Rigid raft

Patent metadata

Field	Value
Publication number	US-9456472-B2
Application number	US-201213716244-A
Country	US
Kind code	B2
Filing date	Dec 17, 2012
Priority date	Dec 22, 2011
Publication date	Sep 27, 2016
Grant date	Sep 27, 2016

Abstract

The present invention provides a rigid raft formed of rigid composite material. The raft has an electrical system and/or a fluid system embedded therein. The raft further has a tank for containing liquid integrally formed therewith. The tank can be formed of the rigid composite material. The tank can be for a gas turbine engine.

First claim

We claim:

1. A gas turbine engine comprising:
a rigid raft being formed of a rigid material, the rigid raft comprising:
multiple electrical conductors embedded in the rigid material, the multiple electrical conductors being at least a part of an electrical system of the gas turbine engine; and
a tank that provides a liquid to a fluid system, the tank being integrally formed with the rigid raft.

2. The gas turbine engine according to claim 1 , wherein the tank is formed of 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 tank is lined.

5. The gas turbine engine according to claim 1 , comprising at least one fluid passage embedded in the rigid material, the least one fluid passage being at least a part of the fluid system.

6. The gas turbine engine according to claim 5 , wherein the at least one fluid passage is in fluid communication with the tank.

7. The gas turbine engine according to claim 1 , wherein:
the tank has a liquid inlet port and a liquid outlet port.

8. The gas turbine engine according to claim 1 , wherein the tank has at least one of the following: a liquid quantity sensor and a liquid temperature sensor.

9. The gas turbine engine according to claim 1 , wherein the rigid raft further comprises a heating system for heating the liquid in the tank.

10. The gas turbine engine according to claim 9 , wherein the heating system includes at least one electrical heating elements.

11. The gas turbine engine according to claim 10 , wherein
the at least one electrical heating element is embedded in the rigid material and electrically connected to at least one of the multiple electrical conductors, such that electrical power for the at least one electrical heating element is provided by the multiple electrical conductors.

12. The gas turbine engine according to claim 1 , wherein the tank is an oil tank or a fuel tank.

13. The gas turbine engine according to claim 1 , wherein:
the electrical system further comprises a flexible cable electrically connected between the rigid raft and another component of the electrical system.

14. The gas turbine engine according to claim 7 , wherein:
the inlet port is fed by a liquid flow passage that is embedded in the rigid material.

15. The gas turbine engine according to claim 7 , wherein:
the outlet port feeds a liquid flow passage that is embedded in the rigid material.

Assignees

• Rolls Royce Plc

Inventors

• Dalton Justin
• Broughton Paul
• Peace Richard
• Skinner Gary Alan
• Kennea Robin Charles

Classifications

• F02C7/047

  Heating to prevent icing · CPC title

• F02C7/00

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• H05B1/0236

  for vehicles · CPC title

• H02G3/04

  Protective tubing or conduits, e.g. cable ladders or cable troughs · CPC title

• Y10T156/10

  Methods of surface bonding and/or assembly therefor · CPC title