RU2016150900A3 - - Google Patents
Download PDFInfo
- Publication number
- RU2016150900A3 RU2016150900A3 RU2016150900A RU2016150900A RU2016150900A3 RU 2016150900 A3 RU2016150900 A3 RU 2016150900A3 RU 2016150900 A RU2016150900 A RU 2016150900A RU 2016150900 A RU2016150900 A RU 2016150900A RU 2016150900 A3 RU2016150900 A3 RU 2016150900A3
- Authority
- RU
- Russia
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/40—Movement of components
- F05D2250/42—Movement of components with two degrees of freedom
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1454927A FR3021704B1 (fr) | 2014-05-30 | 2014-05-30 | Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives |
| FR14/54927 | 2014-05-30 | ||
| PCT/FR2015/051323 WO2015181471A1 (fr) | 2014-05-30 | 2015-05-20 | Nacelle pour turboréacteur d'aéronef comprenant une tuyère secondaire à portes rotatives |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| RU2016150900A RU2016150900A (ru) | 2018-07-02 |
| RU2016150900A3 true RU2016150900A3 (ru) | 2018-11-30 |
| RU2688082C2 RU2688082C2 (ru) | 2019-05-17 |
Family
ID=51417447
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2016150900A RU2688082C2 (ru) | 2014-05-30 | 2015-05-20 | Гондола турбореактивного двигателя, содержащая сопло вторичного контура с поворотными створками |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US10100780B2 (ru) |
| EP (1) | EP3149318B1 (ru) |
| CN (1) | CN106662040B (ru) |
| BR (1) | BR112016028164A2 (ru) |
| CA (1) | CA2949746A1 (ru) |
| FR (1) | FR3021704B1 (ru) |
| RU (1) | RU2688082C2 (ru) |
| WO (1) | WO2015181471A1 (ru) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3054266B1 (fr) * | 2016-07-25 | 2018-08-31 | Safran Nacelles | Systeme d’actionnement d’un panneau de nacelle de turboreacteur |
| US10752371B2 (en) * | 2016-09-30 | 2020-08-25 | General Electric Company | Translating nacelle wall for an aircraft tail mounted fan section |
| US10738737B2 (en) * | 2016-11-18 | 2020-08-11 | Rohr, Inc. | Self-locking alignment at a nacelle interface |
| FR3074776B1 (fr) * | 2017-12-13 | 2020-02-28 | Safran Nacelles | Levre d’entree d’air de nacelle pour turboreacteur |
| FR3075274B1 (fr) * | 2017-12-14 | 2021-10-22 | Airbus Operations Sas | Turboreacteur d'aeronef comportant des moyens permettant de varier sa surface de sortie |
| FR3088373B1 (fr) * | 2018-11-09 | 2021-03-19 | Safran Nacelles | Joint d’etancheite pour nacelle de turboreacteur d’aeronef |
| FR3100578B1 (fr) | 2019-09-05 | 2021-09-24 | Safran Nacelles | Inverseur de poussée muni d’une cinématique à câble pour volets écopants |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3764096A (en) * | 1972-02-24 | 1973-10-09 | Rohr Industries Inc | Thrust reversing apparatus |
| US4605169A (en) * | 1983-12-27 | 1986-08-12 | United Technologies Corporation | Exhaust nozzle construction |
| FR2622929A1 (fr) | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a grilles,a section variable d'ejection |
| FR2741910B1 (fr) * | 1995-11-30 | 1998-01-02 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes a panneau arriere articule |
| FR2903455B1 (fr) * | 2006-07-05 | 2013-01-18 | Airbus France | Procede pour inverser la poussee produite par un ensemble propulsif d'un aeronef, dispositif pour sa mise en oeuvre, nacelle equipee dudit dispositif |
| FR2910937B1 (fr) * | 2007-01-02 | 2009-04-03 | Airbus France Sas | Nacelle de reacteur d'aeronef et aeronef comportant une telle nacelle |
| FR2929998B1 (fr) * | 2008-04-14 | 2011-08-12 | Aircelle Sa | Nacelle de turboreacteur a double flux |
| FR2946696B1 (fr) | 2009-06-10 | 2012-04-20 | Aircelle Sa | Dispositif d'inversion de poussee |
| FR2965304B1 (fr) * | 2010-09-23 | 2012-10-12 | Airbus Operations Sas | Dispositif de decharge d'air pour turboreacteur d'avion a double flux |
| FR2967399B1 (fr) * | 2010-11-16 | 2012-11-02 | Aircelle Sa | Nacelle pour turboreacteur double flux d'un aeronef |
| FR2978800B1 (fr) * | 2011-08-05 | 2014-05-23 | Aircelle Sa | Nacelle de turboreacteur a tuyere variable |
| US9103298B2 (en) * | 2011-12-29 | 2015-08-11 | Rohr, Inc. | Seal for a variable area fan nozzle |
| GB201220378D0 (en) * | 2012-11-13 | 2012-12-26 | Rolls Royce Plc | A gas turbine engine exhaust nozzle |
| FR3011820B1 (fr) * | 2013-10-11 | 2017-03-31 | Aircelle Sa | Nacelle pour moteur d'aeronef a tuyere de section variable |
-
2014
- 2014-05-30 FR FR1454927A patent/FR3021704B1/fr not_active Expired - Fee Related
-
2015
- 2015-05-20 RU RU2016150900A patent/RU2688082C2/ru active
- 2015-05-20 CA CA2949746A patent/CA2949746A1/fr not_active Abandoned
- 2015-05-20 CN CN201580028435.XA patent/CN106662040B/zh not_active Expired - Fee Related
- 2015-05-20 EP EP15729539.5A patent/EP3149318B1/fr not_active Not-in-force
- 2015-05-20 BR BR112016028164A patent/BR112016028164A2/pt not_active Application Discontinuation
- 2015-05-20 WO PCT/FR2015/051323 patent/WO2015181471A1/fr active Application Filing
-
2016
- 2016-11-30 US US15/364,623 patent/US10100780B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| FR3021704B1 (fr) | 2016-06-03 |
| US20170082064A1 (en) | 2017-03-23 |
| FR3021704A1 (fr) | 2015-12-04 |
| US10100780B2 (en) | 2018-10-16 |
| CN106662040A (zh) | 2017-05-10 |
| EP3149318B1 (fr) | 2018-08-22 |
| CA2949746A1 (fr) | 2015-12-03 |
| EP3149318A1 (fr) | 2017-04-05 |
| WO2015181471A1 (fr) | 2015-12-03 |
| BR112016028164A2 (pt) | 2017-08-22 |
| RU2688082C2 (ru) | 2019-05-17 |
| RU2016150900A (ru) | 2018-07-02 |
| CN106662040B (zh) | 2019-10-08 |