FR2619076B1 - Pylone d'avion - Google Patents
Pylone d'avionInfo
- Publication number
- FR2619076B1 FR2619076B1 FR8810363A FR8810363A FR2619076B1 FR 2619076 B1 FR2619076 B1 FR 2619076B1 FR 8810363 A FR8810363 A FR 8810363A FR 8810363 A FR8810363 A FR 8810363A FR 2619076 B1 FR2619076 B1 FR 2619076B1
- Authority
- FR
- France
- Prior art keywords
- pylon
- airplane
- airplane pylon
- 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
Classifications
-
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/04—Power-plant nacelles, fairings, or cowlings associated with fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Electron Sources, Ion Sources (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/081,772 US4966338A (en) | 1987-08-05 | 1987-08-05 | Aircraft pylon |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2619076A1 FR2619076A1 (fr) | 1989-02-10 |
FR2619076B1 true FR2619076B1 (fr) | 1994-01-07 |
Family
ID=22166288
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8810363A Expired - Fee Related FR2619076B1 (fr) | 1987-08-05 | 1988-08-01 | Pylone d'avion |
Country Status (8)
Country | Link |
---|---|
US (1) | US4966338A (fr) |
JP (1) | JPH01101296A (fr) |
CA (1) | CA1316163C (fr) |
DE (1) | DE3826306A1 (fr) |
FR (1) | FR2619076B1 (fr) |
GB (1) | GB2208502B (fr) |
IT (1) | IT1226367B (fr) |
SE (1) | SE504023C2 (fr) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5779191A (en) * | 1996-11-12 | 1998-07-14 | Brislawn; Mark G. | Pylon flap for increasing negative pitching moments |
GB2359052B (en) * | 2000-02-09 | 2003-09-17 | Rolls Royce Plc | Engine arrangement |
US6685143B1 (en) * | 2003-01-03 | 2004-02-03 | Orbital Research Inc. | Aircraft and missile forebody flow control device and method of controlling flow |
US6964397B2 (en) * | 2003-07-18 | 2005-11-15 | The Boeing Company | Nacelle chine installation for drag reduction |
FR2899200B1 (fr) * | 2006-03-28 | 2008-11-07 | Airbus France Sas | Aeronef a impact environnemental reduit |
US7770841B2 (en) * | 2006-12-22 | 2010-08-10 | Calvin Burgess | Inverted airfoil pylon for an aircraft |
FR2915179B1 (fr) * | 2007-04-23 | 2009-05-29 | Airbus France Sa | Aeronef a impact environnemental reduit. |
US8256707B2 (en) * | 2007-08-01 | 2012-09-04 | United Technologies Corporation | Engine mounting configuration for a turbofan gas turbine engine |
US20150377123A1 (en) | 2007-08-01 | 2015-12-31 | United Technologies Corporation | Turbine section of high bypass turbofan |
US11486311B2 (en) | 2007-08-01 | 2022-11-01 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11242805B2 (en) | 2007-08-01 | 2022-02-08 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11149650B2 (en) | 2007-08-01 | 2021-10-19 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11346289B2 (en) | 2007-08-01 | 2022-05-31 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US8844265B2 (en) | 2007-08-01 | 2014-09-30 | United Technologies Corporation | Turbine section of high bypass turbofan |
ES2335459B1 (es) * | 2007-12-21 | 2011-02-03 | Airbus España S.L. | Configuracion optimizada de motores de aeronave. |
US8118251B2 (en) * | 2008-01-18 | 2012-02-21 | United Technologies Corporation | Mounting system for a gas turbine engine |
US8167237B2 (en) * | 2008-03-21 | 2012-05-01 | United Technologies Corporation | Mounting system for a gas turbine engine |
US8800914B2 (en) | 2008-06-02 | 2014-08-12 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8128021B2 (en) * | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
US8511605B2 (en) | 2008-06-02 | 2013-08-20 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8807477B2 (en) | 2008-06-02 | 2014-08-19 | United Technologies Corporation | Gas turbine engine compressor arrangement |
US8695920B2 (en) | 2008-06-02 | 2014-04-15 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
FR2938504B1 (fr) * | 2008-11-14 | 2010-12-10 | Snecma | Entree d'air d'un moteur d'avion a helices propulsives non carenees |
FR2949754A1 (fr) * | 2009-09-04 | 2011-03-11 | Snecma | Pylone d'accrochage pour turbopropulseur |
