초록 ▼

A method and a system for indicating a target idle running speed, a predicted core speed, a predicted time to running, current engine state or automation modes of an operating aircraft engine, and indicating that the current core speed of the aircraft engine is less than a target idle running speed

A method and a system for indicating a target idle running speed, a predicted core speed, a predicted time to running, current engine state or automation modes of an operating aircraft engine, and indicating that the current core speed of the aircraft engine is less than a target idle running speed or is abnormally decreasing towards a target idle running speed. The indicators may be visual or aural. The visual indicators may include graphical or numeric symbols indicating the target idle running speed, the direction of core speed change, the predicted core speed at some future time, or current engine state or automation mode.

대표청구항 ▼

The invention claimed is: 1. A method for communicating aircraft engine information to a pilot, comprising the steps of generating indicators that indicate the current core speed of an operating aircraft engine, a target idle running speed different than said current core speed, and the predicted t

The invention claimed is: 1. A method for communicating aircraft engine information to a pilot, comprising the steps of generating indicators that indicate the current core speed of an operating aircraft engine, a target idle running speed different than said current core speed, and the predicted time duration to idle running, wherein said indicators are visual or aural. 2. The method as recited in claim 1, wherein said indicator that indicates said target idle running speed is generated when the current core speed is less than said target idle running speed. 3. The method as recited in claim 1, wherein said indicator that indicates said target idle running speed is generated when the current core speed is abnormally decreasing toward said target idle running speed. 4. The method as recited in claim 1, wherein said indicator that indicates said target idle running speed is generated when the current core speed of the aircraft engine is greater than said target idle running speed and certain abnormal conditions are present. 5. The method as recited in claim 1, further comprising the step of generating an indicator that indicates the direction in which the current core speed is changing, said indicator being biased to show very small levels of positive engine acceleration and not display relatively small levels of deceleration. 6. The method as recited in claim 1, further comprising the step of generating an indicator that indicates the predicted/estimated core speed at some predetermined future time. 7. The method as recited in claim 1, further comprising the step of generating an indicator that indicates the current engine state or automation mode for engine start, recovery, or operation. 8. The method as recited in claim 1, further comprising the step of displaying a scale for relating a symbol or symbols that indicate the current core speed of the aircraft engine to a symbol or symbols that indicate said target idle running speed. 9. The method as recited in claim 1, wherein the current core speed of the aircraft engine and said target idle running speed are indicated by respective numeric values. 10. A method for communicating aircraft engine information to a pilot, comprising the following steps: (a) calculating the current core speed and speed rate of change of an operating aircraft engine; (b) generating a first indicator that indicates said calculated current core speed while the aircraft engine is operating; and (c) generating second and third indicators at least whenever the operational state of the aircraft engine is a subidle condition, said second indicator indicating a target idle running speed of the aircraft engine different than said current core speed, and said third indicator indicating the predicted time duration to idle running, wherein said first through third indicators are visual or aural. 11. The method as recited in claim 10, wherein said first and second indicators are generated when the current core speed is less than said target idle running speed. 12. The method as recited in claim 10, wherein said first and second indicators are generated when the current core speed is abnormally decreasing toward said target idle running speed. 13. The method as recited in claim 10, wherein said first and second indicators are generated when the current core speed of the aircraft engine is greater than said target idle running speed and certain abnormal conditions are present. 14. The method as recited in claim 10, further comprising the step of displaying a reference scale, said first and second indicators being graphical indicators respectively located along said reference scale. 15. The method as recited in claim 14, wherein said reference scale has a first color and said second indicator has a second color different than said first color. 16. The method as recited in claim 14, wherein the color or graphical format of said second indicator changes when the current core speed is no longer less than said target idle running speed. 17. The method as recited in claim 10, wherein said first and second indicators are numeric. 18. The method as recited in claim 10, further comprising the step of generating a fourth indicator that indicates the direction in which the current core speed is changing, said fourth indicator being biased to show very small levels of positive engine acceleration and not display relatively small levels of deceleration. 19. The method as recited in claim 10, further comprising the step of generating a fourth indicator that indicates predicted/estimated core speed at some predetermined future time. 20. The method as recited in claim 10, further comprising the step of generating a third indicator that indicates current engine state or automation mode for engine start, recovery, or operation. 21. A system for indicating aircraft engine information onboard an aircraft, comprising: an indicator device that can be controlled electronically to generate indicators; and a processor programmed to control said indicator device to generate indicators indicating the current core speed of an operating aircraft engine, a target idle running speed different than said current core speed, and the predicted time duration to idle running in response to receipt of a signal indicating that a predetermined operating condition is present. 22. The system as recited in claim 21, wherein said predetermined operating condition is that the current core speed is less than said target idle running speed. 23. The system as recited in claim 21, wherein said predetermined operating condition is that the current core speed is abnormally decreasing towards said target idle running speed. 24. The system as recited in claim 21, wherein said predetermined operating condition is disagreement between the commanded and indicated thrust. 25. The system as recited in claim 21, wherein said processor is further programmed to control said indicator device to generate an indicator indicating the direction in which the current core speed is changing. 26. The system as recited in claim 21, wherein said processor is further programmed to control said indicator device to generate an indicator indicating the predicted/estimated core speed at some predetermined future time. 27. The system as recited in claim 21, wherein said processor is further programmed to control said indicator device to generate an indicator indicating the current engine state or automation mode for engine start, recovery, or operation.