVES TO TAKE OFF AND VERTICALLY LAND |
GB201107104D0 (en) * | 2011-04-27 | 2011-06-08 | Rotherham Jamie | Lift generating device |
CN103419933B (en) * | 2013-07-24 | 2016-12-28 | 南京航空航天大学 | Based on wing layout vertically taking off and landing flyer before and after high lift device |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB862032A (en) * | 1958-10-03 | 1961-03-01 | Power Jets Res & Dev Ltd | Aircraft |
FR1261961A (en) * | 1960-03-18 | 1961-05-26 | Improvements to carrier wing aerodynes | |
GB1465412A (en) * | 1975-02-14 | 1977-02-23 | Coxon J | Aircraft |
US4848701A (en) * | 1987-06-22 | 1989-07-18 | Belloso Gregorio M | Vertical take-off and landing aircraft |
-
2006
- 2006-09-25 FR FR0608353A patent/FR2906222B1/en not_active Expired - Fee Related
-
2007
- 2007-09-10 ES ES07823490T patent/ES2353029T3/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2906222A1 (en) | 2008-03-28 |
ES2353029T3 (en) | 2011-02-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2909974B1 (en) | NACELLE FOR TURBOJET DOUBLE FLOW | |
EP1895140A3 (en) | Fan exhaust nozzle for turbofan engine | |
EP2784267A3 (en) | A gas turbine engine cooling arrangement | |
BR112012008685A2 (en) | combination of a gas turbine engine and a nacelle | |
WO2008098332A3 (en) | Vortex generator for flush air inlets performance improvement | |
EP2527742A3 (en) | System and method for flow control in gas turbine engine | |
RU2008137530A (en) | AERODYNAMIC FLAP OF THE AIRCRAFT WITH THE DEVICE INFLUENCING THE STREAM OF FLOW | |
ATE530441T1 (en) | ENGINE INLET DOOR FOR ATTACHMENT TO THE HOUSING OF AN AIR INLET OF AN AIRCRAFT ENGINE AND ENGINE HAVING SUCH ENGINE INLET DOOR AND AIRCRAFT SYSTEM | |
EP2196626A3 (en) | A gas turbine engine | |
EP2402250A3 (en) | Pylon for attaching a gas turbine engine | |
RU2014122331A (en) | SUSPENSION Pylon for gas turbine engine | |
US8967964B2 (en) | Boundary layer energiser | |
ATE431287T1 (en) | AIRCRAFT WITH CENTRAL STREAMLINE FAIRING THAT ADJUSTS THE PRESSURE ON THE WING STRUCTURES USING LOCAL GEOMETRIC DEFORMATIONS | |
EP2586977A3 (en) | Turbine of a turbomachine | |
EP3070000A3 (en) | Engine proximate nitrogen generation system for an aircraft | |
EP1998029A3 (en) | Nacelle for an aircraft engine with inlet flow control system and corresponding operating method | |
WO2008045051A3 (en) | Gas turbine nacelle comprising a passive boundary lazer bleed system and method of controlling turbulent airflow | |
EP2530247A3 (en) | Mount Device For Transition Duct In Turbine System | |
WO2009103564A3 (en) | Wind turbine | |
JP2014092157A5 (en) | ||
ATE555018T1 (en) | MEASUREMENT INSTRUMENT CARRIER INSERTED BETWEEN A DRIVE UNIT AND AN AIR INLET OF AN AIRCRAFT ENGINE NACHEL | |
WO2009024662A3 (en) | Coupling system connecting an internal structure and an external structure of a jet engine nacelle | |
FR2938504B1 (en) | AIR INTAKE OF AN AIRCRAFT ENGINE WITH NON-CARINE PROPELLANT PROPELLERS | |
ATE481318T1 (en) | VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITHOUT ROTARY WINGS | |
RU2012140949A (en) | DEVICE FOR REDUCING THE NOISE OF THE INTERACTION OF THE JET / PILON IN TURBO-REACTIVE ENGINES |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20100531 |
|
CL | Concession to grant licences |
Name of requester: COMPOSITES ATLANTIC LIMITED, CA Effective date: 20140408 |