Abstract: A table deployment mechanism is disclosed. In various embodiments, the table deployment mechanism utilizes vertical slides in conjunction with scissor members and a gas spring coupled to the scissor members in order to facilitate movement of the deployment mechanism between a retracted position and a deployed position despite any stresses which may be imparted to the deployment mechanism.
Abstract: A braking mechanism to control rotational movement of a seat is disclosed. The braking mechanism may comprise a circular member (e.g., a disc or ring) that is coupled to a base assembly and a caliper, coupled to a seat assembly, to engage the circular member. In a biased position, a braking element of the caliper applies a braking force to the circular member. A user can reduce the braking force by increasing the tension on a cable coupled to the caliper. Once the braking force is sufficiently reduced, the user may rotate the seat until the desired rotational orientation is attained. Upon release of the cable, the braking mechanism re-engages to prevent further rotational movement.
Type:
Grant
Filed:
April 7, 2003
Date of Patent:
September 6, 2005
Assignee:
DeCrane Aircraft Seating Company, Inc.
Inventors:
George T. Beatty, Nathan A. Hemmer, John H. Traube, Carl R. Hutchison
Abstract: A table deployment mechanism is disclosed. In various embodiments, the table deployment mechanism utilizes vertical slides in conjunction with scissor members and a gas spring coupled to the scissor members in order to facilitate movement of the deployment mechanism between a retracted position and a deployed position despite any stresses which may be imparted to the deployment mechanism.