The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 07, 2015

Filed:

Aug. 09, 2012
Applicants:

Martin S. Day, Colorado Springs, CO (US);

Chad R. Pacheco, Colorado Springs, CO (US);

Donald R. Pinkal, Colorado Springs, CO (US);

Inventors:

Martin S. Day, Colorado Springs, CO (US);

Chad R. Pacheco, Colorado Springs, CO (US);

Donald R. Pinkal, Colorado Springs, CO (US);

Assignee:

AMI Industries, Inc., Colorado Springs, CO (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60N 2/427 (2006.01);
U.S. Cl.
CPC ...
B60N 2/427 (2013.01); B60N 2/42736 (2013.01);
Abstract

A track-mounted aircraft seat has seat track locking pins that are capable of moving independently to remain engaged with the seat track assembly in a warped-floor condition. The seat track locking pins are actuated by means of a pair of torque tubes that rotate independently about a common pilot shaft. A control link, which is operated by the user, acts on a pair of bell cranks each of which acts on one of the torque tubes. The control link is attached to the bell cranks by means of a spherical joint. Because the torque tubes rotate independently and because the spherical joint allows the bell cranks also to move independently, in the event of a warped-floor condition, rotation of one torque tube caused by the skewed seat track will not cause the other torque tube to release its track locking pin.


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