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1. 发明授权

US06666025B2 Wall elements for gas turbine engine combustors 有权
标题翻译：燃气轮机发动机燃烧器的壁元件
公开(公告)号：US06666025B2
公开(公告)日：2003-12-23
申请号：US09784162
申请日：2001-02-16
申请人： Michael P Spooner , Anthony Pidcock , Desmond Close
发明人： Michael P Spooner , Anthony Pidcock , Desmond Close
IPC分类号： F23R300
CPC分类号： F23R3/002
摘要： A wall element (29) for a wall structure (21) of a gas turbine engine combustor (15). The wall element (29) comprises a main member (36) with an upstream edge region (30) and a downstream edge region (31). A plurality of heat removal members (38) are provided on the main member (36). The downstream edge (35) of the wall element and/or the downstream facing surface of the heat removal members closest to the downstream edge (35) are provided with a thermally resistant coating.
摘要翻译：一种用于燃气涡轮发动机燃烧器（15）的壁结构（21）的壁元件（29）。壁元件（29）包括具有上游边缘区域（30）和下游边缘区域（31）的主构件（36）。多个散热构件（38）设置在主构件（36）上。壁元件的下游边缘（35）和/或最靠近下游边缘（35）的散热构件的下游侧表面设置有耐热涂层。

2. 发明授权

US07000397B2 Combustion apparatus 有权
公开(公告)号：US07000397B2
公开(公告)日：2006-02-21
申请号：US11020167
申请日：2004-12-27
申请人： Anthony Pidcock , Desmond Close , Michael P Spooner
发明人： Anthony Pidcock , Desmond Close , Michael P Spooner
IPC分类号： F23R3/04
CPC分类号： F23R3/04 , F23R3/002 , F23R2900/03041 , F23R2900/03045
摘要： A wall element for use as part of an inner wall of a gas turbine engine combustor wall structure is of cast construction and includes a plurality of cooling apertures provided therethrough and formed during the casting process. The cooling apertures may be located in positions where they could not be conventionally formed by laser drilling.

3. 发明授权

US06708499B2 Combustion apparatus 有权
公开(公告)号：US06708499B2
公开(公告)日：2004-03-23
申请号：US10079403
申请日：2002-02-22
申请人： Anthony Pidcock , Desmond Close , Michael P Spooner
发明人： Anthony Pidcock , Desmond Close , Michael P Spooner
IPC分类号： F23R360
CPC分类号： F23R3/04 , F23R3/002 , F23R2900/03041 , F23R2900/03045
摘要： A wall element for use as part of an inner wall of a gas turbine engine combustor wall structure is of cast construction and includes a plurality of cooling apertures provided therethrough and formed during the casting process. The cooling apertures may be located in positions where they could not be conventionally formed by laser drilling.

4. 发明授权

US06408628B1 Wall elements for gas turbine engine combustors 有权
标题翻译：燃气轮机发动机燃烧器的壁元件
公开(公告)号：US06408628B1
公开(公告)日：2002-06-25
申请号：US09703666
申请日：2000-11-02
申请人： Anthony Pidcock , Desmond Close , Michael P. Spooner
发明人： Anthony Pidcock , Desmond Close , Michael P. Spooner
IPC分类号： F02C100
CPC分类号： F23R3/002 , F23R2900/03044
摘要： A wall element (29A, 29B) for a combustor (20) of a gas turbine engine (10). The wall element (29A, 29B) defines an axis. In use, the axis is arranged generally parallel to the principal axis of the engine (10). In one aspect, the length of the wall element (29B) along the axis is at least substantially 20% of the length of the wall element (29B) transverse to the axis. In another aspect, the wall element (29A, 29B) has a first pair of opposite edges extending transverse to the axis and a second pair of opposite edges (48, 50) extending transverse to the first pair, at least one of the second pair of edges (48, 50) being angled relative to the axis of the wall element (29A, 29B).
摘要翻译：一种用于燃气涡轮发动机（10）的燃烧器（20）的壁元件（29A，29B）。壁元件（29A，29B）限定一个轴线。在使用中，轴线大致平行于发动机（10）的主轴布置。一方面，沿着轴线的壁元件（29B）的长度至少基本上是横向于轴线的壁元件（29B）的长度的20％。在另一方面，壁元件（29A，29B）具有横向于轴线延伸的第一对相对边缘和横向于第一对延伸的第二对相对边缘（48,50），第二对中的至少一个的边缘（48,50）相对于壁元件（29A，29B）的轴线成角度。

