ATE520590T1 - Verfahren und vorrichtung zur verstärkung des motorgetriebenen hubs in einem flugzeug - Google Patents
Verfahren und vorrichtung zur verstärkung des motorgetriebenen hubs in einem flugzeugInfo
- Publication number
- ATE520590T1 ATE520590T1 AT08843602T AT08843602T ATE520590T1 AT E520590 T1 ATE520590 T1 AT E520590T1 AT 08843602 T AT08843602 T AT 08843602T AT 08843602 T AT08843602 T AT 08843602T AT E520590 T1 ATE520590 T1 AT E520590T1
- Authority
- AT
- Austria
- Prior art keywords
- airfoil
- aircraft
- gases
- strengthening
- motor
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 2
- 238000005728 strengthening Methods 0.000 title 1
- 239000007789 gas Substances 0.000 abstract 4
- 230000000694 effects Effects 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
Classifications
-
- 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
-
- 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
- B64C3/58—Wings provided with fences or spoilers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
- Toys (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/927,290 US7878458B2 (en) | 2007-10-29 | 2007-10-29 | Method and apparatus for enhancing engine-powered lift in an aircraft |
| PCT/US2008/076950 WO2009058488A1 (en) | 2007-10-29 | 2008-09-19 | Method and apparatus for enhancing engine-powered lift in an aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE520590T1 true ATE520590T1 (de) | 2011-09-15 |
Family
ID=40293810
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT08843602T ATE520590T1 (de) | 2007-10-29 | 2008-09-19 | Verfahren und vorrichtung zur verstärkung des motorgetriebenen hubs in einem flugzeug |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US7878458B2 (de) |
| EP (1) | EP2214958B1 (de) |
| AT (1) | ATE520590T1 (de) |
| ES (1) | ES2370756T3 (de) |
| WO (1) | WO2009058488A1 (de) |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8485476B2 (en) * | 2004-08-20 | 2013-07-16 | University Of Miami | Discrete co-flow jet (DCFJ) airfoil |
| US7878458B2 (en) | 2007-10-29 | 2011-02-01 | The Boeing Company | Method and apparatus for enhancing engine-powered lift in an aircraft |
| US8167249B1 (en) | 2009-03-25 | 2012-05-01 | The Boeing Company | Controllable upper surface blown nozzle |
| US8322655B1 (en) | 2009-03-25 | 2012-12-04 | The Boeing Company | Twin-boom empennage |
| US8353478B1 (en) | 2009-03-25 | 2013-01-15 | The Boeing Company | Blended wing aircraft |
| US8061655B1 (en) * | 2009-03-25 | 2011-11-22 | The Boeing Company | Aircraft configuration utilizing fuselage, wing, empennage, and exhaust flow control devices |
| US8403256B1 (en) | 2009-03-25 | 2013-03-26 | The Boeing Company | Swept-wing powered-lift aircraft |
| US8317129B1 (en) | 2009-03-25 | 2012-11-27 | The Boeing Company | Universal convergent nozzle and distinct nozzle aperture |
| US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
| US8382040B2 (en) * | 2010-04-22 | 2013-02-26 | Terry Wayne Hamilton | Hamilton H.N2 laminar flow diskette wing |
| US9108725B1 (en) | 2012-11-29 | 2015-08-18 | The Boeing Company | Method and apparatus for robust lift generation |
| US9464532B2 (en) * | 2013-03-05 | 2016-10-11 | Bell Helicopter Textron Inc. | System and method for reducing rotor blade noise |
| EA027683B1 (ru) * | 2014-08-04 | 2017-08-31 | Алиби Хакимович Ахмеджанов | Аэродинамический двигатель |
| US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| EP4306789A3 (de) | 2015-09-02 | 2024-06-12 | Jetoptera, Inc. | Fluidisches antriebssystem |
| US20200324891A1 (en) * | 2015-09-02 | 2020-10-15 | Jetoptera, Inc. | Adaptive vertical take-off and landing propulsion system |
| US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| USD868627S1 (en) | 2018-04-27 | 2019-12-03 | Jetoptera, Inc. | Flying car |
