Integrated time/limit exceedance cue system

• US 5,339,244 A
• Filed: 08/13/1992
• Issued: 08/16/1994
• Est. Priority Date: 08/13/1992
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Wright, Gregory P., Lappos, Nicholas D., Stiles, Lorren Jr.
• Primary Examiner(s): Black, Thomas G.
• Assistant Examiner(s): MCFADDEN, SUSAN IRIS
• Application Number:
  US07/929,323
• Time in Patent Office: 733 Days
• Field of Search: 364/426.04, 340/945, 340/963, 340/969, 340/978, 340/980, 340/722, 340/753, 395/141, 395/159
• US Class Current: 701/14
• CPC Class Codes: G05D 1/0066 for limitation of acceleration or stress

Abstract

An integrated time/limit exceedance cue system including a plurality of dedicated subsystem sensors, a processing unit, and a graphics generating/processing unit that is operative to generate an event dependent, time varying visual cue indicative of the exceedance of an established normal operating limit of a specific aircraft subsystem and operation thereof in a time critical exceedance condition. The time varying visual cue provides a relative indication of the elapsed time of operation of the specific subsystem in the time critical exceedance condition. The time varying visual cue is a symbolic image in the form of an outline, having a predetermined length, that defines a void region. The void region is proportionately opaqued or "filled in" in correspondence with the elapsed time of operation of the specific subsystem in the time critical exceedance condition. The outline of the visual cue may be shaped and/or have a spatial orientation that is cognitively connected to the particular subsystem and/or to a symbolic image or display representing the specific generated status data provided by the dedicated subsystem sensors for monitoring the operation of the particular subsystem. The cue system may provide a corrective action cue in conjunction with the time varying visual cue that provides information as to the appropriate recovery procedure to restore the particular subsystem to operation within its established normal operating range.

Claims

1. An integrated time/limit exceedance cue system for alerting a pilot that a specific aircraft subsystem has exceeded an established operating range and is operating in a time critical exceedance condition defined by a predetermined time limit, comprising:

sensor subsystem means for monitoring operation of aircraft subsystems and providing parameter signals representing operating conditions of the aircraft subsystems;

processing means for comparing said parameter signals against stored threshold values defining limits for established operating ranges of the aircraft subsystems and for generating an activation signal indicative of exceedance of the established operating range by the specific aircraft subsystem and operation thereof in the time critical exceedance condition; and

graphics generating/processing means operative in response to said activation signal for generating a visual cue, said visual cue being a symbolic image defined by an outline having a predetermined length and wherein said outline defines a void region, said symbolic image alerting the pilot that the specific aircraft subsystem has exceeded the established operating image and is operating in the time critical exceedance condition;

said graphics generating/processing means being further operative for continually modifying said visual cue by filling in said void region thereof in proportion to said predetermined length of said outline and elapsed time of operation of the specific aircraft subsystem in the time critical exceedance condition with respect to the predetermined time limit thereof to provide the pilot with a time varying visual cue wherein said filled-in void region of said outline is a relative visual indication of the elapsed time of operation of the specific aircraft subsystem within the time critical exceedance condition in relative proportion to the predetermined time limit; and

wherein

said void region which is unfilled provides a relative visual indication to the pilot of time remaining in the predetermined time limit.

2. The integrated time/limit exceedance cue system of claim 1, wherein said graphics generating/processing means is further operative to generate a baseline operating parameter symbolic image for the specific aircraft subsystem operating in the time critical exceedance condition and is further operative to generate said symbolic image comprising said visual cue superposed in combination over said baseline operating parameter symbolic image.

3. The integrated time/limit exceedance cue system of claim 1 wherein said graphics generating/processing means is operative to generate an aural warning in conjunction with said time varying visual cue to indicate that operation of the specific aircraft subsystem in the time critical exceedance condition has exceeded a predetermined percentage of the predetermined time limit of the time critical exceedance condition.

4. The integrated time/limit exceedance cue system of claim 1, wherein said symbolic image comprising said visual cue has a configuration cognitively associated with the specific aircraft subsystem operating in the time critical exceedance condition.

5. The integrated time/limit exceedance cue system of claim 4 wherein the aircraft is a helicopter, the specific subsystem operating in the time critical exceedance condition is the powerplant of the helicopter, and said configuration of said symbolic image comprising said visual cue is a collective control column.

6. The integrated time/limit exceedance cue .system of claim 5 wherein said graphics generating/processing means is further operative for generating a corrective action visual cue in conjunction with said collective control column symbolic image to indicate a recovery procedure to restore the helicopter powerplant to operation within the established operating range.

