Serviceable power modules for a power distribution assembly

• US 6,504,730 B1
• Filed: 07/23/2001
• Issued: 01/07/2003
• Est. Priority Date: 07/23/2001
• Status: Expired due to Term

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Cooney, Robert C., Beneditz, Bruce D., Metzler, Mark W., Dickey, John A.
• Primary Examiner(s): Martin, David
• Assistant Examiner(s): Levi, Dameon E.
• Application Number:
  US09/911,751
• Publication Number:
  US 20030016520A1
• Time in Patent Office: 533 Days
• Field of Search: 361/752-753, 361/759, 361/796-98, 361/801-803, 361/826-828, 361/785, 361/788, 174/50, 174/50.51, 174/52, 174/56, 174/50.6, 174/53, 174/59, 174/72.A, 439/61, 439/62
• US Class Current: 361/826
• CPC Class Codes: H05K 7/1449 with connections to the back board
• CPC Class Codes: H05K 7/1457 Power distribution arrangements

Abstract

A power distribution assembly (PDA) includes AC and/or DC power modules and control modules that are installed within a chassis that is mounted to a vehicle, such as an aircraft. Each module includes a wiring harness connector and a control connector for attachment to a motherboard. A wiring harness is externally mounted to the chassis to provide a simplified connection for the wiring harness connector. The modules can be individually and selectively removed from the chassis for repair or replacement without having to remove the entire PDA from the aircraft. This is accomplished by simply removing the module from the chassis, thereby disconnecting the aircraft interface and motherboard connectors for the selected modules. Also, a common PDA can be utilized on different types of aircraft by installing desired modules within the chassis. Thus, the number and type of modules are selected to meet predetermined specifications for a specific aircraft and then installed within a PDA common to all aircraft.

Claims

1. A power distribution assembly comprising:

a chassis for attachment to a vehicle;

a wiring harness externally mounted to said chassis and including separate busses for AC loads and DC loads; and

a plurality of modules for installation within said chassis with each module including a first connector for attachment to a motherboard and a second connector for attachment to said wiring harness wherein each module is selectively detachable from said chassis for repair or replacement without requiring removal of the other modules.

2. The assembly according to claim 1 wherein said chassis defines a plurality of installation slots for receiving said modules.

3. The assembly according to claim 2 wherein there are more installation slots formed within said chassis than modules installed within said chassis.

4. The assembly according to claim 2 wherein each module includes a plurality of solid state power controllers for controlling multiple DC and/or AC loads within a single module.

8. The assembly according to claim 1 wherein said first and second connectors are mounted to opposite ends of said module with said first connector extending outwardly from said module in a first direction and said second connector extending outwardly from said module in a second direction opposite from said first direction.

9. The assembly according to claim 8 wherein said second connector includes a plurality of configuration pins with both power contacts and signal contacts.

10. The assembly according to claim 9 wherein said power contacts provide a power feed to said module and provide output power to loads requiring high current and wherein said signal contacts provide output power to loads requiring low current and provide said configuration pins for said loads.

11. The assembly according to claim 9 wherein said wiring harness includes a plurality of cables with each cable being strapped to use said configuration pins to uniquely identify each cable.

13. The assembly according to claim 1 wherein said first and second connectors are mounted on a common end of each of said modules.

14. The assembly according to claim 13 wherein first and second connectors are generally simultaneously mated with said motherboard and wiring harness respectively when each of said modules is installed within said chassis.

15. The assembly according to claim 13 wherein said second connector is keyed to ensure the proper module is being installed within said chassis.

16. The assembly according to claim 13 wherein said wiring harness is mounted on an exterior end of said chassis.

19. The assembly according to claim 1 wherein said chassis includes a control section and a power module section.

20. The assembly according to claim 19 wherein said control section includes a first plurality of installation slots for receiving control boards and said power module section includes a second plurality of installation slots for receiving said power modules.

21. The assembly according to claim 20 wherein said second plurality of installation slots is transverse to said first plurality of installation slots.

22. The assembly according to claim 20 wherein said second plurality installation slots is parallel to said first plurality of installation slots.

23. The assembly according to claim 20 wherein said control boards are shop replaceable units and said power modules are line replaceable modules.

24. The assembly according to claim 20 wherein said first plurality of installation slots are intermixed amongst said second plurality of installation slots.

25. The assembly according to claim 1 including a mounting plate for each modules to enclose said module within said chassis.

26. The assembly according to claim 25 including at least one fastener for securing said plate and said module to said chassis.

27. The assembly according to claim 25 wherein said mounting plate includes an identification portion for identifying the type of module enclosed by said mounting plate.

