Aircraft load management center

• US 5,386,363 A
• Filed: 03/25/1993
• Issued: 01/31/1995
• Est. Priority Date: 08/16/1990
• Status: Expired due to Fees

• Current Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Owens, William R., Roettger, Thomas D., Haak, David A.
• Primary Examiner(s): Trans, Vincent N.
• Application Number:
  US08/037,186
• Time in Patent Office: 677 Days
• Field of Search: 364/424.01, 364/424.05, 364/424.06, 364/492, 364/131-133, 364/137-139, 395/725, 395/750, 340/825.06, 340/825.07, 340/825.52, 340/825.53, 307/9.1, 307/43, 307/64, 307/65, 307/85, 307/86, 371/8.1, 371/9.1, 371/11.1
• US Class Current: 701/3
• CPC Class Codes: H02J 13/00016 using a wired telecommunication network or a data transmission bus

Abstract

In an aircraft load management center each LRU is addressed by a separate line. Power control units on an LRU are addressed by a bus to which all the LRUs are connected in parallel. Control and status inputs, and status output lines are connected in parallel to the LRUs. A programmable logic unit on each LRU decodes the controller addresses, couples control and status request inputs to the controller. The load management center automatically connects a status signal to the interface output after each control function input.

Claims

1. A load management center for on-board control of aircraft electrical power, comprising in combination:

a plurality of line replaceable units, each of said line replaceable units including a printed wiring board to which a programmable logic unit and a plurality of power control units are electrically and mechanically coupled, each of said power control units having a control input and a status output means;

an input/output interface for temporarily storing inputs from a computer to the load management center and outputs from the load management center to the computer, said inputs including a line replaceable unit address, a power control unit address, and an operation code, and said outputs including a status code;

decoding means to decode said line replacement unit address;

a dedicated line coupling said decoding means respectively to one of each of said programmable logic units, said decoding means enabling said programmable logic unit to which it is attached in response to a line replaceable unit address;

a bus coupled in parallel to said programmable logic unit electrically and mechanically coupled to each of said plurality of line replaceable units for coupling between said programmable logic unit and said interface, power control unit address, operational code and status code;

a parity detector coupled to said bus, said parity detector generating a retransmit signal on said outputs in response to a parity error on said bus; and

wherein

the computer retransmits said inputs in response to said retransmit signal on said outputs.

2. The load management center of claim 1, wherein said outputs further include a device good/bad signal indicating the operational status of a selected control unit.

3. A load management center for on-board control of aircraft electrical power, comprising in combination:

a plurality of line replaceable units, each of said line replaceable units including a printed wiring board to which a programmable logic unit and a plurality of power control units are electrically and mechanically coupled, each of said power control units having a control input means and a status output means;

an input/output interlace for temporarily storing inputs from a computer to the load management center to the computer, said inputs including a line replaceable unit address, a power control unit address, a control request code and a status request code, and said output including a status output code;

decoding means to decode said line replaceable unit address;

a dedicated line coupling said decoding means respectively to one of each of said programmable logic units, said decoding means enabling said programmable logic unit to which it is attached in response to a line replaceable unit address;

a bus coupled in parallel to said programmable logic unit electrically and mechanically coupled to each of said plurality of line replaceable units for coupling between said programmable logic unit and said interface, power control unit address, operational code and status code;

means to automatically generate said status request code following a control request code;

a parity detector coupled to said bus, said parity detector generating a retransmit signal on said, outputs in response to a parity error on said bus; and

wherein

the computer retransmits said inputs in response to said retransmit signal on said outputs.

4. A load management center for on board control of aircraft electrical power as in claim 3, wherein said input/output interface includes said means to automatically generate said status request code.

5. The load management center of claim 4, wherein said outputs further include a device good/bad signal indicating the operational status of a selected control unit.