US9090346B2 (en) | 2009-10-07 | 2015-07-28 | Toyota Jidosha Kabushiki Kaisha | Wing structure and fairing device |
ES2387595B1 (es) | 2009-11-27 | 2013-08-20 | Airbus Operations S.L. | Métodos y sistemas para minimizar las distorsiones de flujo en las palas de la hélice de una aeronave causadas por pilones delanteros |
FR2958624B1 (fr) * | 2010-04-08 | 2012-06-08 | Airbus Operations Sas | Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence |
GB201011056D0 (en) * | 2010-07-01 | 2010-08-18 | Rolls Royce Plc | Pylon for attaching a gas turbine engine |
EP2402251A3 (fr) | 2010-07-01 | 2015-08-05 | Rolls-Royce plc | Installation de turboréacteur |
FR2968634B1 (fr) * | 2010-12-08 | 2013-08-02 | Snecma | Pylone de fixation d'un moteur d'aeronef a helices propulsives non carenees |
US8622334B2 (en) * | 2011-05-19 | 2014-01-07 | Aurora Flight Sciences Corporation | System and method for reducing the noise of pusher type aircraft propellers |
FR2982236B1 (fr) * | 2011-11-03 | 2014-06-27 | Snecma | Pylone d'accrochage pour turbomachine |
FR2983834B1 (fr) * | 2011-12-12 | 2015-01-02 | Snecma | Pylone d'accrochage pour turbomachine |
WO2015010315A1 (fr) | 2013-07-26 | 2015-01-29 | Mra Systems, Inc. | Mât d'accrochage de moteur pour aéronef |
WO2015088619A2 (fr) | 2013-10-16 | 2015-06-18 | United Technologies Corporation | Moteur à double flux à engrenages à efficacité modulaire ciblée |
US9533754B2 (en) * | 2014-04-19 | 2017-01-03 | The Boeing Company | Wing aerial refueling system |
US9914528B2 (en) * | 2015-02-25 | 2018-03-13 | Embraer S.A. | Airframe-integrated propeller-driven propulsion systems |
US20170233060A1 (en) * | 2016-02-13 | 2017-08-17 | Mra Systems, Inc. | Aircraft and empennage section of an aircraft |
FR3050721B1 (fr) * | 2016-04-28 | 2018-04-13 | Airbus Operations | Ensemble moteur pour aeronef comprenant un bord d'attaque de mat integre a une rangee annulaire d'aubes directrices de sortie non carenees |
FR3052743B1 (fr) * | 2016-06-20 | 2018-07-06 | Airbus Operations | Ensemble pour aeronef comprenant des moteurs a propulsion par ingestion de la couche limite |
US11111029B2 (en) * | 2017-07-28 | 2021-09-07 | The Boeing Company | System and method for operating a boundary layer ingestion fan |
US20190225318A1 (en) * | 2018-01-25 | 2019-07-25 | General Electric Company | Aircraft systems and methods |
US10906657B2 (en) * | 2018-06-19 | 2021-02-02 | Raytheon Technologies Corporation | Aircraft system with distributed propulsion |
US10759545B2 (en) | 2018-06-19 | 2020-09-01 | Raytheon Technologies Corporation | Hybrid electric aircraft system with distributed propulsion |
WO2022198285A1 (fr) * | 2021-03-24 | 2022-09-29 | Embraer S.A. | Surface de contrôle en tangage d'aéronefs, système de contrôle en tangage pour aéronefs et aéronef |
Family Cites Families (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE489796C (de) * | 1928-06-16 | 1930-01-22 | Rudolf Wagner Dr | Propellerleitflaeche fuer mit Luftpropellern betriebene Fahrzeuge, insbesondere Flugzeuge |
US2142123A (en) * | 1938-01-05 | 1939-01-03 | Delmer S Fahrney | Extension wing flap |
US2257940A (en) * | 1938-06-22 | 1941-10-07 | Dornier Werke Gmbh | Airplane having a liftable pusher plant |
US2406625A (en) * | 1941-12-10 | 1946-08-27 | Thomas W Oglesby | Airplane |
US2426635A (en) * | 1941-12-13 | 1947-09-02 | Mercier Pierre Ernest | Engine, propeller, and fan drive |
US2510959A (en) * | 1942-04-16 | 1950-06-13 | Willard R Custer | Airplane with high-lift channeled wings |
US3090584A (en) * | 1956-08-15 | 1963-05-21 | Power Jets Res & Dev Ltd | Aircraft |
US3081964A (en) * | 1958-12-08 | 1963-03-19 | Boeing Co | Airplanes for vertical and/or short take-off and landing |
US3181810A (en) * | 1961-02-27 | 1965-05-04 | Curtiss Wright Corp | Attitude control system for vtol aircraft |
US3121544A (en) * | 1962-01-08 | 1964-02-18 | Alvarez-Calderon Alberto | Safety and high lift system and apparatus for aircraft |
US3179354A (en) * | 1962-04-24 | 1965-04-20 | Alvarez-Calderon Alberto | Convertiplane and apparatus thereof |
