Heated rigid electrical harness for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-9814101-B2
Application number	US-201314100745-A
Country	US
Kind code	B2
Filing date	Dec 9, 2013
Priority date	Dec 22, 2011
Publication date	Nov 7, 2017
Grant date	Nov 7, 2017

Abstract

A rigid electrical raft has electrical conductors embedded in a rigid material. The electrical conductors transmit electrical signals through the rigid electrical raft, which may form part of an electrical system of a gas turbine engine. The rigid electrical raft also has electrical heating elements embedded therein. The electrical heating elements provide heat which may be used, for example, to prevent condensation and/or ice build-up and/or to raise the temperature of electrical components to be within a desired range.

First claim

We claim:

1. A gas turbine engine comprising:
an electrical harness arranged to transmit electrical signals around the gas turbine engine, wherein the electrical harness comprises a rigid electrical raft that is mounted directly to the gas turbine engine, and the rigid electrical raft comprises:
electrical conductors embedded in a material so as to be surrounded and contacted by, and thereby fixed in position by, the material over their entire length, at least some of the electrical conductors being arranged to transmit the electrical signals; and
electrical heating elements embedded in the material so as to be surrounded and contacted by, and thereby fixed in position by, the material, the electrical conductors and the electrical heating elements being spaced apart, and the electrical heating elements being arranged to provide electrical heating, wherein
a cross-sectional area of the electrical heating elements is smaller than a cross-sectional area of the electrical conductors, and/or the electrical heating elements are constructed from a higher resistance material than the electrical conductors.

2. A gas turbine engine according to claim 1 , further comprising
a temperature sensor arranged to measure a temperature at a specific region of the rigid electrical raft.

3. A gas turbine engine according to claim 1 , further comprising
a fluid passage embedded in the material, wherein at least one of the electrical heating elements is positioned so as to provide heat to the fluid passage.

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

5. A gas turbine engine according to claim 1 , wherein
the electrical heating elements are provided as electrical wires and/or flexible printed circuits.

6. A gas turbine engine according to claim 1 , wherein
the electrical conductors are provided as electrical wires and/or flexible printed circuits.

7. A gas turbine engine according to claim 1 , wherein
at least some of the electrical heating elements are electrically connected to the electrical conductors, such that electrical power is supplied to the electrical heating elements by the electrical conductors.

8. A gas turbine engine according to claim 1 , wherein
the rigid electrical raft is part of an anti-icing system, and the electrical heating elements are constructed and arranged to prevent ice build-up on at least a part of the rigid electrical raft.

9. A gas turbine engine according to claim 1 , wherein
the rigid electrical raft is part of an anti-condensation system, and the electrical heating elements are constructed and arranged to prevent condensation build-up on at least a part of the rigid electrical raft.

10. A gas turbine engine according to claim 1 , wherein
the rigid electrical raft is part of a fluid tank, and
the electrical heating elements are constructed and arranged so as to provide, in use, heating to fluid contained in the fluid tank.

11. A gas turbine engine according to claim 1 , wherein
the rigid electrical raft is part of a rigid electrical raft assembly, the rigid electrical raft assembly further comprising an electrical component mounted to the rigid electrical raft, and
the electrical heating elements are constructed and arranged to heat the electrical component such that it is maintained at a desired temperature, or within a range of desired temperatures.

Assignees

• Rolls Royce Plc

Inventors

• Broughton Paul
• Willmot Michael Christopher
• Dalton Justin Sean

Classifications

• F02C7/224

  Heating fuel before feeding to the burner · CPC title

• Y10T29/49234

  Rotary or radial engine making · CPC title

• H05K7/20

  Modifications to facilitate cooling, ventilating, or heating · CPC title

• Y10T29/49117

  Conductor or circuit manufacturing · CPC title

• H01R12/57

  surface mounting terminals · CPC title