RU2014141342A - Сопло с регулируемым сечением и гондола для турбореактивного двигателя летательного аппарата, снабженная таким соплом - Google Patents
Сопло с регулируемым сечением и гондола для турбореактивного двигателя летательного аппарата, снабженная таким соплом Download PDFInfo
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
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- 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
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- 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
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
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- 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
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- 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
- F02K1/1207—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 fixed structure
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- 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
- F02K1/15—Control or regulation
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- 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
- F02K1/15—Control or regulation
- F02K1/18—Control or regulation automatic
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
- F01D17/22—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
- F01D17/22—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical
- F01D17/24—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical electrical
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- 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
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
- F02K1/085—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone by transversely deforming an internal member
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- 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
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- 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
- F02K1/10—Varying effective area of jet pipe or nozzle by distorting the jet pipe or nozzle
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- 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
- F02K1/11—Varying effective area of jet pipe or nozzle by means of pivoted eyelids
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- 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
- F02K1/1215—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, and the downstream series having its flaps hinged at their downstream ends on a fixed structure
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- 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
- F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
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- 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
- F02K1/123—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure
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- 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
- F02K1/1238—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on a substantially axially movable structure
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- 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
- F02K1/1246—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their downstream ends on a substantially axially movable structure
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- 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
- F02K1/1253—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 fixed structure and of a substantially axially movable external member
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- 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
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- 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
- F02K1/1269—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the internal downstream series having its flaps hinged at their downstream ends on the downstream ends of the flaps of the external downstream series hinged on a fixed structure at their upstream ends
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- 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
- F02K1/1276—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a substantially axially movable structure and the downstream or external series having its flaps hinged at their upstream ends on a fixed structure
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- 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
- F02K1/1284—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the internal downstream series having its flaps hinged at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure
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- 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
- F02K1/1292—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure
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- 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
- F05D2260/00—Function
- F05D2260/40—Transmission of power
- F05D2260/407—Transmission of power through piezoelectric conversion
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- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Control Of Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
Abstract
1. Сопло (3) с регулируемым сечением для гондолы (1) летательного аппарата, причем по меньшей мере часть (V1, V2, V3; В) указанного сопла выполнена с возможностью перемещения между по меньшей мере положением, соответствующим меньшему сечению, и по меньшей мере положением, соответствующим большему сечению, и содержит средства перемещения указанной части между указанными положениями, причем указанные средства перемещения включают в себя пьезоэлектрические исполнительные органы (Р, Р1, Р2) и средства управления указанными исполнительными органами, причем указанные исполнительные органы расположены одним из двух нижеперечисленных способов:указанные исполнительные органы (Р1, Р2) расположены на обеих сторонах указанной части (В),указанные исполнительные органы (Р) расположены впритык друг к другу с формированием при этом приводных штанг.2. Сопло по п. 1, в котором указанные исполнительные органы (Р1, Р2) наклеены на указанную деформируемую подвижную часть (В).3. Сопло по п. 1, в котором указанная подвижная часть включает в себя по меньшей мере одну шарнирно установленную створку (V1, V2, V3).4. Сопло по п. 1, в котором между указанными штангами (Р) и указанной подвижной частью помещены средства (15, 17) увеличения движения.5. Сопло по любому из пп. 1-4, в котором установлены пьезоэлектрические датчики (С1, С2) для определения положения указанной подвижной части.6. Сопло по п. 5, в котором указанные средства управления включают в себя электронный контрольный модуль (23), обеспечивающий подачу управляющего напряжения на указанные пьезоэлектрические исполнительные органы (Р1, Р2), и электронный приемный модуль (29), обеспечивающий прием напряжения положения, поступающего от указанных пьезоэлектрических да
Claims (7)
1. Сопло (3) с регулируемым сечением для гондолы (1) летательного аппарата, причем по меньшей мере часть (V1, V2, V3; В) указанного сопла выполнена с возможностью перемещения между по меньшей мере положением, соответствующим меньшему сечению, и по меньшей мере положением, соответствующим большему сечению, и содержит средства перемещения указанной части между указанными положениями, причем указанные средства перемещения включают в себя пьезоэлектрические исполнительные органы (Р, Р1, Р2) и средства управления указанными исполнительными органами, причем указанные исполнительные органы расположены одним из двух нижеперечисленных способов:
указанные исполнительные органы (Р1, Р2) расположены на обеих сторонах указанной части (В),
указанные исполнительные органы (Р) расположены впритык друг к другу с формированием при этом приводных штанг.
2. Сопло по п. 1, в котором указанные исполнительные органы (Р1, Р2) наклеены на указанную деформируемую подвижную часть (В).
3. Сопло по п. 1, в котором указанная подвижная часть включает в себя по меньшей мере одну шарнирно установленную створку (V1, V2, V3).
4. Сопло по п. 1, в котором между указанными штангами (Р) и указанной подвижной частью помещены средства (15, 17) увеличения движения.
5. Сопло по любому из пп. 1-4, в котором установлены пьезоэлектрические датчики (С1, С2) для определения положения указанной подвижной части.
6. Сопло по п. 5, в котором указанные средства управления включают в себя электронный контрольный модуль (23), обеспечивающий подачу управляющего напряжения на указанные пьезоэлектрические исполнительные органы (Р1, Р2), и электронный приемный модуль (29), обеспечивающий прием напряжения положения, поступающего от указанных пьезоэлектрических датчиков (С1, С2), при этом два указанных модуля образуют контур обратной связи.
