Electrical raft assembly

Patent metadata

Field	Value
Publication number	US-9826575-B2
Application number	US-201213716808-A
Country	US
Kind code	B2
Filing date	Dec 17, 2012
Priority date	Dec 22, 2011
Publication date	Nov 21, 2017
Grant date	Nov 21, 2017

Abstract

An electrical raft assembly for a gas turbine engine is provided. The raft assembly comprises a rigid electrical raft formed of a rigid material that includes an electrical system comprising electrical conductors embedded in the rigid material. The raft assembly further comprises an engine component that is mounted to the electrical raft. The electrical raft includes one or more integral cooling passages which guide a coolant fluid through the raft to cool the engine component.

First claim

We claim:

1. A gas turbine engine comprising:
an electrical raft assembly mounted to the gas turbine engine, the electrical raft assembly comprising:
a rigid electrical raft formed of a rigid material that includes an electrical system comprising electrical conductors, embedded in the rigid material, wherein all of the electrical conductors are embedded in the rigid material so as to be surrounded by, and thereby fixed in position by, the rigid material and so that the electrical conductors do not contact each other and are thus spaced apart from each other;
an electrical connector that is embedded in the rigid material and that is connected to at least one of the embedded electrical conductors; and
an electrical control unit (ECU) that is directly mounted to the rigid electrical raft and that is directly electrically connected to the electrical connector embedded in the rigid material so as to be electrically connected to at least one of the embedded electrical conductors, wherein:
the rigid electrical raft includes one or more integral cooling passages which guide a coolant fluid through the rigid electrical raft to cool the ECU; and
the ECU is only mounted to the gas turbine engine via the rigid electrical raft to which the ECU is directly mounted.

2. The gas turbine engine according to claim 1 , wherein the one or more integral cooling passages are formed by the rigid material.

3. The gas turbine engine according to claim 1 , wherein the rigid material is a rigid composite material.

4. The gas turbine engine according to claim 1 , wherein the one or more integral cooling passages feed the coolant fluid to an array of impingement holes formed in the rigid electrical raft, the coolant fluid exiting the array of impingement holes as cooling jets which impinge on one or more surfaces of the ECU.

5. The gas turbine engine according to claim 1 , wherein the ECU has a double-walled housing and the one or more integral cooling passages feed the coolant fluid into a cavity formed between two walls of the double-walled housing.

6. The gas turbine engine according to claim 5 , wherein an outer wall of the double-walled housing is at least partly formed by a removably replaceable cover to the cavity.

7. The gas turbine engine according to claim 5 , wherein the cavity has internal walls which guide the coolant fluid on a convoluted route through the cavity.

8. The gas turbine engine according to claim 1 , wherein the one or more integral cooling passages guide the coolant fluid on a convoluted route over a heat-withdrawing surface of the ECU.

9. The gas turbine engine according to claim 8 , wherein the heat-withdrawing surface of the ECU has an intimate, heat-conducting relationship with one side of a wall of the rigid electrical raft, the coolant fluid in the convoluted route being in direct contact with a second side of the wall.

10. The gas turbine engine according to claim 1 , wherein the one or more integral cooling passages are arranged to guide a flow of cooling air.

11. The gas turbine engine or a gas turbine engine installation, having the electrical raft assembly according to claim 1 mounted to a part thereof, wherein: the part of the gas turbine engine or gas turbine engine installation to which the electrical raft assembly is mounted is different from the ECU that is directly mounted to the rigid electrical raft.

12. The gas turbine engine or the gas turbine engine installation according to claim 11 , wherein:
the electrical raft assembly is part of an electrical system of the gas turbine engine; and
the electrical system further comprises a flexible cable electrically connected between the electrical raft assembly and another electronic component that is different than the ECU.

13. The gas turbine engine according to claim 1 , wherein the one or more integral cooling passages are configured to cool the ECU.

14. The gas turbine engine according to claim 1 , wherein the ECU that is directly mounted to the rigid electrical raft is secured to the rigid electrical raft by electrically conductive fasteners.

15. A gas turbine engine according to claim 1 , wherein the embedded electrical conductors are surrounded by the rigid material along their entire length.

Assignees

• Rolls Royce Plc

Inventors

• Willmot Michael Christopher
• Broughton Paul
• Peace Richard
• Skinner Gary Alan
• Kennea Robin Charles

Classifications

• Y10T29/49236

  Fluid pump or compressor making · CPC title

• F24H1/105

  formed by the tube through which the fluid flows · CPC title

• H02G3/00

  Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles (installations of bus-bars H02G5/00; overhead installations H02G7/00; installations in or on the ground H02G9/00) · CPC title

• Y10T29/49117

  Conductor or circuit manufacturing · CPC title

• B60R16/08

  fluid · CPC title