| US10106246B2 (en) | 2016-06-10 | 2018-10-23 | Coflow Jet, LLC | Fluid systems that include a co-flow jet |
| US10315754B2 (en) | 2016-06-10 | 2019-06-11 | Coflow Jet, LLC | Fluid systems that include a co-flow jet |
| US10730607B2 (en) * | 2016-11-15 | 2020-08-04 | Colorado Seminary Which Owns And Operates The University Of Denver | Circulation control system for aerial vehicles |
| CA3068569A1 (en) | 2017-06-27 | 2019-01-03 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| US10618625B2 (en) * | 2017-07-12 | 2020-04-14 | The Boeing Company | Integrated slat chine apparatus and methods |
| US10683076B2 (en) | 2017-10-31 | 2020-06-16 | Coflow Jet, LLC | Fluid systems that include a co-flow jet |
| RU2743214C1 (ru) * | 2017-12-12 | 2021-02-16 | Америкэн Хонда Мотор Ко., Инк. | Гребень ограничения потока для винглета летательного аппарата |
| EP3732101A1 (de) * | 2017-12-28 | 2020-11-04 | Aero Design Labs, Inc. | Vorrichtung zur verminderung des strömungswiderstands einer abströmung eines querkanals |
| 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 |
| US11920617B2 (en) | 2019-07-23 | 2024-03-05 | Coflow Jet, LLC | Fluid systems and methods that address flow separation |
| CN110588956B (zh) * | 2019-10-08 | 2023-03-07 | 江西洪都航空工业集团有限责任公司 | 一种吹气式舵效增益装置 |
| WO2021257271A1 (en) | 2020-06-17 | 2021-12-23 | Coflow Jet, LLC | Fluid systems having a variable configuration |
| WO2022204278A1 (en) | 2021-03-26 | 2022-09-29 | Coflow Jet, LLC | Wind turbine blades and wind turbine systems that include a co-flow jet |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2928627A (en) * | 1956-07-10 | 1960-03-15 | Lockheed Aircraft Corp | Aircraft propulsion systems |
| US3018983A (en) | 1957-10-16 | 1962-01-30 | Power Jets Res & Dev Ltd | Jet aircraft with jet deflector |
| US3360218A (en) * | 1965-06-14 | 1967-12-26 | Wendell S Miller | Vertical take-off aircraft |
| US3697020A (en) * | 1970-09-14 | 1972-10-10 | Chandler Evans Inc | Vertical lift machine |
| US4019696A (en) | 1973-12-28 | 1977-04-26 | The Boeing Company | Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface |
| US3971534A (en) * | 1973-12-28 | 1976-07-27 | The Boeing Company | Method of and apparatus for controlling flow attachment to the wing and flap surfaces of an upper surface blowing type aircraft |
| US3940092A (en) * | 1974-11-07 | 1976-02-24 | The Boeing Company | Jet flow deflector for aircraft |
| US3960345A (en) * | 1975-05-16 | 1976-06-01 | Grumman Aerospace Corporation | Means to reduce and/or eliminate vortices, caused by wing body combinations |
| JPS5498000A (en) * | 1978-01-19 | 1979-08-02 | Kawasaki Heavy Ind Ltd | Device for strengthening thrust of aircraft |
| GB2038995B (en) * | 1979-01-02 | 1982-11-17 | Boeing Co | Flap shapes for an upper surface blowing powered lift system |
| US4447028A (en) | 1979-01-02 | 1984-05-08 | The Boeing Company | Upper surface blown powered lift system for aircraft |
| US4426054A (en) | 1979-01-02 | 1984-01-17 | The Boeing Company | Upper surface blown powered lift system |
| GB2051706A (en) * | 1979-06-19 | 1981-01-21 | British Aerospace | Aircraft wings |
| US4645140A (en) * | 1983-08-18 | 1987-02-24 | Rockwell International Corporation | Nozzle system |
| FR2554081A1 (fr) * | 1983-11-02 | 1985-05-03 | Sirretta Raymond | Dispositif pour ameliorer les conditions aerodynamiques de penetration et de sustentation des planeurs d'aeronefs |
| DE3345154C2 (de) * | 1983-12-14 | 1987-02-12 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Tragflügel für Luftfahrzeuge |
| DE3909347A1 (de) * | 1989-03-22 | 1990-09-27 | Mtu Muenchen Gmbh | Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete |
| US5253828A (en) * | 1992-07-17 | 1993-10-19 | The Board Of Regents Of The University Of Oklahoma | Concealable flap-actuated vortex generator |
