Helicopter deicer system power transfer assembly

Details Helicopter deicer system power transfer assembly Helicopter deicer system power transfer assembly

1981-07-02

1984-01-10

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft structure

Ice prevention

219202, 219483, 339 5M, 416 95, B64D 1512

Patent

active

044249470

ABSTRACT:
A device (10) for isolating from vibrational and impulse loads a power transfer unit (14) that transfers power from a helicopter electrical system to a plurality of deicing segments on the rotor blades includes a distributor (13) rotating with the rotor blades for distributing power from the power transfer unit (14) to the deicing segments, a housing (11) having an upper cylinder (24) and lower cylinder (23) the latter of which is flexibly secured to the helicopter as by a joint including ball (40), housing 11 substantially isolating the power transfer unit (14) from such loads, and a shaft (12) rotatably engaging the upper cylinder (24) for carrying the distributor (13) in rotation with the rotor blades.

REFERENCES:
patent: 1821132 (1931-09-01), Baker
patent: 3218595 (1965-11-01), Motsinger
patent: 3317878 (1967-05-01), Garls et al.
patent: 3496331 (1970-02-01), Fleury et al.
patent: 3988049 (1976-10-01), Williams et al.
patent: 4083518 (1978-04-01), Garrison et al.

Affiliated with

Also associated with

Rating

Helicopter deicer system power transfer assembly 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 deicer system power transfer assembly, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Helicopter deicer system power transfer assembly will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-450954