Method and apparatus for automatically providing jet engine thrust ratings to avionic systems

• US 5,893,040 A
• Filed: 05/15/1996
• Issued: 04/06/1999
• Est. Priority Date: 05/15/1996
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Martindale, Ian C., Paulson, Clement Val, Herald, Richard Allen, Gunn, Peter D.
• Primary Examiner(s): NGUYEN, TAN QUANG
• Application Number:
  US08/648,554
• Time in Patent Office: 1,056 Days
• Field of Search: 701/3, 701/4, 701/7, 701/8, 701/10, 701/9, 701/14, 701/15, 701/99, 701/16, 244/234, 244/76 R, 244/178, 244/182, 244/194, 244/195, 73/117.3, 73/117.4, 73/116
• US Class Current: 701/15
• CPC Class Codes: B64D 31/00 Power plant control systems; Arrangement of power plant control systems in aircraft
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G05D 1/0607 specially adapted for aircraft
• CPC Class Codes: G05D 1/101 specially adapted for aircraft

Abstract

An avionic system (102) in which engine thrust rating data is transmitted from electronic engine controllers (108a and 108b) to flight management computer/thrust management computers (120a and 120b) via digital data buses (110a, 110c, and 114) is disclosed. The flight management computer/thrust management computers (120a and 120b) select the proper data set for the specified engine thrust rating upon power-up. If the thrust rating changes, the flight management computer/thrust management computers (120a and 120b) select a new data set corresponding to the new thrust rating as received over the digital data bus (110a, 110c, and 114). This is accomplished without the need to change aircraft wiring. The flight management computer/thrust management computers (120a and 120b) store the thrust rating in nonvolatile memory (126), allowing the flight management computer/thrust management computers (120a and 120b) to use the stored value to initialize relevant settings according to current engine thrust rating.

Claims

1. Apparatus for automatically providing jet engine thrust rating data to aircraft avionic systems comprising:

a data bus;

a jet engine of an aircraft having a plurality of pins in a selected configuration to represent a thrust rating of the jet engine;

an electronic engine controller coupled to said data bus and coupled to the pins of the jet engine for reading thrust rating data directly from the selected configuration of the pins and applying said thrust rating data to said data bus; and

an avionic computer coupled to said data bus for receiving said thrust rating data applied to said data bus by said electronic engine controller, said avionic computer including a memory provided with a plurality of data entries whose values are a function of the thrust rating of the jet engine of said aircraft, said avionic computer determining if the thrust rating data is valid by determining if any of the plurality of data entries stored in the memory of said avionic computer correspond to the thrust rating data, said avionic computer using said thrust rating data received from said electronic engine controller to choose the data entries corresponding to the thrust rating data.

2. The apparatus of claim 1, wherein the memory of said avionic computer includes nonvolatile memory, and wherein said thrust rating data is stored in the nonvolatile memory only if the thrust rating data is valid.

3. The apparatus of claim 2, wherein the avionic computer:

(a) periodically receives new thrust rating data from said electronic engine controller; and

(b) compares the new thrust rating data with the thrust rating data stored in nonvolatile memory and stores the new thrust rating data in nonvolatile memory if the new thrust rating data differs from the stored thrust rating data.

4. The avionic system of claim 3, wherein the jet aircraft includes multiple jet engines and wherein the avionic computer compares the thrust rating data received from the jet engines and reports a fault condition if the thrust rating data does not match.

5. The avionic system of claim 4, wherein the avionic computer compares the thrust rating data received from the jet engines and reports said fault condition only when the jet aircraft is on the ground.

6. The apparatus of claim 2, wherein the avionic computer:

(a) periodically receives new thrust rating data from said electronic engine controller; and

(b) compares the new thrust rating data with the thrust rating data stored in nonvolatile memory and stores the new thrust rating data in nonvolatile memory if the new thrust rating data differs from the stored thrust rating data.

7. The avionic system of claim 6, wherein the jet aircraft includes multiple jet engines and wherein the avionic computer compares the thrust rating data received from the jet engines and reports a fault condition if the thrust rating data does not match.

8. The avionic system of claim 7, wherein the avionic computer compares the thrust rating data received from the jet engines and reports said fault condition only when the jet aircraft is on the ground.

9. The avionic system of claim 1, wherein the jet aircraft includes multiple jet engines and wherein the avionic computer compares the thrust rating data received from the jet engines and reports a fault condition if the thrust rating data does not match.

10. The avionic system of claim 9, wherein the avionic computer compares the thrust rating data received from the jet engines and reports said fault condition only when the jet aircraft is on the ground.

11. A method of automatically providing an engine thrust rating to an avionic computer of an aircraft, said method comprising:

determining a configuration of a plurality of plugs provided in a jet engine to represent a thrust rating of the jet engine;

transmitting a digital data representation of the thrust rating to the avionic computer;

causing the avionic computer to determine if a database includes entries corresponding to said thrust rating; and

causing said avionic computer to store said thrust rating if said database includes entries corresponding to said thrust rating.

