Negative climb after take-off warning system with configuration

Details Negative climb after take-off warning system with configuration Negative climb after take-off warning system with configuration

1980-01-04

1982-03-09

Groody, James J.

Communications: electrical

Selective

Having indication or alarm

73178T, 244180, G01C 2100, G08B 2300

Patent

active

043192181

ABSTRACT:
During a take-off or missed approach phase of operation the aircraft's maximum barometric altitude is retained in a memory element and compared to the aircraft's current altitude, and if the aircraft's current barometric altitude should be below the maximum altitude by a predetermined amount based on the aircraft's radio altitude, a voice warning is generated indicating that the aircraft is descending. Landing gear and flaps are monitored by the system and if the gear or flaps are down, an additional voice warning is generated indicating that the gear or flaps are down.

REFERENCES:
patent: 3715718 (1973-02-01), Astengo
patent: 3946358 (1976-03-01), Bateman
patent: 3947810 (1976-03-01), Bateman et al.
patent: 4030065 (1977-06-01), Bateman
patent: 4060793 (1977-11-01), Bateman
Sundstrand Data Control, Inc., "Mark II Ground Proximity Warning System", 1976.

Affiliated with

Also associated with

Rating

Negative climb after take-off warning system with configuration does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Negative climb after take-off warning system with configuration , we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Negative climb after take-off warning system with configuration will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1843083