RU2009107697A - Элемент конструкции летательного аппарата - Google Patents
Элемент конструкции летательного аппарата Download PDFInfo
- Publication number
- RU2009107697A RU2009107697A RU2009107697/11A RU2009107697A RU2009107697A RU 2009107697 A RU2009107697 A RU 2009107697A RU 2009107697/11 A RU2009107697/11 A RU 2009107697/11A RU 2009107697 A RU2009107697 A RU 2009107697A RU 2009107697 A RU2009107697 A RU 2009107697A
- Authority
- RU
- Russia
- Prior art keywords
- nacelle
- composite material
- geopolymer resin
- air intake
- rear frame
- Prior art date
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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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B20/00—Use of materials as fillers for mortars, concrete or artificial stone according to more than one of groups C04B14/00 - C04B18/00 and characterised by shape or grain distribution; Treatment of materials according to more than one of the groups C04B14/00 - C04B18/00 specially adapted to enhance their filling properties in mortars, concrete or artificial stone; Expanding or defibrillating materials
- C04B20/0048—Fibrous materials
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B28/00—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
- C04B28/006—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing mineral polymers, e.g. geopolymers of the Davidovits type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- 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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
-
- 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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0233—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/00982—Uses not provided for elsewhere in C04B2111/00 as construction elements for space vehicles or aeroplanes
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/40—Organic materials
- F05D2300/44—Resins
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/614—Fibres or filaments
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P40/00—Technologies relating to the processing of minerals
- Y02P40/10—Production of cement, e.g. improving or optimising the production methods; Cement grinding
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ceramic Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Inorganic Chemistry (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Control Of Motors That Do Not Use Commutators (AREA)
- Bipolar Transistors (AREA)
- Details Of Aerials (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
- Radio Relay Systems (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Abstract
1. Задний шпангоут воздухозаборника гондолы летательного аппарата, отличающийся тем, что он выполнен частично из композитного материала на базе геополимерной смолы, усиленной волокнами, и содержит, по меньшей мере, одну часть (56), окружающую отверстие, предусмотренное для прохода системы для устранения обледенения из композитного материала на базе геополимерной смолы, усиленной волокнами и, по меньшей мере, одну другую металлическую часть (58). ! 2. Задний шпангоут воздухозаборника гондолы летательного аппарата по п.1, отличающийся тем, что он содержит две концентрические части, первую кольцевую часть (56) из композитного материала на базе геополимерной смолы, усиленной волокнами, в контакте с наружной обшивкой (34) гондолы и вторую кольцевую металлическую часть (58) в контакте с внутренней обшивкой (32) гондолы. !3. Задний шпангоут воздухозаборника гондолы летательного аппарата по п.1 или 2, отличающийся тем, что он выполнен из композитного материала на базе волокон, утопленных в геополимерной смоле типа сиалата (xSiO2·AIO2), в котором x заключен между или равен 1,75 и 50. ! 4. Задний шпангоут воздухозаборника гондолы летательного аппарата по п.3, отличающийся тем, что волокна были, по меньшей мере, частично расшлихтованы предварительно перед пропиткой геополимерной смолой.
Claims (4)
1. Задний шпангоут воздухозаборника гондолы летательного аппарата, отличающийся тем, что он выполнен частично из композитного материала на базе геополимерной смолы, усиленной волокнами, и содержит, по меньшей мере, одну часть (56), окружающую отверстие, предусмотренное для прохода системы для устранения обледенения из композитного материала на базе геополимерной смолы, усиленной волокнами и, по меньшей мере, одну другую металлическую часть (58).
2. Задний шпангоут воздухозаборника гондолы летательного аппарата по п.1, отличающийся тем, что он содержит две концентрические части, первую кольцевую часть (56) из композитного материала на базе геополимерной смолы, усиленной волокнами, в контакте с наружной обшивкой (34) гондолы и вторую кольцевую металлическую часть (58) в контакте с внутренней обшивкой (32) гондолы.
3. Задний шпангоут воздухозаборника гондолы летательного аппарата по п.1 или 2, отличающийся тем, что он выполнен из композитного материала на базе волокон, утопленных в геополимерной смоле типа сиалата (xSiO2·AIO2), в котором x заключен между или равен 1,75 и 50.