| US5575442A (en) * | 1995-01-19 | 1996-11-19 | The United States Of America As Represented By The Secretary Of The Navy | Guided wing for aircraft flying at high angles of attack |
| GB2318558A (en) | 1996-10-23 | 1998-04-29 | Everitt Ray | Vehicle with lift producing arrangement |
| US6837465B2 (en) * | 2003-01-03 | 2005-01-04 | Orbital Research Inc | Flow control device and method of controlling flow |
| US6926229B2 (en) | 2003-12-08 | 2005-08-09 | The Boeing Company | Aircraft with thrust vectoring for switchably providing upper surface blowing |
| US7878458B2 (en) | 2007-10-29 | 2011-02-01 | The Boeing Company | Method and apparatus for enhancing engine-powered lift in an aircraft |
-
2007
- 2007-10-29 US US11/927,290 patent/US7878458B2/en not_active Expired - Fee Related
-
2008
- 2008-09-19 EP EP08843602A patent/EP2214958B1/de not_active Not-in-force
- 2008-09-19 WO PCT/US2008/076950 patent/WO2009058488A1/en not_active Ceased
- 2008-09-19 ES ES08843602T patent/ES2370756T3/es active Active
- 2008-09-19 AT AT08843602T patent/ATE520590T1/de not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EP2214958A1 (de) | 2010-08-11 |
| EP2214958B1 (de) | 2011-08-17 |
| US20090108141A1 (en) | 2009-04-30 |
| ES2370756T3 (es) | 2011-12-22 |
| WO2009058488A1 (en) | 2009-05-07 |
| US7878458B2 (en) | 2011-02-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ATE520590T1 (de) | Verfahren und vorrichtung zur verstärkung des motorgetriebenen hubs in einem flugzeug | |
| DE602006008332D1 (de) | INTEGRIERTE FLÜGELSPITZENVERLÄNGERUNGEN UND VERFAHREN ZUM VERGRöSSERN DER FLÜGELOBERFLÄCHE EINES FLUGZEUGGRUNDMODELLS | |
| WO2009079046A3 (en) | Systems and methods for control of engine exhaust flow | |
| EP2589797A3 (de) | Sekundärtragfläche, die auf einem Abrissgitter auf eine Windturbinenschaufel montiert ist | |
| EP2607231A3 (de) | Tragflächen mit Spitzenprofil zur Geräuschreduktion und Verfahren zur Herstellung davon | |
| DE60335895D1 (de) | Schlitzflügel für flugzeug | |
| ATE512049T1 (de) | Flugzeug mit ringförmigem heck | |
| ATE466766T1 (de) | Luftfahrzeug mit einer vorrichtung zur erzeugung einer aerodynamischen auftriebskraft | |
| WO2012010116A3 (de) | Angetriebenes fluggerät, insbesondere als nurflügler und/oder mit geringer radarsignatur ausgebildetes fluggerät | |
| EP2452873A3 (de) | Flugzeugflügelverlängerung und Düsensystem | |
| ATE478354T1 (de) | Verfahren und vorrichtung zum schutz eines luftfahrzeugs gegen turbulenzen bei klarer luft | |
| DE602007002979D1 (de) | Verfahren und vorrichtung zur flughilfe für ein flugzeug während eines autonomen landeanfluges | |
| GB201120256D0 (en) | An aircraft | |
| JP2008169834A (ja) | 境界層制御による粒子分離機 | |
| ATE418490T1 (de) | Verfahren zur verbesserung der sicherheit im luftfahrtransport | |
| DE602007002897D1 (de) | Flugzeugflügelanordnung mit einer triebwerksbefestigungsgondel, die im vorderen bereich einen lateralen luftstromkanal definiert | |
| WO2013064768A3 (fr) | Pylone d'accrochage pour turbomachine | |
| FR2938504B1 (fr) | Entree d'air d'un moteur d'avion a helices propulsives non carenees | |
| EP2610179A3 (de) | Flugzeuglufteinlassumlenkanordnungen mit verbesserten aerodynamischen Merkmalen | |
| GB2488172B (en) | Flow-modifying formation for aircraft wing | |
| FR2974563B1 (fr) | Profil aerodynamique reduisant le deficit de vitesse dans son sillage | |
| EP2604517A3 (de) | Minimal intrusive Flügelspitzenverwirbelungsbeginnabschwächung | |
| DE602005002397D1 (de) | Verfahren und Vorrichtung zur Führung eines Flugzeugs bei der Landung | |
| EP2778374A3 (de) | Plasmabetätigtes Kaskadenluftstromleitsystem | |
| DE602007003098D1 (de) | Verfahren und vorrichtung zum erzeugen eines aerodynamischen widerstands an einem flugzeug |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |