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Title: Excessive sink rate warning system for aircraft
Claims: I claim: 1. A warning system for use in aircraft having a source of signals representing the aircraft's barometric rate of descent and a source of signals representing the aircraft's altitude above terrain, comprising: means for comparing the aircraft's barometric rate of descent with the aircraft's altitude above the terrain; a first signal generating means, responsive to said comparing means, for generating a voice sink rate type of warning signal representing a condition wherein the aircraft is exceeding a descent rate according to a first predetermined, essentially linear, relationship between barometric descent rate and aircraft altitude above the terrain, wherein said first predetermined relationship has a slope of approximately 1,000 feet per minute for each 580 feet of altitude; and a second signal generating means, responsive to said comparing means, for generating a voice pull-up type of warning signal representing a condition wherein the aircraft is exceeding a descent rate amounting to a second predetermined relationship between barometric descent rate and aircraft altitude above the terrain wherein said second predetermined relationship requires a lesser descent rate for a given altitude above the terrain than said first predetermined relationship. 2. The warning system of claim 1 wherein said first predetermined relationship between descent rate and altitude will result in said first signal generating means generating said first a warning signal when the descent rate exceeds approximately 1,700 feet per minute for an altitude of 500 feet above the terrain. 3. The warning system of claim 1 wherein said first signal generating means additionally includes means for increasing the repetition rate of said voice sink rate warning a function of increasing descent rate for a given altitude. 4. The warning system of claim 1 additionally including means responsive to the altitude above the terrain signal to inhibit said sink rate warning signal when the aircraft is above a predetermined altitude above the terrain. 5. A warning system for use in aircraft having a barometric altimeter and a radar altimeter comprising: a circuit responsive to the barometric altimeter for generating a barometric altitude rate signal; a first comparator circuit responsive to said radar altimeter and said barometric rate signal effective to generating a first logic signal responsive to a first predetermined relationship between said barometric rate signal and altitude above ground; a circuit for generating a voice sink rate warning in response to said first logic signal; a second comparator circuit responsive to said radar altimeter and said second barometric rate signal effective to generate a second logic signal responsive to a second predetermined relationship between altitude and barometric descent rate; a circuit responsive to said logic signal for inhibiting said voice sink rate warning; and a circuit for generating a voice pull-up warning in response to said second logic signal. 6. The system of claim 5 additionally including a variable repetition rate circuit responsive to said barometric rate signal and operatively connected to said voice sink rate warning circuit for increasing the repetition rate of said sink rate signal as a function of increasing barometric descent rate. 7. The system of claim 6 additionally including a circuit operatively connected to said variable repetition rate circuit and said voice sink rate warning circuit for increasing the amplitude of said sink rate circuit as a function of said repetition rate. 8. An excessive descent rate warning system for use in aircraft having a source of signals representing the aircrafts barometric descent rate and a radio altimeter, comprising: means, responsive to the descent rate signal and the radio altimeter, for generating a voice sink rate advisory warning according to a first predetermined relationship between descent rate and radio altitude; means, responsive to the descent rate signal and the radio altimeter, for generating a voice pull-up type warning signal according to a second predetermined relationship between descent rate and radio altitude wherein said second predetermined relationship requires a greater descent rate for each altitude to generate said pull-up type warning than does said first predetermined relationship; and means for inhibiting said sink rate warning when said pull-up warning is generated. 9. The system of claim 8 wherein said sink rate warning means will generate said sink rate warnings for descent rates of 1,200 feet per minute at an altitude of 100 feet. 10. The system of claim 9 additionally including means responsive to the descent rate for varying the repetition rate of said voice sink rate warning as a function of the amount that the aircraft exceeds said first predetermined relationship. 11. The system of claim 10 additionally including means to increase the amplitude of said sink rate voice warning as a function of said repetition rate. 12. The system of claim 8 wherein said first predetermined relationship between descent rate and radio altitude is essentially linear. 13. The system of claim 12 wherein said first predetermined relationship has a slope of approximately 0.6 feet of altitude for each foot per minute of altitude descent rate. 14. The system of claim 8 wherein said voice warning generating means includes means to change said second predetermined relationship to a third predetermined relationship for descent rates above a predetermined value. 15. The system of claim 14 wherein said third predetermined relationship is essentially linear and has a slope of approximately 0.40 feet for each foot per minute of descent rate. 16. The system of claim 14 wherein said second predetermined relationship is essentially linear and has a slope of approximately 1.5 feet for each foot per minute of descent rate. 17. The system of claim 14 wherein said predetermined descent rate is approximately 1,500 feet per minute. 18. A warning system for use in aircraft having a source of signals representing the aircraft's barometric rate of descent and a source of signals representing the aircraft's altitude above terrain, comprising: means for comparing the aircraft's barometric rate of descent with the aircraft's altitude above the ground; a first signal generating means, responsive to said comparing means, for generating a voice sink rate type of warning signal representing a condition wherein the altitude aircraft is exceeding a descent rate according to a first predetermined relationship between barometric descent rate and aircraft altitude above the terrain; a second signal generating means, responsive to said comparing means, for generating a second type of warning signal representing a condition wherein the aircraft is exceeding a descent rate amounting to a second predetermined relationship between barometric descent rate and aircraft altitude above the terrain; and means for increasing the amplitude of said voice sink rate warning as a function of increasing descent rate for a given altitude. 19. The warning system of claim 18 wherein said first signal generating means additionally includes means for increasing the repetition rate of said voice sink rate warning as a function of increasing descent rate for a given altitude. 20. A warning system for use in aircraft having a source of signals representing the aircraft's altitude above terrain, comprising: means for comparing the aircraft's barometric rate of descent with the aircraft's altitude above the terrain; a first signal generating means, responsive to said comparing means, for generating a voice sink rate type of warning signal representing a condition wherein the aircraft is exceeding a descent rate according to a first predetermined relationship between barometric descent rate and aircraft altitude above the terrain, wherein said first predetermined relationship will cause said first signal generating means to generate said voice sink rate warning at a descent rate of 1,200 feet per minute for an altitude of 100 feet above the terrain; and a second signal generating means, responsive to said comparing means, for generating a voice pull-up type warning signal representing a condition wherein the aircraft is exceeding a descent rate amounting to a second predetermined relationship between barometric descent rate and aircraft altitude above terrain. Other info: Inventors: Bateman, Charles Donald (Bellevue, WA, US) Application Number: 706518 Filing Date: 1976-07-19 Publication_date: 1977-11-29 Assignee: Sundstrand Data Control, Inc. (Redmond, WA) Primary Class(es): 340/970 244/180, 340/945, 340/964, 342/65, 342/455 Other Classes: US Patent Ref:
Other Refs: Other References: The Sundstrand Ground Proximity Warning System, Advertising Circular, Sundstrand Data Control, Inc., 13-475. | |