5. 发明授权

US06857275B2 Combustion apparatus 有权
标题翻译：燃烧装置
公开(公告)号：US06857275B2
公开(公告)日：2005-02-22
申请号：US10688875
申请日：2003-10-21
申请人： Anthony Pidcock , Desmond Close , Michael P. Spooner
发明人： Anthony Pidcock , Desmond Close , Michael P. Spooner
IPC分类号： F23R3/00 , F23R3/04 , F02C3/60
CPC分类号： F23R3/04 , F23R3/002 , F23R2900/03041 , F23R2900/03045
摘要： A wall element for use as part of an inner wall of a gas turbine engine combustor wall structure is of cast construction and includes a plurality of cooling apertures provided therethrough and formed during the casting process. The cooling apertures may be located in positions where they could not be conventionally formed by laser drilling.
摘要翻译：用作燃气涡轮发动机燃烧器壁结构的内壁的一部分的壁元件是铸造结构，并且包括多个设置在其中并通过铸造过程形成的冷却孔。冷却孔可以位于它们不能通过激光钻孔通常形成的位置。

6. 发明授权

US06470685B2 Combustion apparatus 有权
标题翻译：燃烧装置
公开(公告)号：US06470685B2
公开(公告)日：2002-10-29
申请号：US09826927
申请日：2001-04-06
申请人： Anthony Pidcock , Desmond Close , Michael P Spooner
发明人： Anthony Pidcock , Desmond Close , Michael P Spooner
IPC分类号： F23R360
CPC分类号： F23R3/002 , F05B2260/201 , F05B2260/202 , F23R3/08
摘要： A wall structure for a gas turbine combustor arranged to have a general direction of fluid flow therethrough includes inner and outer walls defining a space therebetween. The inner wall is made up of a plurality of tiles having axial edges aligned generally with the direction of fluid flow, a gap being defined between axial edges of adjacent tiles. Orifices are provided within the axial edges to direct leakage air passing through the gaps to give the leakage air a flow component in the general direction of fluid flow through the combustor.
摘要翻译：用于燃气轮机燃烧器的壁结构，其布置成具有流体流动的大致方向，其中包括限定其间的空间的内壁和外壁。内壁由多个瓦片组成，其多个瓦片具有大致与流体流动方向对齐的轴向边缘，间隙限定在相邻瓦片的轴向边缘之间。在轴向边缘内设置有孔口，以引导通过间隙的泄漏空气，使得泄漏空气在流体通过燃烧器的流体的大致方向上流动。

7. 发明授权

US06170266B2 Combustion apparatus 有权
标题翻译：燃烧装置
公开(公告)号：US06170266B2
公开(公告)日：2001-01-09
申请号：US09245414
申请日：1999-02-05
申请人： Anthony Pidcock , Desmond Close , Michael P Spooner
发明人： Anthony Pidcock , Desmond Close , Michael P Spooner
IPC分类号： F02G300
CPC分类号： F23R3/08 , F23R3/06 , F23R2900/03041
摘要： A double wall structure for a gas turbine engine has an inner wall comprising a number of tiles. The outer wall is provided with a number of apertures through which air is directed into the space between the two walls. Inclined apertures are provided in the tiles so that cooling air can pass into the combustion chamber and form a cooling film underneath the tile. Each tile is provided with a number of pedestals. The orientation of the inclined apertures is such that the axis of each aperture lies upon an unobstructed channel between the pedestals.
摘要翻译：用于燃气涡轮发动机的双壁结构具有包括多个瓦的内壁。外壁设置有多个孔，空气通过该孔被引导到两个壁之间的空间中。倾斜的孔设置在瓦片中，使得冷却空气可以进入燃烧室并在瓦片下方形成冷却膜。每个瓦片都设有多个基座。倾斜孔的方向使得每个孔的轴线位于基座之间的无障碍通道之间。

