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公开(公告)号：EP2824308B1
公开(公告)日：2018-12-26
申请号：EP14173655.3
申请日：2014-06-24
Applicant: Pratt & Whitney Canada Corp.
Inventor： Cunningham, Mark , Marini, Remo , Girgis, Sami , Kameshki, Mohammad Reza , Ramamurhty, Raja
CPC classification number: F01D25/30 , F02K1/386 , F02K1/48 , F05D2250/314 , F05D2250/37 , F05D2250/71 , Y02T50/672
Abstract: An exhaust mixer (32) for a gas turbine engine where each outer lobe (44) has at the downstream end a circumferential offset in a direction corresponding to that of the swirl component of the flow entering the mixer (32). The mixer (32) has a crest line (45) having at least a downstream portion curved with respect with respect to a circumferential direction of the mixer (32) and/or a center line at the downstream end tilted with respect to a radial line extending to the tip of the outer lobe (44) to define the circumferential offset.
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公开(公告)号：EP3406861A1
公开(公告)日：2018-11-28
申请号：EP18184008.3
申请日：2016-03-11
Applicant: United Technologies Corporation
Inventor： PETERS, Donald W. , PLACE, Emma J.
CPC classification number: F02K1/80 , F01D25/168 , F02K1/1223 , F05D2220/32 , F05D2240/128 , F05D2260/231 , F05D2300/434 , F05D2300/44 , F05D2300/603 , F05D2300/614 , F16C29/001 , F16C29/02 , F16C33/201 , Y02T50/672
Abstract: A composite wear pad (300, 306; 520) for being coupled to a slider block (204; 510) of a convergent nozzle of a gas turbine engine (100) includes a first rod (404), a second rod (405) and a high heat capacity composite (301; 505) having a plurality of carbon fibers (600) bonded together by a resin (602). The first and second rods are coupled to the high heat capacity composite (301; 505) at a respective first (460) and second axial end (463) of the composite wear pad (300, 306; 520) such that the first (460) and the second axial end (463) of the composite wear pad (300, 306; 520) each have an end thickness (452) that is greater than a middle thickness of the composite wear pad (300, 306; 520).
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公开(公告)号：EP3059169B1
公开(公告)日：2018-11-21
申请号：EP16154793.0
申请日：2016-02-09
Applicant: The Boeing Company
Inventor： ADAMSON, Eric E , FUGAL, Spencer Robert
CPC classification number: B64D33/02 , B64D2033/026 , F02C7/04 , F05D2220/80 , F05D2250/14 , Y02T50/672
Abstract: An apparatus is formed of a cowl and a flow inlet formed on an interior surface of the cowl. The flow inlet has a supersonic compression section attached to a subsonic diffusion section at a throat. The supersonic compression section includes an at least partially elliptical compression ramp which extends along an approximately 180 degree arc along the interior surface. The flow inlet may form part of an aircraft. A method of air flow using the flow inlet is also disclosed.
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公开(公告)号：EP3045674B1
公开(公告)日：2018-11-21
申请号：EP16150210.9
申请日：2016-01-05
Inventor： VETTERS, Daniel K. , SHI, Jun , WALSTON, Jeffrey A. , SIPPEL, Aaron D.
IPC: F01D11/12
CPC classification number: F01D11/08 , F01D11/12 , F01D21/003 , F01D25/28 , F05D2220/32 , F05D2230/642 , F05D2250/291 , F05D2260/30 , F05D2300/2261 , F05D2300/6033 , F05D2300/6034 , Y02T50/672
Abstract: A turbine shroud for a gas turbine engine includes a carrier and blade track. The blade track includes an annular runner and a plurality of inserts that extend radially outward away from the annular runner. The inserts extend through the carrier to couple the annular runner with the carrier.
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公开(公告)号：EP2613015B1
公开(公告)日：2018-11-21
申请号：EP13150281.7
申请日：2013-01-04
Applicant: United Technologies Corporation
CPC classification number: F01D11/12 , F01D5/14 , F01D11/122 , F05D2230/236 , F05D2240/11 , Y02T50/672 , Y02T50/6765 , Y10T29/49236
Abstract: A Blade Outer Air Seal (BOAS) includes a body (80) manufactured of a metal alloy, the body (80) includes a face (80F) opposite a forward interface (82) and an aft interface (84), the face (80F) includes a cavity (92). A non-metallic insert (94) is within the cavity (92) such that the insert (94) is flush with the face (80F).
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Patent Agency Ranking
公开(公告)号：EP2607661B1
公开(公告)日：2018-11-21
申请号：EP12197395.2
申请日：2012-12-17
Applicant: Rolls-Royce plc
Inventor： Broughton, Paul , Peace, Richard , Skinner, Gary , Willmot, Michael , Kennea, Robin
CPC classification number: H05B3/28 , B23P6/005 , B60R16/00 , B60R16/02 , B60R16/0207 , B60R16/0215 , B60R16/08 , B64C3/34 , B64D29/08 , F02C7/00 , F02C7/047 , F02C7/12 , F02C7/141 , F02C7/16 , F02C7/20 , F02C7/224 , F02C7/32 , F05D2260/30 , F05D2300/603 , F16M13/02 , F24H1/105 , H01R12/00 , H01R12/51 , H01R12/515 , H01R12/57 , H01R12/59 , H01R12/592 , H01R12/61 , H02G1/00 , H02G3/00 , H02G3/02 , H02G3/04 , H02G3/0487 , H02G3/32 , H05B1/0236 , H05K1/0393 , H05K7/20 , H05K2201/029 , Y02T50/672 , Y10T29/49002 , Y10T29/49117 , Y10T29/49234 , Y10T29/49236 , Y10T29/49238 , Y10T156/10
Abstract: An electrical raft (200) is provided that has electrical conductors (252) embedded in a rigid material (220). The electrical raft (200) may have other embedded components, such as embedded fluid pipes (210). The electrical raft (200) is provided with a raft map (400) that indicates the location and/or path of components embedded in the electrical raft (200). The raft map (400) can be used to identify the positions of the embedded components, and may also be provided with active elements, such as LEDs, which may be used to indicate an operating state of the systems/components embedded in the electrical raft (200). The raft map (400) may be useful in assembly, repair and fault diagnosis, for example.
