Aircraft spoiler blow-down mechanism

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244228, 244 75R, 74 8915, B64C 358, B64C 1350, F16H 2702

Patent

active

059188367

ABSTRACT:
An electrical mechanical blow-down mechanism for use with an aircraft spoiler avoids possible damage due to high inertial loading when a power failure occurs as the spoiler (10) is moving toward or is at an extended position by means of a structure including a ball screw mechanism (18) adapted to be connected to the spoiler (10) and including an input gear (34) adapted for rotation about an axis (36). The mechanism is ultimately driven by an electrical motor (20) having a rotary output (22) with at least one gear (26, 28) interconnecting the input gear (34) and the rotary output (22). A pawl (36) is mounted for movement between positions engaged with and disengaged from the input gear (34) and a spring (78) is utilized to normally bias the pawl (36) toward the engaged position. A solenoid (50) is operable to move the pawl (36) against the spring (78) toward the disengaged position and a motion sensor (90) is associated with the input gear 34 to determine the direction of rotation thereof. A latch (42, 106) is provided for holding the pawl (36) in the disengaged position for one direction of movement of the input gear (34) and releasing the pawl (36) for the other direction of rotation of the input gear (34). Motion sensor (90) controls movement of latch (42, 106) to prevent pawl (36) engagement after a power failure until such engagement will not damage the spoiler actuator.

REFERENCES:
patent: 2653691 (1953-09-01), Weiland
patent: 2747709 (1956-05-01), Bennett
patent: 2873848 (1959-02-01), Steinmetz
patent: 3017963 (1962-01-01), Landschulze
patent: 4410072 (1983-10-01), Dickinson et al.
patent: 4575027 (1986-03-01), Cronin
patent: 4628752 (1986-12-01), Paxton et al.
patent: 4697672 (1987-10-01), Linton
patent: 4705144 (1987-11-01), Yabe et al.
patent: 4745815 (1988-05-01), Klopfenstein
patent: 4762205 (1988-08-01), Ortman
patent: 4834225 (1989-05-01), Klopfenstein et al.
patent: 4858491 (1989-08-01), Shube
patent: 4876906 (1989-10-01), Jones
patent: 4991800 (1991-02-01), Schwarz
patent: 5582390 (1996-12-01), Russ

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 spoiler blow-down mechanism 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 spoiler blow-down mechanism, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft spoiler blow-down mechanism will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-893941

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