-
-
公开(公告)号:EP3282092B1
公开(公告)日:2018-12-12
申请号:EP17183952.5
申请日:2017-07-31
发明人: THIES, Robert
CPC分类号: B64D29/06 , F01D9/02 , F01D9/065 , F01D25/28 , F02C7/04 , F02K1/52 , F02K3/06 , F05D2230/64 , F05D2230/70 , F05D2240/121 , F05D2240/122 , F05D2260/30 , F05D2260/36 , F05D2260/38
-
公开(公告)号:EP3401537A1
公开(公告)日:2018-11-14
申请号:EP18160521.3
申请日:2018-03-07
发明人: KING, Christopher
CPC分类号: F01D25/28 , F01D25/243 , F01D25/30 , F02C7/20 , F02K1/822 , F05D2230/642 , F05D2260/30
摘要: A hanger (12) for mounting an exhaust liner (32) to an exhaust duct (30) is provided. The hanger (12) includes at least one cable (50), a cable flange (52), and a J-shaped liner flange (54). The at least one cable (50) extends lengthwise between a first end (56) and a second end (58). The cable flange (52) has at least one cable aperture (92) configured to receive a portion of the cable (50). The J-shaped liner flange (54) is configured for attachment to the exhaust liner (32). The liner flange (54) and cable flange (52) are configured to mate with one another to prevent substantial relative motion between the cable flange (52) and the liner flange (54) in a first direction (Dl) and in a second direction (D2). The first and second directions (D1,D2) are substantially orthogonal to one another.
-
公开(公告)号:EP2096259B1
公开(公告)日:2018-10-17
申请号:EP09002854.9
申请日:2009-02-27
发明人: Kawakami, Hiroshi , Iwai, Yasunori
IPC分类号: F01D25/26
CPC分类号: F01D25/26 , F01D25/28 , F05D2220/31
摘要: A steam turbine is provided, comprising a rotor and a casing that installs the rotor inside, wherein the casing comprises an upper-half section and a lower-half section, which are coupled with each other by an upper-half flange and a lower-half flange thereof, wherein the upper-half section includes: a semi-cylindrical wrapper plate extending in an axial direction of the rotor, end plates coupled with the wrapper plate, each of the end plate is disposed perpendicular to the rotor, wherein at least one of axial ends of the wrapper plate includes a wrapper plate projecting portion that projects from the corresponding end plates in the axial direction, and a first end plate reinforcing rib disposed on the outside surfaces of the end plates in a peripheral direction of the inner periphery of the wrapper plate; and a plurality of second end plates reinforcing ribs disposed radially on the outside surfaces of the end plates, wherein the second end plates reinforcing ribs couple the wrapper plate projecting portion with the first end plate reinforcing rib.
-
公开(公告)号:EP3177425B1
公开(公告)日:2018-09-26
申请号:EP14753430.9
申请日:2014-08-08
IPC分类号: B23K20/02 , B21D26/021 , B21D53/78 , B23K20/18 , B23K20/24
CPC分类号: B23P11/00 , B21D39/00 , B21D39/03 , B21D53/78 , B23K20/021 , B23K20/18 , B23K20/24 , B23K2101/001 , F01D25/28 , F05D2230/42
摘要: A method (300) of using hot isostatic pressing to join metallic members that form a component in a gas turbine engine is disclosed. The method (300) may include applying (306) a surface treatment to the outer surfaces (14, 15, 16, 20, 22,24) of first and second metallic members (12, 18) based on whether a mechanical or metallurgical joint for the component is desired. Additionally, the method (300) may include aligning (310) the outer surfaces (14, 15, 16, 20, 22, 24) of the first and second metallic members (12, 18) to create a sealed cavity, which encompasses the joint, between the first and second metallic members(12, 18). Once the outer surfaces (14, 15, 16, 20, 22, 24) are aligned, the method (300) may include subjecting (314) the members (12, 18) to hot isostatic pressing such that material from the first metallic member (12) flows into a recess (26) within the second metallic member (18) so as to join the first and second metallic members (12, 18) to form a consolidated component (10). The consolidated component (10) may then be machined and finished (316) for use in a turbine engine.