4. Задний шпангоут воздухозаборника гондолы летательного аппарата по п.3, отличающийся тем, что волокна были, по меньшей мере, частично расшлихтованы предварительно перед пропиткой геополимерной смолой.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0653291 | 2006-08-04 | ||
FR0653291A FR2904604B1 (fr) | 2006-08-04 | 2006-08-04 | Element de structure d'un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2009107697A true RU2009107697A (ru) | 2010-09-10 |
RU2438923C2 RU2438923C2 (ru) | 2012-01-10 |
Family
ID=37895996
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2009107697/11A RU2438923C2 (ru) | 2006-08-04 | 2007-07-30 | Элемент конструкции летательного аппарата |
Country Status (11)
Country | Link |
---|---|
US (1) | US20090314899A1 (ru) |
EP (1) | EP2046638B1 (ru) |
JP (1) | JP5031834B2 (ru) |
CN (1) | CN101535122B (ru) |
AT (1) | ATE481313T1 (ru) |
BR (1) | BRPI0714253A2 (ru) |
CA (1) | CA2659821A1 (ru) |
DE (1) | DE602007009256D1 (ru) |
FR (1) | FR2904604B1 (ru) |
RU (1) | RU2438923C2 (ru) |
WO (1) | WO2008015362A1 (ru) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2936776A1 (fr) * | 2008-10-08 | 2010-04-09 | Aircelle Sa | Structure d'entree d'air de nacelle |
FR2966128B1 (fr) | 2010-10-15 | 2013-06-14 | Airbus Operations Sas | Nacelle d'aeronef incorporant une zone de jonction continue entre une paroi exterieure et un cadre avant et/ou un cadre arriere |
FR2966126B1 (fr) | 2010-10-15 | 2013-06-28 | Airbus Operations Sas | Nacelle d'aeronef incorporant un cadre arriere incline vers l'arriere |
FR2976556B1 (fr) | 2011-06-17 | 2013-12-27 | Airbus Operations Sas | Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule |
FR2978731B1 (fr) * | 2011-08-05 | 2014-05-02 | Airbus Operations Sas | Nacelle d'aeronef incorporant un anneau de renfort. |
FR2981049B1 (fr) * | 2011-10-07 | 2014-04-11 | Aircelle Sa | Procede de fabrication d'un panneau d'absorption acoustique |
FR2998548B1 (fr) * | 2012-11-23 | 2015-01-30 | Airbus Operations Sas | Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation |
FR3000463B1 (fr) * | 2012-12-27 | 2016-02-05 | Eads Europ Aeronautic Defence | Dispositif d'absorption d'energie pour element de structure d'aeronef |
FR3041937B1 (fr) * | 2015-10-05 | 2017-10-20 | Airbus Operations Sas | Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure |
US10189572B2 (en) * | 2016-05-02 | 2019-01-29 | The Boeing Company | Systems and methods for preventing ice formation on portions of an aircraft |
FR3083265A1 (fr) * | 2018-06-29 | 2020-01-03 | Airbus Operations | Structure d'entree d'air pour une nacelle d'aeronef comportant un element amortisseur de chocs |
FR3084648B1 (fr) * | 2018-08-03 | 2020-07-17 | Safran Nacelles | Procede de traitement contre le givre de piece d’aeronef |
US11408341B2 (en) * | 2018-11-05 | 2022-08-09 | Rohr, Inc. | Anti-icing system for an aircraft nacelle |
CN109606708B (zh) * | 2018-12-03 | 2022-04-08 | 江西洪都航空工业集团有限责任公司 | 一种小尺寸进气道结构制备方法 |
US11220344B2 (en) * | 2018-12-17 | 2022-01-11 | Rohr, Inc. | Anti-ice double walled duct system |
PL3932801T3 (pl) | 2020-06-30 | 2022-09-19 | Airbus Helicopters Deutschland GmbH | Wiropłat z układem przegrody przeciwogniowej |