12. The method of claim 11, also comprising causing said avionic computer to update said stored thrust rating if a new thrust rating is received by said avionic computer.

13. The method of claim 12, also comprising causing said avionic computer to compare thrust rating data from different jet engines of the aircraft and produce a fault if the thrust rating data does not match.

14. Apparatus for automatically providing jet engine thrust rating data to aircraft avionic systems comprising:

a data bus;

an electronic engine controller coupled to the data bus and coupled to a jet engine of an aircraft for reading data supplied by the jet engine describing the thrust rating of the jet engine and applying the thrust rating data to the data bus;

an avionic computer coupled to the data bus for receiving the thrust rating data applied to the data bus by the electronic engine controller, the avionic computer including a memory provided with data related to the aircraft whose values are a function of the thrust rating of the jet engine of the aircraft, the avionic computer using the thrust rating data to choose the values of the data related to the aircraft; and

wherein the memory of the avionic computer includes nonvolatile memory, and the thrust rating data is stored in the nonvolatile memory, and wherein the avionic computer periodically receives new thrust rating data from the electronic engine controller, and compares the new thrust rating data with the thrust rating data stored in nonvolatile memory and stores the new thrust rating data in nonvolatile memory if the new thrust rating data differs from the stored thrust rating data.

15. The avionic system of claim 14, wherein the jet aircraft includes multiple jet engines and wherein the avionic computer compares the thrust rating data received from the jet engines and reports a fault condition if the thrust rating data does not match.

16. The avionic system of claim 15, wherein the avionic computer compares the thrust rating data received from the jet engines and reports said fault condition only when the jet aircraft is on the ground.

17. Apparatus for automatically providing jet engine thrust rating data to aircraft avionic systems comprising:

an electronic engine controller coupled to a data bus and to each of a plurality of jet engines of an aircraft for reading data supplied by the jet engines describing the thrust rating of each of the jet engines and applying the thrust rating data to the data bus; and

an avionic computer coupled to the data bus for receiving the thrust rating data, the avionic computer comparing the thrust rating data received from the jet engines and reporting a fault condition if the thrust rating data from each of the jet engines does not match, the avionic computer including a memory provided with data related to the aircraft whose values are a function of the thrust rating of the jet engines of the aircraft, the avionic computer using the thrust rating data to choose the values of the data related to the aircraft corresponding to the thrust rating data.

18. The avionic system of claim 17, wherein the avionic computer compares the thrust rating data received from the jet engines and reports said fault condition only when the jet aircraft is on the ground.

19. Apparatus for automatically providing jet engine thrust rating data to aircraft avionic systems comprising:

a data bus;

an electronic engine controller coupled to said data bus and coupled to a jet engine of an aircraft for reading thrust rating data supplied by the jet engine describing the thrust rating of the jet engine and applying said thrust rating data to said data bus;

an avionic computer coupled to said data bus for receiving said thrust rating data applied to said data bus by said electronic engine controller, said avionic computer including a memory provided with a plurality of data entries whose values are a function of the thrust rating of the jet engine of said aircraft, said avionic computer determining if the thrust rating data is valid by determining if any of the plurality of data entries stored in the memory of said avionic computer correspond to the thrust rating data, said avionic computer using said thrust rating data received from said electronic engine controller to choose the data entries corresponding to the thrust rating data, wherein the memory of said avionic computer includes nonvolatile memory, and wherein said thrust rating data is stored in the nonvolatile memory; and

wherein the avionic computer periodically receives new thrust rating data from said electronic engine controller, and compares the new thrust rating data with the thrust rating data stored in nonvolatile memory and stores the new thrust rating data in nonvolatile memory if the new thrust rating data differs from the stored thrust rating data.

20. The avionic system of claim 19, wherein the jet aircraft includes multiple jet engines and wherein the avionic computer compares the thrust rating data received from the jet engines and reports a fault condition if the thrust rating data does not match.

21. The avionic system of claim 20, wherein the avionic computer compares the thrust rating data received from the jet engines and reports said fault condition only when the jet aircraft is on the ground.

22. A method of automatically providing an engine thrust rating defined by a plurality of plugs associated with a jet engine to an avionic computer of an aircraft, said method comprising:

determining, in accordance with a configuration of the plugs, the thrust rating of the jet engine;

transmitting a digital data representation of the thrust rating to the avionic computer;

causing the avionic computer to determine if a database includes entries corresponding to said thrust rating;

causing said avionic computer to store said thrust rating if said database includes entries corresponding to said thrust rating; and

causing said avionic computer to update said stored thrust rating if a new thrust rating is received by said avionic computer.

23. The method of claim 22, also comprising causing said avionic computer to compare thrust rating data from different jet engines of the aircraft and to produce a fault if the thrust rating data does not match.