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公开(公告)号：EP2949903B1
公开(公告)日：2018-11-14
申请号：EP15154124.0
申请日：2012-12-03
Applicant: LEONARDO S.P.A.
Inventor： Copiello, Diego , Duccini, Gianni , Ferrante, Per Giorgio , Gurioli, Alessandro , Merlo, Emanuele , Pertile, Roberto
CPC classification number: F02C7/045 , F02K1/827 , F05B2260/962 , Y02T50/672
Abstract: The element (26; 126) comprises a front layer (28), which is, at least in a region thereof, sound-permeable; a back layer (30), which is substantially sound-reflecting; and a honeycomb layer (32), which is sandwiched between the front layer (28) and the back layer (30), and defines a mesh structure having a plurality of hollow cells (34) bordering on one another. The cells (34) are provided to resonate within their side walls the sound waves entering through the front layer (28) and being diverted by the back layer (30). The element (26;126) further comprises a plasma actuator (38, 40, 42, 44; 38, 40, 142, 44) provided to generate in the cells (34) a plasma discharge (D) inducing a flow of ionized air particles (A) interacting with the sound waves coming from the front layer (28).
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公开(公告)号：EP2789827B1
公开(公告)日：2018-11-14
申请号：EP11877169.0
申请日：2011-12-07
Applicant: IHI Corporation , IHI Aerospace Co., Ltd.
Inventor： OTSU, Osamu , SHIGENARI, Yu , HARADA, Takashi , MURAKAMI, Tsutomu
CPC classification number: F01D25/28 , F02C7/00 , F02C7/04 , F02C7/32 , F05D2260/31 , F05D2300/603 , F05D2300/614 , F16B5/02 , Y02T50/672
Abstract: A boss for attachment of an auxiliary device to a fan case of an engine is comprised of a pedestal including a plurality of accumulated layers of reinforcement fibers and a matrix combining the reinforcement fibers together, the pedestal comprising a bottom face in a shape capable of being in close contact with an outer periphery of the fan case; and an embedded body embedded in the pedestal and including a combining structure combinable with the auxiliary device.
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公开(公告)号：EP3393764A1
公开(公告)日：2018-10-31
申请号：EP16829413.0
申请日：2016-12-21
Applicant: Safran Aircraft Engines , SAFRAN
Inventor： FABRE, Hubert, Jean-Marie , HELLOT, Jérémy , PHELIPPEAU, Antoine , MARCHAL, Yann, Didier, Simon , DAMBRINE, Bruno, Jacques, Gérard
IPC: B29C70/02 , B29C70/32 , B32B1/00 , B32B5/00 , B29C53/56 , F01D25/24 , B29C70/24 , B29C70/88 , B32B5/18 , B32B5/26
CPC classification number: B29C70/24 , B29C70/88 , B32B5/18 , B32B5/26 , F01D21/045 , F05D2300/60 , Y02T50/672
Abstract: A method of manufacturing a variable-thickness composite-material casing (100) for a gas turbine, comprises: – using three-dimensional or multi-layer weaving to create a fibrous texture (140) in the form of a strip, – winding the fibrous texture (140) in several superposed layers (141, 142, 143, 144) onto a mandrel having a profile corresponding to that of the casing that is to be manufactured, so as to obtain a fibrous preform of a shape corresponding to that of the casing that is to be manufactured, – densifying the fibrous preform using a matrix. During the winding of the fibrous texture (140) onto the mandrel, a textile strip (150) is interposed between the adjacent turns of the fibrous texture, the textile strip (150) having a width smaller than the width of the fibrous texture (140) and delimiting a retention zone of the casing.
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公开(公告)号：EP3000979B1
公开(公告)日：2018-10-31
申请号：EP15186400.6
申请日：2015-09-23
Applicant: United Technologies Corporation
Inventor： CARR, Jesse M. , DUBE, Bryan P.
CPC classification number: F01D9/041 , F01D9/042 , F01D25/246 , F01D25/28 , F02C3/04 , F05D2220/32 , F05D2240/12 , F05D2240/80 , Y02T50/672 , Y02T50/673
Abstract: A vane arc segment (62) includes a radially inner and outer platforms (64,66) and an airfoil (72) mechanically clamped between the platforms (62,64). The airfoil (72) has an airfoil section that extends radially between radially inner and outer fairing platforms (74,76). At least one of the fairing platforms (74,76) includes forward and aft sides (82a,82b), circumferential sides (84a,84b), and a gas path side (86a) and an opposed radial side (86b). The radial side (86b) includes a plurality of protrusions (88) that have faces that are oriented substantially normal to, respectively, radial, tangential, and axial load transmission directions of the airfoil such that the faces, respectively, primarily bear radial, tangential, and axial load transmissions of the airfoil.
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