Helicopter power available to hover indicator

Details Helicopter power available to hover indicator Helicopter power available to hover indicator

G - Physics

05

D

354/18

G05D 1/00 (2006.01) B64D 43/00 (2006.01) G01C 23/00 (2006.01)

Patent

CA 1206261

Abstract Helicopter Power Available To Hover Indicator The power required for a helicopter to hover is generated (14, 82) as the ratio of current operating power in forward flight (12, 77) determined (10, 73) from data relating operating power in forward flight to power required for hover for the aircraft. The power required to hover is compared (18, 83) with the maximum power available developed (16, Fig. 2; Fig. 3) by an engine model algorithm utilizing actual engine parameters. The comparison of maximum power to power required for hover is utilized to provide an indication (22) to the pilot. The viability of the indication is indicated by a "ready" indication (26).

427361

Affiliated with

Also associated with

Rating

Helicopter power available to hover indicator does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Helicopter power available to hover indicator, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Helicopter power available to hover indicator will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1281671