5. A power distrbution assembly comprising:

a chassis for attachment to a vehicle and defining a plurality of installation slots;

a wiring harness externally mounted to said chassis; and

a plurality of modules for installation within said installation slots with each module including a first connector for attachment to a motherboard and a second connector for attachment to said wiring harness such that each module is selectively detachable from said chassis for repair or replacement without requiring removal of the other modules wherein each module includes a plurality of solid state power controllers for controlling multiple DC and/or AC loads within a single module and wherein said plurality of solid state power controllers is unique to each of said modules with some of said plurality of solid state power controllers having a fixed amp per load setting, some of said plurality of solid state power controllers having a programmable amp per load setting, or all of said solid state power controllers having a programmable amp per load setting.

6. The assembly according to claim 5 wherein said second connector includes a plurality of pins for connecting said solid state power controllers to a cable from said wiring harness to identify loads serviced by said cable.

7. The assembly according to claim 6 wherein said programmable amp-per-load settings are set based on cable load identification.

12. A power distribution assembly comprising:

a chassis for attachment to a vehicle;

a wiring harness externally mounted to said chassis and including separate busses for AC loads and DC loads; and

a plurality of modules for installation within said chassis with each module including a first connector mounted to one end of said module for attachment to a motherboard and a second connector mounted to an opposite end of said module for attachment to said wiring harness wherein each module is selectively detachable from said chassis for repair or replacement without requiring removal of the other modules.

17. A power distribution assembly comprising:

a chassis for attachment to a vehicle;

a wiring harness externally mounted to said chassis and including an AC bus and a DC bus that is wired separately from said AC bus; and

a plurality of modules for installation within said chassis with each module including a first connector for attachment to a motherboard and a second connector for attachment to said wiring harness, said first and second connectors being mounted on a common end of each of said modules wherein each module is selectively detachable from said chassis for repair or replacement without requiring removal of the other modules.

18. The assembly according to claim 17 wherein DC loads are shared between said DC bus and an essential bus wired separately from both said buses.

28. A method for distributing power from a vehicle power distribution assembly having a chassis with a plurality of installation slots for receiving modules comprising the steps of:

(a) externally mounting an aircraft wiring harness to the chassis including separating the wiring harness into an AC bus and a DC bus with both busses being independently wired from each other;

(b) attaching a motherboard connector to each module;

(c) attaching an aircraft interface connector to each module;

(d) installing one module into one slot by mating the motherboard connector to a motherboard and mating the aircraft interface connector to the aircraft wiring harness to form a selectively detachable connection to allow the modules to be removed from the chassis for repair or replacement without requiring removal of the other power modules.

29. The method according to claim 28 further including installing a predetermined number of modules into the installation slots wherein the predetermined number varies depending upon vehicle application.

30. The method according to claim 28 further including selectively removing modules for repair or replacement without removing the power distribution assembly from the vehicle.

31. The method according to claim 28 including attaching the motherboard and wiring harness connectors on a common side of the modules.

32. The method according to claim 31 including simultaneously connecting the motherboard connector to the motherboard and the aircraft interface connector to the aircraft wiring harness when the module is inserted within the installation slot.

33. The method according to claim 31 including keying the aircraft interface connector to ensure that the correct module is being installed within the correct installation slot.

34. The method according to claim 31 including mounting the wiring harness on an inwardly facing external surface portion of the chassis.

35. The method according to claim 28 including attaching the motherboard and wiring harness connectors on opposite sides of the module.

36. The method according to claim 28 including separating the chassis into a control section having a first plurality of installation slots for receiving control modules and a power section having a second plurality of installation slots for receiving the power modules.

37. The method according to claim 36 including orientating the first plurality of installation slots parallel to the second plurality of installation slots.

38. The method according to claim 37 including orientating the first plurality of installation slots transversely to the second plurality of installation slots.

39. The method according to claim 28 including controlling multiple DC and/or AC loads within a single power module with solid state power controllers.

43. The method according to claim 28 further including installing a predetermined number of power modules into the installation slots with some modules providing AC power and some modules providing DC power.

44. The method according to claim 28 including utilizing all programmable solid state power controllers for each controller.

40. A method for distributing power from a vehicle power distribution assembly having a chassis with a plurality of installation slots for receiving modules comprising the steps of:

(a) externally mounting an aircraft wiring harness to the chassis;

(b) attaching a motherboard connector to each module;

(c) attaching an aircraft interface connector to each module;

(d) installing one module into one slot by mating the motherboard connector to a motherboard and mating the aircraft interface connector to the aircraft wiring harness to form a selectively detachable connection to allow the modules to be removed from the chassis for repair or replacement without requiring removal of the other power modules; and

(e) utilizing some fixed solid state power controllers and some programmable solid state power controllers for each power module.

41. The method according to claim 40 including identifying service loads for the power module by connection of the wiring harness connector to the wiring harness.

42. The method according to claim 41 including programming the programmable solid state power controllers after identification of the service loads.