-
公开(公告)号:EP3004556B1
公开(公告)日:2018-09-26
申请号:EP14753034.9
申请日:2014-08-05
发明人: AHMAD, Fathi , HÄNDLER, Michael , KAMPKA, Kevin , KOWALSKI, Christian , KOWALZIK, Christian , KURT, Nihal , SCHMITT, Stefan , SCHRÖDER, Peter
CPC分类号: F01D11/08 , F01D5/143 , F01D11/14 , F01D25/28 , F02C3/04 , F05D2220/32 , F05D2260/83 , Y02T50/673
-
公开(公告)号:EP3045741B1
公开(公告)日:2018-09-19
申请号:EP16150753.8
申请日:2016-01-11
IPC分类号: F16B31/04
CPC分类号: F01D25/28 , B23P19/04 , F16B31/04 , F16B35/041
摘要: An exemplary pre-assembled fastener device (100) includes a bushing (120, 620) attached to a bolt fastener (108) before the fastener device (100) is used to attach two or more components (102, 104, 106) to one another, thus reducing the probability that the bushing (120, 620) will be inadvertently separated from the bolt fastener (108). The bolt fastener (108) can have an external thread (116), and the bushing (120) can have an internal thread (124, 624) that is configured to fasten to the external thread (116). The internal thread (124, 624) has a profile including a flat crest (130, 630) configured to be spaced apart from the bolt fastener (108), thus preventing the bushing (120, 620) and bolt fastener (108) from interfering from one another when the fastener device (100) is used to attach the components (102, 104, 106) to one another, thus in turn permitting narrow tolerances between those components (102, 104, 106).
-
公开(公告)号:EP3029278B1
公开(公告)日:2018-09-19
申请号:EP15196236.2
申请日:2015-11-25
CPC分类号: F01D25/28 , F01D11/08 , F01D25/24 , F01D25/246 , F05D2220/32 , F05D2230/60 , F05D2240/11 , F05D2240/55 , F05D2240/91
摘要: A support structure (110) for a gas turbine engine (20) includes an axially extending portion (112) that forms a loop. A radially extending portion (114) extends radially inward from the axially extending portion (112). A plurality of retention members (120) are attached to at least one of the axially extending portion (112) and the radially extending portion (114) for retaining a blade outer air seal (72).
-
9.
公开(公告)号:EP3372795A1
公开(公告)日:2018-09-12
申请号:EP18160305.1
申请日:2018-03-06
CPC分类号: F01D25/12 , F01D9/023 , F01D11/003 , F01D11/005 , F01D25/08 , F01D25/243 , F01D25/28 , F01D25/30 , F04D29/545 , F05D2220/32 , F05D2240/35 , F05D2240/55 , F05D2260/201 , F23R3/002 , F23R3/005 , F23R3/60 , F23R2900/00012
摘要: A system includes a web plate (36) axially disposed between a transition piece (32) and a turbine nozzle (34). The web plate (36) includes a radial arm (114) extending in a radial direction between an inner surface (112) and an outer surface (110) of the web plate (36). The radial arm (114), the inner surface (112), and the outer surface (110) are disposed about an axial passage (82) configured to facilitate a flow of combustion products (61) from the transition piece (32) to the turbine nozzle (34). The transition piece (32) is disposed within a compressor discharge cavity (28) configured to receive an oxidant (60). The radial arm (114) includes an upstream face (134) in fluid communication with the compressor discharge cavity (28). The radial arm (114) also includes an arm passage (172, 173, 174, 175) that extends an axial length (182) in an axial direction (72) from the upstream face (134) through at least an axial depth (180) of the radial arm (114). The arm passage (172, 173, 174, 175) is configured to receive a portion of the oxidant (60) through the upstream face (134).
-
公开(公告)号:EP2938862B1
公开(公告)日:2018-09-12
申请号:EP13867850.3
申请日:2013-12-17
CPC分类号: F01D25/28 , F01D25/162 , F01D25/285 , F01D25/30 , F05D2260/31 , Y10T29/49826
摘要: A frame employed in a turbine exhaust case of a gas turbine engine includes a frame outer ring, a frame inner ring, and a plurality of frame struts that connect the frame outer ring to the frame inner ring. The frame outer ring includes a plurality of bosses disposed circumferentially around the frame outer ring, wherein at least one of the plurality of bosses includes a mounting surface that receives and secures a removable bracket to the frame outer ring that supports a weight of the frame.
-
-
-
-
-
-
-
-
-