Fire resistant electronic engine controller

• US 6,771,501 B2
• Filed: 09/19/2002
• Issued: 08/03/2004
• Est. Priority Date: 09/24/2001
• Status: Expired due to Fees

• Current Assignee: Goodrich Control Systems (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Lucas Industries Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Inventors: Cheshire, Anthony, Slack, Geoffrey, Coleman, David
• Primary Examiner(s): Thompson, Gregory D.
• Application Number:
  US10/247,001
• Publication Number:
  US 20030056491A1
• Time in Patent Office: 684 Days
• Field of Search: 60/392.81, 602/39, 607/34, 165/80.3, 165/104.33, 165/185, 174/52-- 5, 361/600, 361/679, 361/688-695, 361/700-715, 361/725-727, 361/728-744
• US Class Current: 361/700
• CPC Class Codes: F01D 25/26 Double casings; Measures against temperature strain in casings
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: F02C 9/46 Emergency fuel control
• CPC Class Codes: F02D 2400/11 After-sales modification devices designed to be used to modify an engine afterwards
• CPC Class Codes: F02D 2400/18 Packaging of the electronic circuit in a casing
• CPC Class Codes: F02D 41/042 for stopping the engine
• CPC Class Codes: F02D 41/3005 Details not otherwise provided for
• CPC Class Codes: F05D 2270/02 to control rotational speed (n)
• CPC Class Codes: F05D 2270/09 to cope with emergencies
• CPC Class Codes: F28D 15/0266 with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers F28D15/043 takes precedence
• CPC Class Codes: H05K 5/0065 wherein modules are associated together, e.g. electromechanical assemblies, modular structures
• CPC Class Codes: H05K 5/0209 Thermal insulation, e.g. for fire protection or for fire containment or for high temperature environments
• CPC Class Codes: H05K 5/0213 Venting apertures; Constructional details thereof
• CPC Class Codes: H05K 7/1412 hold down mechanisms, e.g. avionic racks
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An electronic engine controller is provided in which a backup controller or independent protection module is located in a sealed housing 8 which itself is located within the main housing 4 of the controller. The backup controller is thermally insulated such that it has enhanced durability in the event of a fire or the like occurring in the vicinity of the controller.

Claims

1. An engine controller, characterised by comprising a primary controller for controlling an engine, said primary controller located within a first housing, and an auxiliary controller for controlling the engine, said auxiliary controller located within a second housing supported within the first housing, and in which the auxiliary controller is thermally insulated from the first housing, and in which at least one heat dissipation device is provided to remove heat from the interior of the second housing.

2. An engine controller as claimed in claim 1, in which the second housing sits within a recess in the first housing.

3. An engine controller as claimed in claim 2, in which the second housing is substantially enclosed by the first housing.

4. An engine controller as claimed in claim 1, in which a first wall of the second housing does not face towards the interior of the first housing, and forms support for electrical connectors of the auxiliary controller.

5. An engine controller as claimed in claim 4, in which the first wall is disposed behind a fire shield.

6. An engine controller as claimed in claim 1, in which the at least one heat dissipation device comprises a heat pipe.

7. An engine controller as claimed in claim 6, in which the heat pipe is configured to act as a thermal diode.

8. An engine controller as claimed in claim 6, in which the heat pipe of the or each heat dissipation device is connected to a heat sink located on an external surface of the first housing.

9. An engine controller as claimed in claim 6, in which the return of fluid from the cool end of the heat pipe to the hot end of the heat pipe is by gravity.

10. An engine controller as claimed in claim 1, in which the auxiliary is thermally insulated by thermal insulation within the second housing.

11. An engine controller as claimed in claim 1, in which the auxiliary controller is thermally insulated by thermal insulation provided in the first housing in the vicinity of the second housing.

12. An engine controller as claimed in claim 1, in which electrical connections to electrical connectors for supplying power to the auxiliary controller, and for supplying and removing signals from the auxiliary controller are made via crimped connections.

13. An engine controller as claimed in claim 1, in which the auxiliary controller has limited functionality.

14. An engine controller as claimed in claim 1, in which the auxiliary controller is a protection module to limit the fuel flow to the engine so as to avoid hazardous operation of the engine.

15. An engine controller as claimed in claim 14, in which the protection module provides protection against one or more of engine overspeed and engine overthrust.

16. An engine controller as claimed in claim 1, in which the second housing is, at least in part, defined by walls which define a recess in the first housing.

17. An engine controller as claimed in claim 1, in which electrical circuitry of the auxiliary controller is separated from the environment surrounding the engine controller by two layers of material forming the first and second housings respectively.