Negative climb after take-off warning system with...

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

G - Physics

01

C

343/15, 343/73

G01C 21/00 (2006.01) G01C 5/00 (2006.01) G01P 3/62 (2006.01) G05D 1/06 (2006.01) G08B 23/00 (2006.01)

Patent

CA 1157132

NEGATIVE CLIMB AFTER TAKE-OFF WARNING SYSTEM WITH CONFIGURATION WARNING MEANS 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.

365920

Affiliated with

Also associated with

Rating

Negative climb after take-off warning system with... 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..., 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... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-396355