7. Гондола (1) для турбореактивного двигателя летательного аппарата, содержащая сопло (3) с регулируемым сечением по любому из пп. 1-6.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1252472A FR2988439B1 (fr) | 2012-03-20 | 2012-03-20 | Tuyere a section variable et nacelle pour turboreacteur d'aeronef equipee d'une telle tuyere |
FR1252472 | 2012-03-20 | ||
PCT/FR2013/050585 WO2013140088A1 (fr) | 2012-03-20 | 2013-03-19 | Tuyère à section variable et nacelle pour turboréacteur d'aéronef équipée d'une telle tuyère |
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RU2014141342A true RU2014141342A (ru) | 2016-05-10 |
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Application Number | Title | Priority Date | Filing Date |
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RU2014141342A RU2014141342A (ru) | 2012-03-20 | 2013-03-19 | Сопло с регулируемым сечением и гондола для турбореактивного двигателя летательного аппарата, снабженная таким соплом |
Country Status (7)
Country | Link |
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US (1) | US9850776B2 (ru) |
EP (1) | EP2828490B1 (ru) |
CN (1) | CN104204421A (ru) |
CA (1) | CA2865995A1 (ru) |
FR (1) | FR2988439B1 (ru) |
RU (1) | RU2014141342A (ru) |
WO (1) | WO2013140088A1 (ru) |
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Publication number | Priority date | Publication date | Assignee | Title |
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US10040563B1 (en) * | 2013-04-11 | 2018-08-07 | Geoffrey P. Pinto | Dual panel actuator system for jet engines |
CN105197246A (zh) * | 2015-09-15 | 2015-12-30 | 上海交通大学 | 压电纤维复合材料驱动的发动机扇形降噪喷嘴 |
FR3052810B1 (fr) * | 2016-06-21 | 2018-07-27 | Safran Nacelles | Inverseur de poussee pour nacelle de turboreacteur |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2623352A (en) * | 1945-05-23 | 1952-12-30 | Rateau Soc | Method and means for adjusting the outlet cross section of the exhaust nozzle of a reaction jet propeller for aircraft and the like high-speed vehicles |
FR1053282A (fr) | 1951-04-11 | 1954-02-01 | Basf Ag | Procédé pour le finissage de textiles de cellulose |
FR1052971A (fr) | 1951-04-13 | 1954-01-29 | Fu Rstlich Hohenzollernsche Hu | Procédé de fabrication de paliers ou coussinets composés en acier et alliage de cuivre et à surfaces en acier durcies |
FR1057240A (fr) | 1952-05-19 | 1954-03-05 | Machine à écrire à commande non manuelle des caractères | |
US3040523A (en) * | 1958-10-23 | 1962-06-26 | Nathan C Price | Variable area propulsive nozzle |
GB0105349D0 (en) * | 2001-03-03 | 2001-04-18 | Rolls Royce Plc | Gas turbine engine exhaust nozzle |
US7578132B2 (en) * | 2001-03-03 | 2009-08-25 | Rolls-Royce Plc | Gas turbine engine exhaust nozzle |
BR0306781B1 (pt) * | 2002-01-09 | 2013-01-22 | bocal de exaustço de turbofan e mÉtodo para reduzir ruÍdo em um motor turbofan possuindo um bocal de exaustço de turbofan. | |
JP4026122B2 (ja) * | 2002-04-15 | 2007-12-26 | 株式会社Ihi | 推力偏向機能付きミキサノズル |
GB0312505D0 (en) * | 2003-05-31 | 2003-07-09 | Rolls Royce Plc | Engine nozzle |
DE502005001475D1 (de) * | 2004-12-22 | 2007-10-25 | Airbus Deutschland Gmbh Hrb 43527 | Tragwerk einer aerodynamischen Wirkfläche eines Flugzeugs |
US7721551B2 (en) * | 2006-06-29 | 2010-05-25 | United Technologies Corporation | Fan variable area nozzle for a gas turbine engine fan nacelle |
US20080211353A1 (en) * | 2007-03-02 | 2008-09-04 | Charles Erklin Seeley | High temperature bimorph actuator |
US20090226303A1 (en) * | 2008-03-05 | 2009-09-10 | Grabowski Zbigniew M | Variable area fan nozzle fan flutter management system |
US8240126B2 (en) * | 2008-03-22 | 2012-08-14 | Pratt & Whitney Rocketdyne, Inc. | Valve system for a gas turbine engine |
US8056865B2 (en) * | 2009-03-05 | 2011-11-15 | The Boeing Company | Mechanism for changing the shape of a control surface |
US8590842B2 (en) * | 2009-03-18 | 2013-11-26 | The Boeing Company | Tailorable stiffness shape morphing flow-path |
-
2012
- 2012-03-20 FR FR1252472A patent/FR2988439B1/fr not_active Expired - Fee Related
-
2013
- 2013-03-19 CA CA2865995A patent/CA2865995A1/fr not_active Abandoned
- 2013-03-19 WO PCT/FR2013/050585 patent/WO2013140088A1/fr active Application Filing
- 2013-03-19 RU RU2014141342A patent/RU2014141342A/ru not_active Application Discontinuation
- 2013-03-19 CN CN201380014784.7A patent/CN104204421A/zh active Pending
- 2013-03-19 EP EP13719903.0A patent/EP2828490B1/fr active Active
-
2014
- 2014-09-22 US US14/492,274 patent/US9850776B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2988439B1 (fr) | 2014-11-28 |
US9850776B2 (en) | 2017-12-26 |
EP2828490A1 (fr) | 2015-01-28 |
EP2828490B1 (fr) | 2020-02-05 |
CN104204421A (zh) | 2014-12-10 |
US20150345423A1 (en) | 2015-12-03 |
CA2865995A1 (fr) | 2013-09-26 |
FR2988439A1 (fr) | 2013-09-27 |
WO2013140088A1 (fr) | 2013-09-26 |
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