Electronic unit mounting

Patent metadata

Field	Value
Publication number	US-9699833-B2
Application number	US-201213716439-A
Country	US
Kind code	B2
Filing date	Dec 17, 2012
Priority date	Dec 22, 2011
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

An electrical assembly 600 comprising an electrical raft 200 and an electronic unit 300 is provided to a gas turbine engine 10 . The electrical raft 200 has electrical conductors 252 embedded in a rigid material 220 , which may be a rigid composite material. The electrical conductors 252 are in electrical contact with the electronic unit 300 . When the electronic unit 300 is installed, at least a part 310 of it forms a part of a gas-washed surface of the engine 10 . The electronic unit 300 is then easily accessible from the engine 10 , and potentially complex and/or heavy access doors/panels may not be required.

First claim

We claim:

1. A gas turbine engine comprising:
a nacelle; and
an electrical assembly that comprises:
an electrical raft having a rigid material with at least one electrical conductor embedded therein; and
an electronic unit mounted on the electrical raft and in electrical connection with the electrical raft,

wherein:
the electrical raft is mechanically fixed to a component of the gas turbine engine; and
at least a part of the electronic unit has an external surface that is flush with an external surface of the nacelle and is exposed to free-stream flow.

2. A gas turbine engine according to claim 1 , wherein:
the electrical raft is provided with a first electrical connector in electrical contact with at least one of said embedded electrical conductors, the first electrical connector being fixed relative to the electrical raft;
the electronic unit is provided with a second electrical connector, that is complimentary to the first electrical connector, the second electrical connector being fixed relative to the electronic unit; and
the electrical raft and the electronic unit are in electrical connection through the first and second electrical connectors.

3. A gas turbine engine according to claim 1 , wherein the electronic unit is mechanically fixed to another component of the gas turbine engine.

4. A gas turbine engine according to claim 3 , wherein the electronic unit and the electrical raft are mechanically fixed to different components of the gas turbine engine.

5. A gas turbine engine according to claim 1 , wherein the electronic unit forms at least a part of an external gas-washed surface that, in use, is gas-washed by free-stream flow.

6. A gas turbine engine according to claim 1 , wherein:
the gas turbine engine is a turbofan gas turbine engine having a bypass duct; and
the electronic unit forms at least a part of a gas-washed surface of the bypass duct.

7. A gas turbine engine according to claim 1 , wherein the external surface of the electronic unit forms a substantially continuous gas-washed surface with the external surface the nacelle.

8. A gas turbine engine according to claim 1 , wherein the electrical raft is mounted inside the nacelle.

9. A gas turbine engine according to claim 1 , wherein the electronic unit is mechanically fixed to the nacelle.

10. A gas turbine engine according to claim 1 , wherein the gas turbine engine comprises a fan and a fan case, and the electrical raft is mechanically fixed to the fan case.

11. A gas turbine engine according to claim 1 , wherein:
the electrical assembly forms part of a gas turbine engine electrical system; and
the electrical raft comprises a linking electrical connector through which the electrical assembly is electrically connected to a remainder of the gas turbine engine electrical system.

12. A gas turbine engine according to claim 11 , further comprising at least one flexible cable electrically connected to the linking electrical connector of the electrical raft and to the remainder of the gas turbine engine electrical system to thereby electrically connect the electrical assembly to the remainder of the gas turbine engine electrical system.

13. A gas turbine engine according to claim 1 , wherein the electrical raft comprises a plurality of said electrical conductors provided in a flexible printed circuit as electrically conductive tracks in a flexible substrate.

14. A method of attaching an electronic unit to a gas turbine engine, the gas turbine engine comprising a nacelle and an electrical raft,
the method comprising:
slotting the electronic unit into an opening formed in a gas-washed surface of the nacelle; and
electrically connecting the electronic unit to the electrical raft, the electrical raft comprising a rigid material with at least one electrical conductor embedded therein;

wherein
an external surface of the electronic unit, when inserted into the opening, is flush with an external surface of the nacelle that completes the gas-washed surface in which the opening is formed; and
the external surface of the electronic unit is exposed to free-stream flow.

15. A method of attaching an electronic unit to a gas turbine engine according to claim 14 , wherein:
the electronic unit and the electrical raft comprise complimentary connectors configured such that electrically connecting the electronic unit to the electrical raft is performed automatically when slotting the electronic unit into the opening.

16. A gas turbine according to claim 1 , wherein the electronic unit is mechanically fixed to the component of the gas turbine engine.

Assignees

• Rolls Royce Plc

Inventors

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

Classifications

• F02C7/12

  Cooling of plants (of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P) · CPC title

• H05K7/20

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

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

• F02C7/224

  Heating fuel before feeding to the burner · CPC title

• B60R16/02

  electric {constitutive elements} · CPC title