Electrically coupling an avionics line replaceable unit with an avionics test station

• US 6,350,130 B1
• Filed: 06/01/1999
• Issued: 02/26/2002
• Est. Priority Date: 06/01/1999
• Status: Expired due to Term

• Current Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Original Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Inventors: Eller, Roger D.
• Primary Examiner(s): Sircus, Brian
• Assistant Examiner(s): Nguyen, Son V.
• Application Number:
  US09/323,776
• Time in Patent Office: 1,001 Days
• Field of Search: 439/61, 439/248, 439/247, 324/760, 324/158.1, 324/73.1
• US Class Current: 439/61
• CPC Class Codes: G01R 1/0408 Test fixtures or contact fields; Connectors or connecting adaptors; Test clips; Test sockets G01R1/067 takes precedence; mass production testing systems G01R31/59; testing of connections G01R31/66; for testing printed circuit boards G01R31/2808
• CPC Class Codes: G01R 31/008 on air- or spacecraft, railway rolling stock or sea-going vessels
• CPC Class Codes: H01R 12/52 connecting to other rigid printed circuits or like structures
• CPC Class Codes: H01R 12/79 connecting to rigid printed circuits or like structures
• CPC Class Codes: H01R 2201/20 for testing or measuring purposes
• CPC Class Codes: H05K 7/1424 Card cages

Abstract

An avionics test unit adapter for interfacing between an avionics test station and an avionics line replaceable unit, where the test unit adapter is blind mated with both. The test unit adapter has therein at least two rigid circuit cards used for signal distribution or transmission. The two rigid circuit cards being rigidly coupled to each other through an edge connector while each circuit card is mounted within the test unit adapter with the ability to float therein in at least three orthogonal directions.

Claims

1. A system of a type having an avionics rack, on an aircraft, for containing a plurality of avionics line replaceable units, and further

having a first rack/line replaceable unit connector, said plurality of avionics line replaceable units comprising a first avionics replaceable unit, coupled to said avionics rack, the improvement comprising:

a test unit adapter having a second rack/line replaceable unit connector, a test unit adapter/test station connector, and a rigid electrical connection between two printed circuit boards, disposed therebetween;

said test unit adapter is disposed outside of said aircraft;

a second avionics line replaceable unit, having an avionics line replaceable unit rear blind mating connector thereon, which has a predetermined configuration so as to be readily mated with said first rack/line replaceable unit connector, said predetermined configuration further configured so as to be readily mated to said second rack/line replaceable unit connector; and

,

a test station coupled to said test unit adapter, said test station for testing said second avionics line replaceable unit.

2. An adapter comprising:

a first connector coupled with an avionics line replaceable unit;

a second connector coupled with an avionics test station disposed outside of an aircraft; and

,

a plurality of rigid circuit boards, disposed in said adapter, and electrically coupling said first connector and said second connector, where said rigid circuit boards are connected to each other through a rigid electrical connection.

3. The adapter of claim 2 wherein said rigid electrical connection is a pin and socket connector.

4. The adapter of claim 3 wherein said pin and socket connector is an edge-mounted pin and socket connector.

5. The adapter of claim 2 wherein each of said plurality of circuit boards is simultaneously mounted to said adapter and allowed to float in said adapter in at least two orthogonal directions.

6. A rigid inter-connection test unit adapter comprising:

said test unit adapter is disposed outside of an aircraft;

an avionics line replaceable unit test unit adapter/line replaceable unit connector for coupling with an avionics line replaceable unit;

a mother board mounted in said rigid inter-connection test unit adapter and having an ability to float in at least one direction;

a rigid test unit adapter/test station connector assembly mounted therein and having an ability to float in at least one direction;

said mother board and said rigid test unit adapter/test station connector assembly are coupled to each other through a rigid electrical connection.

7. The rigid inter-connection test unit adapter of claim 6 wherein said rigid electrical connection is an edge-mounted pin and socket connector, where a pin is disposed on said rigid test unit adapter/test station connector assembly, and a socket is disposed on said mother board.

8. A rigid inter-connection test unit adapter of claim 6 wherein said rigid electrical connection is an edge-mounted pin and socket connector where a pin is disposed on said mother board, and a socket is disposed on said rigid test unit adapter/test station connector assembly.

9. A rigid inter-connection test unit adapter of claim 8 wherein said rigid test unit adapter/test station connector assembly includes a floating pin for mating with a socket in a test station.

10. An avionics test unit adapter comprising:

said avionics test unit adapter is disposed outside of an aircraft,

means for electrically coupling with an avionics line replaceable unit;

means for electrically coupling with an avionics test station;

means for rigidly coupling a plurality of circuit boards to provide a signal path between said means for electrically coupling with an avionics line replaceable unit and said means for electrically coupling with an avionics test station.

11. The avionics test unit adapter of claim 10 wherein said means for rigidly coupling comprises a first circuit card and a second circuit card.

12. The avionics test unit adapter of claim 11 further comprising a frame wherein said first circuit card is mounted in said frame.

13. The avionics test unit adapter of claim 12 wherein said first circuit card is allowed to float in at least one direction within said frame.

14. The avionics test unit adapter of claim 13 wherein said second circuit card is allowed to float in at least one direction within said frame.

15. The avionics test unit adapter of claim wherein said first circuit card and said second circuit card are coupled through an edge-mounted pin and socket connector, and both said first circuit card and said second circuit card are allowed to float in unison in at least one direction.

16. The avionics test unit adapter of claim 15 wherein said means for electrically coupling with an avionics test station includes a floating pin coupled to said first circuit card.

17. A method of connecting an avionics line replaceable unit with an avionics test station comprising the steps of:

providing a first connector coupled with an avionics line replaceable unit;

providing a second connector coupled with an avionics test station which is disposed outside of an aircraft;

providing a mother board for distributing signals provided by said first connector and said second connector;

coupling said mother board with said first connector;

rigidly coupling said mother board with a second circuit board; and

,

coupling said second circuit board with said second connector.

18. The method of claim 17 wherein said step of rigidly coupling said mother board to said second circuit board uses a pin and socket connector.

19. The method of claim 18 wherein said step of providing a mother board includes mounting said mother board in a frame with an ability to float in at least one direction.

20. The method of claim 19 wherein said step of coupling said second circuit board with said second connector includes using a floating pin which mates with said avionics test station.