IT1226367B - Pilone di aereo. - Google Patents
Pilone di aereo.Info
- Publication number
- IT1226367B IT1226367B IT8821640A IT2164088A IT1226367B IT 1226367 B IT1226367 B IT 1226367B IT 8821640 A IT8821640 A IT 8821640A IT 2164088 A IT2164088 A IT 2164088A IT 1226367 B IT1226367 B IT 1226367B
- Authority
- IT
- Italy
- Prior art keywords
- pilon
- plane
- plane pilon
- Prior art date
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 |
|---|---|
| IT8821640A0 IT8821640A0 (it) | 1988-08-04 |
| IT1226367B true IT1226367B (it) | 1991-01-11 |
Family
ID=22166288
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT8821640A IT1226367B (it) | 1987-08-05 | 1988-08-04 | Pilone di aereo. |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US4966338A (it) |
| JP (1) | JPH01101296A (it) |
| CA (1) | CA1316163C (it) |
| DE (1) | DE3826306A1 (it) |
| FR (1) | FR2619076B1 (it) |
| GB (1) | GB2208502B (it) |
| IT (1) | IT1226367B (it) |
| SE (1) | SE504023C2 (it) |
Families Citing this family (48)
| 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. |
| US20150377123A1 (en) | 2007-08-01 | 2015-12-31 | United 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 |
| US11242805B2 (en) | 2007-08-01 | 2022-02-08 | Raytheon 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 |
| US11149650B2 (en) | 2007-08-01 | 2021-10-19 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
| US8256707B2 (en) * | 2007-08-01 | 2012-09-04 | United Technologies Corporation | Engine mounting configuration for a turbofan gas turbine engine |
| US11346289B2 (en) | 2007-08-01 | 2022-05-31 | Raytheon 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 |
| US8695920B2 (en) | 2008-06-02 | 2014-04-15 | 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 |
| US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | 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 |
| US8800914B2 (en) | 2008-06-02 | 2014-08-12 | 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 |
| JP5445586B2 (ja) * | 2009-10-07 | 2014-03-19 | トヨタ自動車株式会社 | 翼構造および整流装置 |
| 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 |
| US8651426B2 (en) | 2010-07-01 | 2014-02-18 | Rolls-Royce Plc | Jet engine installation |
| GB201011056D0 (en) * | 2010-07-01 | 2010-08-18 | Rolls Royce Plc | Pylon for attaching a gas turbine engine |
| 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 |
| JP6266775B2 (ja) | 2013-07-26 | 2018-01-24 | エムアールエイ・システムズ・エルエルシー | 航空機エンジンパイロン |
| WO2015088619A2 (en) | 2013-10-16 | 2015-06-18 | United Technologies Corporation | Geared turbofan engine with targeted modular efficiency |
| 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 (pt) * | 2021-03-24 | 2022-09-29 | Embraer S.A. | "superfície de controle longitudinal de aeronaves, sistema de controle longitudinal para aeronaves e aeronave" |
| TWM657368U (zh) * | 2023-11-20 | 2024-07-01 | 台灣飛行器股份有限公司 | 無人飛行裝置 |
| US20250368315A1 (en) * | 2024-06-04 | 2025-12-04 | General Electric Company | Engine pylon assembly with a control surface for an aircraft |
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/en 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 - Lifetime
- 1988-08-05 JP JP63194678A patent/JPH01101296A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| FR2619076A1 (fr) | 1989-02-10 |
| DE3826306A1 (de) | 1989-02-16 |
| SE504023C2 (sv) | 1996-10-21 |
| FR2619076B1 (fr) | 1994-01-07 |
| CA1316163C (en) | 1993-04-13 |
| IT8821640A0 (it) | 1988-08-04 |
| US4966338A (en) | 1990-10-30 |
| SE8802793D0 (sv) | 1988-08-02 |
| GB8818581D0 (en) | 1988-09-07 |
| GB2208502A (en) | 1989-04-05 |
| GB2208502B (en) | 1991-10-02 |
| SE8802793L (sv) | 1989-02-06 |
| JPH01101296A (ja) | 1989-04-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19950829 |