Ami Industries, Inc.

Aircraft Mechanics, Inc.

Othar P Kennedy

Keith Michael Ferguson

Ryan S Porter

Douglas E Hoover

William D Reida

Christopher Isherwood

Don Pinkal

Ryan Stuart Porter

A bi-directional linear clutch lock is provided that may selectively restrain a rack from translating. A bi-directional rotary clutch lock is provided that may selectively restrain a rotary rack from rotating.

Bi-directional clutch lock

A self-stowing jumpseat consists of a seat frame that is deployed by pulling the seat frame out of a pocket formed in the edge of a bulkhead. Once the seat frame has been deployed and locked in position, the seat pan is folded down to enable a user to be seated. The seat pan is spring-loaded to fold up, so that when the user vacates the seat, the seat pan automatically folds up into the closed configuration. As it does so, an interlock lever attached to the seat pan trips the seat frame locks from their locked to their unlocked positions. The seat frame has a retraction mechanism that urges the seat into the pocket. Accordingly, as soon as the seat pan interlock lever releases the seat frame locks, the retraction mechanism causes the folded seat frame to move into the stowed position within the bulkhead.

Self-stowing jumpseat for aircraft

A support for an aircraft seat, table or other piece of equipment has a lower support link that sweeps out a lateral arc. The lower support link cooperates with a conventional linear track to support the piece of equipment. The linear track provides fore/aft movement substantially orthogonal to a line tangent to the center of the lateral arc. A pilot link is operatively attached to the piece of equipment to form a four-bar linkage that maintains the equipment in a predetermined rotational attitude as the lower support link sweeps out its lateral arc.

Aircraft equipment support

A support for aircraft seats and other equipment has a lower support link that sweeps out a lateral arc. The lower support link supports a platform that may have a conventional linear track. The linear track provides fore/aft movement substantially orthogonal to a line tangent to the center of the lateral arc. A pilot link is attached to the platform to form a parallelogram linkage that maintains the equipment platform in a rotationally fixed attitude as the lower support link sweeps out its lateral arc.

An apparatus for adjusting the position of a seat comprises a rack and a clock nut that grips the rack. The rack comprises a threaded rod, while the clock nut comprises a short cylindrical body that is drilled and threaded along its diameter with internal threads corresponding to the thread diameter and pitch of the rack. Circumferential reliefs are then formed in the threaded bore to enable the clock nut to be 'clocked' from a position in which the threads of the clock nut engage the threads of the rack to a second position in which the threads of the clock nut disengage the threads of the rack. A pair of linkages are provided to rotate the clock nut between the engaged and disengaged positions and to transmit loads from the clock nut. Because the clock nut engages multiple teeth of the rack simultaneously, the seat track locking mechanism of the present invention is capable of extremely fine position adjustment without sacrificing ruggedness and because of the design of the linkages, the seat track locking mechanism locks bi-directionally and with little or no backlash.

Seat track locking mechanism

A equipment support for aircraft and the like comprises a base to which a lower link, an intermediate link, and a equipment platform are attached. The lower link rotates horizontally about the base. The intermediate link rotates horizontally about the end of the lower link and the equipment platform rotates horizontally about the end of the intermediate link. This arrangement gives the equipment platform the ability to assume an infinite number of lateral positions and 360 degrees of rotation. The equipment support is locked in position by means of locking pins that engage corresponding metering plates adjacent the support bearings. The locking pins are released by a common linkage that sequentially releases the equipment platform rotation lock then simultaneously releases the rotation locks of the intermediate and lower links.

Aircraft interior equipment support

A floor track fitting for securing seating or other equipment to a section of aircraft floor track consists of a pair of substantially U-shaped cleat members and a captive bolt. The cleat members are inserted back-to-back through the holes in the floor track. Once the cleat members are in place, a cover is placed over the cleat members so that the captive bolt passes through the top of the cover. The inside of the cover has a pair of integral spaces that force the cleat members outward against the sides of the track channel holes so that the undercut portion of the cleat members locks onto the underside of the floor track. As the bolt is tightened it presses down on the cover and simultaneously draws the cleat members upward against the underside of the floor track to clamp the floor track firmly between the cleat members and the cover.

Aircraft seat floor track fitting

A device for rotating a first structure relative to a second structure has a rotatable shaft for attachment to the first structure. A first cylinder is coaxially attached to the rotatable shaft, and has a plurality of bearing constraining apertures for holding a plurality of bearings. A hollow fixed member for attachment to the second structure has a coaxially attached second cylinder outside of the first cylinder. The second cylinder has a plurality of bearing seats on its inside wall for selectively receiving the bearings. The number of bearing constraining apertures is different from the number of bearing seats, so that the bearings are harmonically aligned by the constraining apertures to be movable to within the bearing seats only at selected progressive locations. A handle is coaxially and rotatably mounted to the fixed member, and carries a cam inside the first and second cylinders. The cam has a protruding cam face in one location to sequentially engage the bearings to urge the engaged bearings into bearing seats with which they align. The cam also has a recessed cam face in another location that allows the bearings to move laterally with movement of the first cylinder without engaging the bearing seats in nonaligned locations. Thus, when the handle is rotated with respect to the fixed member, the bearings engaged by the cam are progressively forced sequentially within the bearing constraining apertures into the tapered bearing seats of the second cylinder to move the first and second cylinders relative to each other.

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Colorado Springs, CO, United States of America

Othar P Kennedy