Blade flap locking for out-of-use helicopters

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Including movement limit stop or damping means

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C416S107000, C416S143000

Reexamination Certificate

active

07744349

ABSTRACT:
In the absence of centrifugal force produced during rotation of helicopter blades, damage may result if a blade is rotated upward by wind or other forces. Lock units removably appended between the rotor assembly and each blade pitch housing attached to a helicopter blade are usable to restrict upward rotation. A base portion of a lock unit may be configured to be held in position by a removable pin device. An extendible device extending from the base portion to a surface of a blade pitch housing can be adjusted to press the base portion back against a surface of the rotor assembly. The lock unit thereby restricts these surfaces of the blade pitch housing and rotor assembly from moving closer to each other and thereby restricts upward rotation of the blade pitch housing and its attached helicopter blade. The lock units are readily removable in preparation for returning a helicopter to active use.

REFERENCES:
patent: 2906348 (1959-09-01), Lovegrove
patent: 4203708 (1980-05-01), Rybicki
patent: 4289448 (1981-09-01), Declerco et al.
patent: 5951252 (1999-09-01), Muylaert
patent: 6309182 (2001-10-01), Muylaert

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

Blade flap locking for out-of-use helicopters does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Blade flap locking for out-of-use helicopters, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Blade flap locking for out-of-use helicopters will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4238982

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