EP4001105B1 (en) | 2020-11-20 | 2023-07-05 | Airbus Helicopters Deutschland GmbH | A stiffener skeleton for a firewall arrangement of a rotary wing aircraft |
EP4071046B1 (en) | 2021-04-09 | 2023-06-07 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A rotary wing aircraft with a firewall arrangement |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU581684B2 (en) * | 1984-10-08 | 1989-03-02 | Short Brothers Plc | Duct for hot air |
IL78786A0 (en) * | 1985-06-03 | 1986-08-31 | Short Brothers Plc | Duct for hot air |
US5925449A (en) * | 1996-12-26 | 1999-07-20 | Davidovits; Joseph | Method for bonding fiber reinforcement on concrete and steel structures and resultant products |
FR2757823B1 (fr) * | 1996-12-26 | 1999-03-12 | Aerospatiale | Nacelle de turboreacteur a ecoulement laminaire |
FR2838733B1 (fr) * | 2002-04-18 | 2004-06-25 | Joseph Davidovits | Procede d 'obtention de resines geopolymeriques liquides pretes a l'emploi et produits realises par le procede |
US6725645B1 (en) * | 2002-10-03 | 2004-04-27 | General Electric Company | Turbofan engine internal anti-ice device |
FR2859992B1 (fr) * | 2003-09-24 | 2005-10-21 | Commissariat Energie Atomique | Procede de preparation par sol-gel d'un materiau composite a matrice vitroceramique d'aluminosilicate de lithium |
FR2868123B1 (fr) * | 2004-03-29 | 2006-06-23 | Airbus France Sas | Structure d'entree d'air pour moteur d'aeronef |
US7210611B2 (en) * | 2004-10-21 | 2007-05-01 | The Boeing Company | Formed structural assembly and associated preform and method |
US7721525B2 (en) * | 2006-07-19 | 2010-05-25 | Rohr, Inc. | Aircraft engine inlet having zone of deformation |
US7900872B2 (en) * | 2007-12-12 | 2011-03-08 | Spirit Aerosystems, Inc. | Nacelle inlet thermal anti-icing spray duct support system |
-
2006
- 2006-08-04 FR FR0653291A patent/FR2904604B1/fr not_active Expired - Fee Related
-
2007
- 2007-07-30 CA CA002659821A patent/CA2659821A1/en not_active Abandoned
- 2007-07-30 BR BRPI0714253-6A2A patent/BRPI0714253A2/pt not_active IP Right Cessation
- 2007-07-30 RU RU2009107697/11A patent/RU2438923C2/ru not_active IP Right Cessation
- 2007-07-30 EP EP07823666A patent/EP2046638B1/fr not_active Ceased
- 2007-07-30 CN CN2007800288426A patent/CN101535122B/zh not_active Expired - Fee Related
- 2007-07-30 WO PCT/FR2007/051751 patent/WO2008015362A1/fr active Application Filing
- 2007-07-30 AT AT07823666T patent/ATE481313T1/de not_active IP Right Cessation
- 2007-07-30 JP JP2009522316A patent/JP5031834B2/ja not_active Expired - Fee Related
- 2007-07-30 US US12/376,143 patent/US20090314899A1/en not_active Abandoned
- 2007-07-30 DE DE602007009256T patent/DE602007009256D1/de active Active
Also Published As
Publication number | Publication date |
---|---|
CN101535122B (zh) | 2012-06-27 |
RU2438923C2 (ru) | 2012-01-10 |
JP2009545695A (ja) | 2009-12-24 |
BRPI0714253A2 (pt) | 2013-06-18 |
US20090314899A1 (en) | 2009-12-24 |
JP5031834B2 (ja) | 2012-09-26 |
FR2904604B1 (fr) | 2009-02-27 |
DE602007009256D1 (de) | 2010-10-28 |
FR2904604A1 (fr) | 2008-02-08 |
EP2046638A1 (fr) | 2009-04-15 |
WO2008015362A1 (fr) | 2008-02-07 |
EP2046638B1 (fr) | 2010-09-15 |
CN101535122A (zh) | 2009-09-16 |
CA2659821A1 (en) | 2008-02-07 |
ATE481313T1 (de) | 2010-10-15 |
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