Aircraft engine propeller overspeed protection technical field

Fluid reaction surfaces (i.e. – impellers) – With control means responsive to non-cyclic condition... – With electrical means comparing and reducing error related...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416 36, 416 43, 416 44, B64C 1140

Patent

active

050190067

ABSTRACT:
An aircraft engine propeller autofeather system (4) has a feather solenoid (8) which is actuated by either a signal provided by an engine power loss detector (10) or a signal provided by an engine overspeed detector (12). The overspeed detector (12) detects excessive propeller speed by comparing the speed to a first predetermined value (21) or by comparing the speed rate of change to a second predetermined value (23) combined with comparing the speed to a third predetermined value (25).

REFERENCES:
patent: 2322303 (1943-06-01), Martin
patent: 2499376 (1950-03-01), Ferrill, Jr.
patent: 2640550 (1953-06-01), Knapp et al.
patent: 2667228 (1954-01-01), Wood et al.
patent: 3589830 (1971-06-01), Morgren et al.
patent: 4845617 (1989-07-01), Kamenetz et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Aircraft engine propeller overspeed protection technical field does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft engine propeller overspeed protection technical field, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft engine propeller overspeed protection technical field will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-32720

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.