-
公开(公告)号：US10920619B2
公开(公告)日：2021-02-16
申请号：US16446242
申请日：2019-06-19
IPC分类号： F01D25/24
摘要： A part for a turbine engine, the part having a general annular shape about an axis of revolution, this part including a first annular shrink-fitted mounting flange and comprising an annular row of orifices for the passage of screws, this part being made by casting and including protruding pads required for the control and the manufacture of the part by casting, wherein the pads are located on the flange and in that each comprises a thread configured to engage with an extraction screw of the flange.
-
公开(公告)号：US10760436B2
公开(公告)日：2020-09-01
申请号：US15579006
申请日：2016-05-27
摘要： An annular turbine engine combustion chamber wall including air admission orifices to create zones of steep temperature gradient, and cooling orifices to enable the air flowing on the cold side to penetrate to the hot side in order to form a film of cooling air along the annular wall, the annular wall being further includes, in the zones of steep temperature gradient, multi-perforation holes having respective bends of an angle α greater than 90°, the angle α being measured between an inlet axis Ae and an outlet axis As of the multi-perforation hole, the outlet axis of the multi-perforation hole being inclined at an angle θ3 relative to the normal N to the annular wall through which the multi-perforation holes with bends are formed, in a “gyration” direction that is at most perpendicular to the axial flow direction D of the combustion gas.
-
公开(公告)号：US11808456B2
公开(公告)日：2023-11-07
申请号：US17431254
申请日：2020-02-19
CPC分类号： F23R3/283 , F02C3/00 , F23R3/50 , F23R3/60 , F05D2220/32 , F05D2230/60 , F05D2240/35 , F23R2900/00017
摘要： A combustion chamber includes a bottom wall having at least one opening, at least one sleeve mounted upstream of the bottom wall and fixed to the bottom wall, a closing ring defining an annular groove with the sleeve and fixed to the sleeve, and at least one air and fuel injection system having an axis, mounted in the opening of the bottom wall. The injection system has an annular flange extending radially with respect to the axis and is mounted in the groove with radial clearance. A baffle is situated downstream of the bottom wall and is fixed to the sleeve and/or to the bottom wall.
-
公开(公告)号：US11280494B2
公开(公告)日：2022-03-22
申请号：US16412958
申请日：2019-05-15
摘要： An assembly for a combustion chamber of a turbomachine. The assembly comprises an annular shell extending along a longitudinal axis, the shell having an inner wall intended to be turned towards a furnace of the combustion chamber and an outer wall opposite the inner wall and a projecting element extending radially from an area of the outer wall. The shell has at least one deflector projecting from the outer wall and located downstream of the projecting element with respect to a direction of gas flow along the outer wall, oriented along the longitudinal axis. The deflector extends circumferentially. Perforations are provided axially between the projecting element and the or each deflector.
-
公开(公告)号：US11971174B2
公开(公告)日：2024-04-30
申请号：US17610893
申请日：2020-05-14
IPC分类号： F23R3/50
CPC分类号： F23R3/50 , F23R2900/00017
摘要： A turbomachine has the upstream portion of the annular combustion chamber is fixed to the outer housing via individual pins with a swivel connection.
The swivel connection is established between the pin and a part of the outer housing.
The pin is slidable radially, or with a radial component, by a slide established between the pin and a tubular part of the outer annular shroud and/or the annular wall of the chamber bottom.-
公开(公告)号：US11480340B2
公开(公告)日：2022-10-25
申请号：US17256963
申请日：2019-06-28
摘要： The present disclosure provides devices for guiding an element in a combustion chamber wall opening. Between the welds or brazes joining a bushing with a cup and the trajectory of the ring edge, an intermediate space is reserved in an internal annular groove for said welds or brazes to protrude into, so that said welds or brazes lie outside the trajectory of the ring edge.
-
公开(公告)号：US20210131666A1
公开(公告)日：2021-05-06
申请号：US17256963
申请日：2019-06-28
摘要： The present disclosure provides devices for guiding an element in a combustion chamber wall opening. Between the welds or brazes joining a bushing with a cup and the trajectory of the ring edge, an intermediate space is reserved in an internal annular groove for said welds or brazes to protrude into, so that said welds or brazes lie outside the trajectory of the ring edge.
-
公开(公告)号：US20200033004A1
公开(公告)日：2020-01-30
申请号：US16520838
申请日：2019-07-24
发明人： Jacques Marcel Arthur Bunel , William Louis Rodolphe Dousse , Dan Ranjiv Joory , Benjamin Frantz Karl Villenave
摘要： A combustion chamber for a gas turbomachine. The combustion chamber comprising inner and outer walls, a chamber bottom, and a heat shield arranged downstream of the chamber bottom, to protect it thermally. The inner and outer walls and the heat shield form a one-piece unit.
-
公开(公告)号：US10247101B2
公开(公告)日：2019-04-02
申请号：US15391578
申请日：2016-12-27
摘要： A device for mounting a spark plug in a combustion chamber of a gas turbine engine includes a chimney including a collar extending radially inwards, a washer fastened on an axial end of the chimney so as to project towards the inside of the chimney, and a bushing forming a spark plug guide and including an inner collar and an outer collar that are axially spaced apart from each other by a cylindrical portion. Each collar extends radially outwards. The bushing is floatingly mounted inside the chimney with its collars axially positioned between the collar of the chimney and the washer. The inner collar comes in operation to bear against the collar of the chimney. The outer collar presents an outside diameter (d1) greater than the inside diameter (d2) of the washer.
-
公开(公告)号：US11952901B2
公开(公告)日：2024-04-09
申请号：US17642019
申请日：2020-09-11
CPC分类号： F01D11/12 , F01D11/001 , F01D11/003 , F01D11/005 , F05D2220/32 , F05D2240/55
摘要： A turbomachine sealing ring has an axis of revolution and includes an annular support, an annular coating made of abradable material which is carried by the support, and an annular thermal protection plate which is carried by the support. The ring is divided into sectors and has a plurality of ring sectors disposed circumferentially next to one another about the axis. Each ring sector has a support sector, a coating sector, and a plate sector. Each plate sector ling includes a flat tab that is pressed against a face of the corresponding support sector and is fixed to this face by brazing. The tab is inserted into a through-slot in the support sector in order to improve its integrity in operation.
-
-
-
-
-
-
-
-
-
搜索结果
20 条记录 (耗时 0.016 秒)
