Configuration responsive descent rate warning system for aircraf

Communications: electrical – Aircraft alarm or indicating systems – Flight alarm

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340963, 342 65, 364433, G08B 2300

Patent

active

050381415

ABSTRACT:
Warning systems that monitor the altitude above ground and descent rate of an aircraft and generate a warning if the descent rate of the aircraft is excessive for the altitude in which the aircraft is flying are well suited to aircraft whose flight and operational characteristics are readily predictable but not as suitable for aircraft, such as tactical aircraft whose operating conditions are not so predictable. To overcome this problem, the criteria for providing the warnings are altered (30, 32) as a function of flight configuration (16, 18) to optimize the warnings for different flight conditions.

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patent: 3958219 (1976-05-01), Bateman et al.
patent: 4030065 (1977-06-01), Bateman
patent: 4215334 (1980-07-01), Bateman
patent: 4551723 (1985-11-01), Paterson
patent: 4567483 (1986-01-01), Bateman et al.

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