8. 发明授权

US07089742B2 Wall elements for gas turbine engine combustors 有权
标题翻译：燃气轮机发动机燃烧器的壁元件
公开(公告)号：US07089742B2
公开(公告)日：2006-08-15
申请号：US10635482
申请日：2003-08-07
申请人： Michael P. Spooner , Anthony Pidcock , Desmond Close
发明人： Michael P. Spooner , Anthony Pidcock , Desmond Close
IPC分类号： F23R3/00
CPC分类号： F23R3/002
摘要： A wall element (29) for a wall structure (21) of a gas turbine engine combustor (15). The wall element (29) comprises a main member (36) with an upstream edge region (30) and a downstream edge region (31). A plurality of heat removal members (38) are provided on the main member (36). The downstream edge (35) of the wall element and/or the downstream facing surface of the heat removal members closest to the downstream edge (35) are provided with a thermally resistant coating.
摘要翻译：一种用于燃气涡轮发动机燃烧器（15）的壁结构（21）的壁元件（29）。壁元件（29）包括具有上游边缘区域（30）和下游边缘区域（31）的主构件（36）。多个散热构件（38）设置在主构件（36）上。壁元件的下游边缘（35）和/或最靠近下游边缘（35）的散热构件的下游侧表面设置有耐热涂层。

9. 发明授权

US06324830B1 Gas turbine engines 失效
标题翻译：燃气涡轮发动机
公开(公告)号：US06324830B1
公开(公告)日：2001-12-04
申请号：US09672446
申请日：2000-09-29
申请人： Michael P Spooner , Anthony Pidcock , Desmond Close
发明人： Michael P Spooner , Anthony Pidcock , Desmond Close
IPC分类号： F02C200
CPC分类号： F23R3/60
摘要： A fuel injector assembly designed to withstand a predetermined impact load resulting from ingestion of a bird or other foreign object into the combustion stage of a gas turbine engine comprises a body member adapted to be mounted adjacent to and to extend into the combustion chamber and an abutment member disposed downstream of the injector assembly in the direction of air flow through the combustion stage, the arrangement being such that the body member moves into contact with the abutment member when subjected to an impact load in excess of the impact load it is designed to withstand.
摘要翻译：设计成承受由鸟或其他异物摄取到燃气涡轮发动机的燃烧阶段而产生的预定冲击载荷的燃料喷射器组件包括适于安装在燃烧室附近并延伸到燃烧室中的主体部件，在喷射器组件的下游设置在通过燃烧级的空气流动的方向上的构件，该构造使得当受到冲击载荷超过其被设计为承受的冲击载荷时，本体构件与抵靠构件接触移动。

10. 发明申请

US20060117755A1 WALL ELEMENTS FOR GAS TURBINE ENGINE COMBUSTORS 有权
标题翻译：气体涡轮发动机组件的壁面元件
公开(公告)号：US20060117755A1
公开(公告)日：2006-06-08
申请号：US10635482
申请日：2003-08-07
申请人： Michael Spooner , Anthony Pidcock , Desmond Close
发明人： Michael Spooner , Anthony Pidcock , Desmond Close
IPC分类号： F23R3/42
CPC分类号： F23R3/002
摘要： A wall element (29) for a wall structure (21) of a gas turbine engine combustor (15). The wall element (29) comprises a main member (36) with an upstream edge region (30) and a downstream edge region (31). A plurality of heat removal members (38) are provided on the main member (36). The downstream edge (35) of the wall element and/or the downstream facing surface of the heat removal members closest to the downstream edge (35) are provided with a thermally resistant coating.
摘要翻译：一种用于燃气涡轮发动机燃烧器（15）的壁结构（21）的壁元件（29）。壁元件（29）包括具有上游边缘区域（30）和下游边缘区域（31）的主构件（36）。多个散热构件（38）设置在主构件（36）上。壁元件的下游边缘（35）和/或最靠近下游边缘（35）的散热构件的下游侧表面设置有耐热涂层。

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