US3191888A (en) * | 1963-02-25 | 1965-06-29 | Robert C Sklenka | Aircraft having forward and aft propulsion means |
US3415468A (en) * | 1966-09-19 | 1968-12-10 | Philip D. Labombarde | Aircraft |
US3572960A (en) * | 1969-01-02 | 1971-03-30 | Gen Electric | Reduction of sound in gas turbine engines |
GB1209723A (en) * | 1969-06-14 | 1970-10-21 | Rolls Royce | Improvements in or relating to boundary layer air flow |
US3599749A (en) * | 1969-07-28 | 1971-08-17 | Rohr Corp | Jet noise control system |
DE2009105A1 (de) * | 1970-02-26 | 1971-09-02 | Messerschmitt Boelkow Blohm | Larmminderung bei Propellertriebwerken |
US3726091A (en) * | 1971-02-16 | 1973-04-10 | Rohr Corp | Sound suppressing apparatus |
US3695388A (en) * | 1971-06-14 | 1972-10-03 | Textron Inc | Quiet jet discharge nozzle |
US3826331A (en) * | 1972-02-29 | 1974-07-30 | Bolt Beranek & Newman | Method of and apparatus for reducing sound generated by surfaces in fluid jet streams and the like |
US4007896A (en) * | 1975-08-08 | 1977-02-15 | Reynolds Iii Collins J | Upwardly extendible wing flap system |
FR2370171A1 (fr) * | 1976-11-05 | 1978-06-02 | Snecma | Procede et dispositif pour la diminution du bruit des turbomachines |
GB2107426A (en) * | 1981-10-07 | 1983-04-27 | Sidney Walmsley | Boundary layer control |
US4466587A (en) * | 1981-12-21 | 1984-08-21 | General Electric Company | Nacelle installation |
GB2138507B (en) * | 1983-04-22 | 1987-07-29 | Rolls Royce | Mounting and exhausting in turbo-propellor aircraft engines |
US4540143A (en) * | 1983-08-04 | 1985-09-10 | The Boeing Company | Nacelle/wing assembly with wake control device |
US4685643A (en) * | 1983-08-04 | 1987-08-11 | The Boeing Company | Nacelle/wing assembly with vortex control device |
DE3521329A1 (de) * | 1985-06-14 | 1986-12-18 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Wirbelgeneratoren- und grenzschichtabweiseranordnung |
-
1987
- 1987-08-05 US US07/081,772 patent/US4966338A/en not_active Expired - Fee Related
-
1988
- 1988-07-07 CA CA000571418A patent/CA1316163C/fr not_active Expired - Fee Related
- 1988-08-01 FR FR8810363A patent/FR2619076B1/fr not_active Expired - Fee Related
- 1988-08-02 SE SE8802793A patent/SE504023C2/sv not_active IP Right Cessation
- 1988-08-03 DE DE3826306A patent/DE3826306A1/de not_active Withdrawn
- 1988-08-04 IT IT8821640A patent/IT1226367B/it active
- 1988-08-04 GB GB8818581A patent/GB2208502B/en not_active Expired - Fee Related
- 1988-08-05 JP JP63194678A patent/JPH01101296A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US4966338A (en) | 1990-10-30 |
JPH01101296A (ja) | 1989-04-19 |
DE3826306A1 (de) | 1989-02-16 |
GB2208502A (en) | 1989-04-05 |
GB2208502B (en) | 1991-10-02 |
SE504023C2 (sv) | 1996-10-21 |
CA1316163C (fr) | 1993-04-13 |
GB8818581D0 (en) | 1988-09-07 |
IT8821640A0 (it) | 1988-08-04 |
FR2619076A1 (fr) | 1989-02-10 |
SE8802793L (sv) | 1989-02-06 |
IT1226367B (it) | 1991-01-11 |
SE8802793D0 (sv) | 1988-08-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2619076B1 (fr) | Pylone d'avion | |
IT8820190A0 (it) | Pilone per aereo. | |
IT1217508B (it) | Turbopropulsore ad eliche propfan | |
FR2653742B1 (fr) | Helice d'avion. | |
GB2199795B (en) | Aircraft propulsion | |
DK15988A (da) | Diuretisk praeparat | |
FR2585326B3 (fr) | Configuration d'arriere de fuselage d'avion | |
FR2546476B1 (fr) | Atterrisseur pour structure d'aeronef | |
GB2201931B (en) | Flapping-wing aircraft | |
GB2189752B (en) | Weight-shift aircraft | |
GB8715073D0 (en) | Aircraft twin-wing configuration | |
GB2188301B (en) | Aeroplane wing | |
SE457329B (sv) | Flygfarkost | |
ES1000506Y (es) | Cabina anti-atraco | |
FR2576579B1 (fr) | Cabine d'aeronef | |
BR8702924A (pt) | Aeronave | |
GB2195308B (en) | An aircraft | |
SE8601417D0 (sv) | Flygplansform | |
ES282291Y (es) | Avion de juguete | |
IT8735550V0 (it) | Aeroscivolante monomotore | |
BR8704007A (pt) | Camara-de-ar seccionada | |
SE8402461D0 (sv) | Flygplan | |
SU1369165A1 (ru) | Cbepxлeгkий лetateльhый aппapat | |
GB8628325D0 (en) | Aircraft | |
BR6601078U (pt) | Paraquedas de aviao |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |