Honeywell International Inc.

Omaha Standard, LLC

Ross F Meyer

Darrell Horner

Govind Yadav

Albert Kang

David P Gentile

Beth Miller

Kevin Prodromides

Karl Schroeder

Roy F Kruegel

James Delaloye

Barry Fuhrmann

Clark D Barrand

Barrett Fuhrmann

David E Boyer

Jungsuk J Ryu

Jeffrey L Tilley

An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.

Lightweight cabin pressure thrust recovery outflow valve

An apparatus is provided for activating switches in a leading edge flap drive actuator. The apparatus comprises a mount plate having at least a first side, a second side, and an outer peripheral surface, an actuator arm rotationally coupled to the mount plate and rotationally moveable between at least an activate position and a deactivate position, and a spring arm coupled to the mount plate and extending away from the mount plate outer perpheral surface, the spring arm configured to supply a force that biases the actuator arm toward the deactivate position at least when the actuator arm is in the activate position.

Swing arm switch actuator assembly

A detachable stabilized intermodal container dumping apparatus for removable mounting on an intermodal container transport vehicle includes a container support frame having forward and rearward ends, a lower frame section and an upper frame section. The upper frame section is constructed of at least two upper section long sill members and at least two upper section crossbeam members mounted on the upper section long sill members. The lower frame section is constructed of at least two lower section long sill members and at least two lower section crossbeam members mounted on the lower section long sill members. The upper frame section is hingedly connected to the lower frame section adjacent the rearward end of the container support frame along a hinge pivot axis extending generally perpendicular to the longitudinal axis of the container support frame such that the upper frame section may pivot relative to the lower frame section, thus permitting dumping of an intermodal container situated thereon. The lower frame section includes at least two lower frame connection devices mounted thereon for removably mounting the container support frame on an intermodal container transport vehicle. The upper frame section includes at least two upper frame connection devices mounted thereon which are designed to accept and secure an intermodal container. Finally, a hoist unit is mounted on the lower frame section forward of the hinge pivot axis, the hoist unit is further connected to the upper frame section forward of the hinge pivot axis such that upon engagement of the lifting device, the upper frame section is pivoted about the hinge pivot axis relative to the lower frame section, thus dumping an intermodal container mounted thereon.

Detachable stabilized intermodal container dumping apparatus

Growing community of inventors

Mesa, AZ, United States of America

Ross F Meyer