WO2010130690A3 - Verkleidung für eine auftriebshilfe - Google Patents
Verkleidung für eine auftriebshilfe Download PDFInfo
- Publication number
- WO2010130690A3 WO2010130690A3 PCT/EP2010/056374 EP2010056374W WO2010130690A3 WO 2010130690 A3 WO2010130690 A3 WO 2010130690A3 EP 2010056374 W EP2010056374 W EP 2010056374W WO 2010130690 A3 WO2010130690 A3 WO 2010130690A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- casing
- lifting aid
- aircraft
- relates
- aid
- Prior art date
Links
Classifications
-
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
-
- 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
Abstract
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201080021131.8A CN102438893B (zh) | 2009-05-13 | 2010-05-10 | 用于升力辅助装置的壳体 |
RU2011145806/11A RU2011145806A (ru) | 2009-05-13 | 2010-05-10 | Кожух для вспомогательной несущей поверхности |
EP10719337.7A EP2429895B1 (de) | 2009-05-13 | 2010-05-10 | Verkleidung für eine auftriebshilfe |
US13/293,570 US9669920B2 (en) | 2009-05-13 | 2011-11-10 | Casing for a lifting aid |
US15/587,902 US20170305528A1 (en) | 2009-05-13 | 2017-05-05 | Aircraft comprising a casing for a lifting aid |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US17783109P | 2009-05-13 | 2009-05-13 | |
DE102009003084A DE102009003084B4 (de) | 2009-05-13 | 2009-05-13 | Verkleidung für eine Auftriebshilfe |
DE102009003084.0 | 2009-05-13 | ||
US61/177,831 | 2009-05-13 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/293,570 Continuation US9669920B2 (en) | 2009-05-13 | 2011-11-10 | Casing for a lifting aid |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2010130690A2 WO2010130690A2 (de) | 2010-11-18 |
WO2010130690A3 true WO2010130690A3 (de) | 2011-04-28 |
Family
ID=42978900
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2010/056374 WO2010130690A2 (de) | 2009-05-13 | 2010-05-10 | Verkleidung für eine auftriebshilfe |
Country Status (6)
Country | Link |
---|---|
US (2) | US9669920B2 (de) |
EP (1) | EP2429895B1 (de) |
CN (1) | CN102438893B (de) |
DE (1) | DE102009003084B4 (de) |
RU (1) | RU2011145806A (de) |
WO (1) | WO2010130690A2 (de) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2982236B1 (fr) * | 2011-11-03 | 2014-06-27 | Snecma | Pylone d'accrochage pour turbomachine |
DE102012111690A1 (de) | 2012-11-30 | 2014-06-05 | Airbus Operations Gmbh | Formvariabler aerodynamischer Verkleidungskörper für einen Klappen-Verstellmechanismus eines Luftfahrzeugs |
FR3045012B1 (fr) * | 2015-12-11 | 2017-12-08 | Airbus Operations Sas | Mat d'accrochage d'une turbomachine muni d'un element de protection thermique |
US10723445B2 (en) | 2017-05-16 | 2020-07-28 | Rohr, Inc. | Strake for aircraft propulsion system nacelle |
US20190225318A1 (en) * | 2018-01-25 | 2019-07-25 | General Electric Company | Aircraft systems and methods |
RU2752502C1 (ru) * | 2020-12-18 | 2021-07-28 | Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") | Аэродинамический профиль несущего элемента летательного аппарата |
RU2762464C1 (ru) * | 2021-05-14 | 2021-12-21 | Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") | Аэродинамический профиль несущего элемента летательного аппарата |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4712750A (en) * | 1986-05-02 | 1987-12-15 | The Boeing Company | Temperature control device for jet engine nacelle associated structure |
DE3641247A1 (de) * | 1986-12-03 | 1988-06-16 | Messerschmitt Boelkow Blohm | Landeklappenfuehrungsschienen-verkleidung fuer luftfahrzeuge |
EP1627811A1 (de) * | 2004-08-20 | 2006-02-22 | The Boeing Company | Installation einer Wirbelsteuervorrichtung für Luftwiderstandsreduzierung |
FR2905930A1 (fr) * | 2006-09-18 | 2008-03-21 | Airbus France Sa | Generateur de tourbillon en sortie de gaz chauds |