7. The integrated time/limit exceedance cue system of claim 6 wherein said corrective action visual cue is a triangle, and wherein said triangle points downwardly to indicate the proper recovery is to lower the collective control column to restore the helicopter powerplant to operation within the established operating range and points upwardly to indicate the proper recovery is to raise the collective control column to restore the helicopter powerplant to operation within the established operating range.

8. The integrated time/limit exceedance cue system of claim 1 wherein said processing means is operative to generate a reset signal once the pilot has taken corrective action to restore the specific aircraft subsystem to operation within the established operating range, and wherein said graphics generating/processing means is operative in response to said reset signal to blank out said time varying visual cue.

9. The integrated time/limit exceedance cue system of claim 8 wherein the specific aircraft subsystem has an established recovery period defined by a predetermined time interval, and wherein said graphic generating/processing means is further operative in response to said reset signal for clocking the predetermined time interval of the established recovery period of the specific aircraft subsystem.

10. The integrated time/limit exceedance cue system of claim 9 wherein

said processing means is operative to generate a reinitiate signal if the specific aircraft subsystem is re-operated in the time critical exceedance condition prior to elapse of the predetermined time interval of the established recovery period of the specific aircraft subsystem;

and wherein

said graphics generating/processing means is operative in response to said reinitiate signal to provide a partially modified visual cue to alert the pilot that the specific aircraft subsystem has reexceeded the established operating range and is operating in the time critical exceedance condition, said partially modified visual cue providing a visual indication of exceedance elapsed time utilizing a set of recovery equations based upon the predetermined time limit of the time critical exceedance condition, the actual elapsed operating time in the prior time critical exceedance condition, the established recovery period, and actual operating time in the established recovery period; and

wherein

said graphics generating/processing means is operative for continually modifying said partially modified visual cue to provide said time varying visual cue indicative of remaining time of operation of the specific aircraft subsystem within the time critical exceedance condition relative proportionately to a time period defined by the predetermined time limit minus said exceedance elapsed time.

11. The integrated time/limit exceedance cue system of claim 10 wherein said set of recovery equations comprises ##EQU2## where T is an initial time setting, Y represents the actual elapsed operating time in the prior time interval condition, R is the established recovery period associated with the time interval condition, and Q represents the actual operating time in the established recovery period, and further wherein said exceedance elapsed time of said partially modified visual cue is equal to P where X is the predetermined time limit of the time critical exceedance condition.

12. The integrated time/limit exceedance cue system of claim 1 wherein said graphics generating/processing means is further operative for generating a corrective action visual cue in conjunction with said visual cue to indicate a recovery procedure to restore the specific aircraft subsystem to operation within the established operating range.

13. The integrated time/limit exceedance cue system of claim 12 wherein said graphics generating/processing means is operative to strobe said corrective action visual cue to indicate that operation of the specific aircraft subsystem in the time critical exceedance condition has exceeded a predetermined percentage of the predetermined time limit of the time critical exceedance condition.

14. The integrated time/limit exceedance cue system of claim 1 wherein the specific aircraft subsystem has established therefor first and second time critical exceedance conditions having first and second predetermined time limits, respectively, the first predetermined time limit being greater in time value than the second predetermined time limit;

and wherein

said processing means is operative for comparing said parameter signals against the stored threshold values defining limits for established operating ranges for the aircraft subsystems, for generating said activation signal indicative of operation of the specific aircraft subsystem in the first time critical exceedance condition, and for generating a priority signal indicative of transition of operation of the specific aircraft subsystem from the first time critical exceedance condition to the second time critical exceedance condition; and

wherein

said graphics processing means is operative in response to said activation signal for generating said visual cue to alert the pilot that the specific aircraft subsystem has exceeded the established operating limit and is operating in the first time critical exceedance condition and for continually modifying said visual cue to provide a first time varying visual cue indicative of time of operation of the specific aircraft subsystem within the first time critical exceedance condition in relative proportion to the first predetermined time limit; and

wherein

said graphics generating/processing means is operative in response to said priority signal to reinitialize said visual cue to indicate operation of the specific aircraft subsystem in the second time exceedance condition and for continually modifying said visual cue to provide a second time varying visual cue indicative of time of operation of the specific aircraft subsystem within the second time critical exceedance condition in relative proportion to the second predetermined time limit.

15. The integrated time/limit exceedance cue system of claim 1 wherein said graphics generating/processing means is operative to strobe said time varying visual cue to indicate that operation of the specific aircraft subsystem in the time critical exceedance condition has exceeded a predetermined percentage of the predetermined time limit of the time critical exceedance condition.