FR2930235A1 (fr) * | 2008-04-21 | 2009-10-23 | Airbus France Sas | Mat de suspension pour turbomoteur. |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3578264A (en) * | 1968-07-09 | 1971-05-11 | Battelle Development Corp | Boundary layer control of flow separation and heat exchange |
US3744745A (en) * | 1971-09-30 | 1973-07-10 | Mc Donnell Douglas Corp | Liftvanes |
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 |
US3960345A (en) * | 1975-05-16 | 1976-06-01 | Grumman Aerospace Corporation | Means to reduce and/or eliminate vortices, caused by wing body combinations |
US4354648A (en) * | 1980-02-06 | 1982-10-19 | Gates Learjet Corporation | Airstream modification device for airfoils |
US4466587A (en) * | 1981-12-21 | 1984-08-21 | General Electric Company | Nacelle installation |
AU555526B2 (en) | 1982-10-29 | 1986-09-25 | General Electric Company | Aircraft engine nacelle |
US4685643A (en) * | 1983-08-04 | 1987-08-11 | The Boeing Company | Nacelle/wing assembly with vortex control device |
US4540143A (en) * | 1983-08-04 | 1985-09-10 | The Boeing Company | Nacelle/wing assembly with wake control device |
US5069402A (en) * | 1990-04-06 | 1991-12-03 | Istar, Inc. | Alleviation of aircraft fuselage form drag |
JP3714722B2 (ja) * | 1996-05-09 | 2005-11-09 | 本田技研工業株式会社 | 剥離抑制装置 |
US6837465B2 (en) * | 2003-01-03 | 2005-01-04 | Orbital Research Inc | 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 |
FR2891525B1 (fr) * | 2005-09-30 | 2007-11-09 | Airbus France Sas | Dispositif de controle d'un sillage tourbillonnaire engendre par un element oblong sur l'extrados d'une surface portante d'un aeronef. |
RU72198U1 (ru) | 2007-02-20 | 2008-04-10 | Владимир Тарасович Шведов | Самолет с высоким аэродинамическим качеством |
US8087617B2 (en) * | 2008-08-15 | 2012-01-03 | The Boeing Company | Retractable nacelle chine |
-
2009
- 2009-05-13 DE DE102009003084A patent/DE102009003084B4/de not_active Expired - Fee Related
-
2010
- 2010-05-10 WO PCT/EP2010/056374 patent/WO2010130690A2/de active Application Filing
- 2010-05-10 CN CN201080021131.8A patent/CN102438893B/zh active Active
- 2010-05-10 EP EP10719337.7A patent/EP2429895B1/de not_active Not-in-force
- 2010-05-10 RU RU2011145806/11A patent/RU2011145806A/ru not_active Application Discontinuation
-
2011
- 2011-11-10 US US13/293,570 patent/US9669920B2/en active Active
-
2017
- 2017-05-05 US US15/587,902 patent/US20170305528A1/en not_active Abandoned
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4712750A (en) * | 1986-05-02 | 1987-12-15 | The Boeing Company | Temperature control device for jet engine nacelle associated structure |
DE3641247A1 (de) * | 1986-12-03 | 1988-06-16 | Messerschmitt Boelkow Blohm | Landeklappenfuehrungsschienen-verkleidung fuer luftfahrzeuge |
EP1627811A1 (de) * | 2004-08-20 | 2006-02-22 | The Boeing Company | Installation einer Wirbelsteuervorrichtung für Luftwiderstandsreduzierung |
FR2905930A1 (fr) * | 2006-09-18 | 2008-03-21 | Airbus France Sa | Generateur de tourbillon en sortie de gaz chauds |
FR2930235A1 (fr) * | 2008-04-21 | 2009-10-23 | Airbus France Sas | Mat de suspension pour turbomoteur. |
Also Published As
Publication number | Publication date |
---|---|
RU2011145806A (ru) | 2013-05-20 |
WO2010130690A2 (de) | 2010-11-18 |
US20120112011A1 (en) | 2012-05-10 |
CN102438893A (zh) | 2012-05-02 |
DE102009003084B4 (de) | 2013-03-14 |
US9669920B2 (en) | 2017-06-06 |
US20170305528A1 (en) | 2017-10-26 |
EP2429895A2 (de) | 2012-03-21 |
DE102009003084A1 (de) | 2010-11-18 |
CN102438893B (zh) | 2014-12-17 |
EP2429895B1 (de) | 2013-04-17 |
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