Raytheon Company

Douglas M Beard

Frederick B Koehler

Terry M Sanderson

Ward D Lyman

Scott W Sparrold

Gary H Johnson

James P Mills

Anthony O Lee

Daniel C Harrison

Rene D Perez

Dean B McKenney

John A Thomas

Blake G Crowther

Michael J Broyles

Brian D Alfing

A method and system for selectively dissipating thermal energy are provided. The system includes a heat-generating structure, a first heat sink, a second heat sink, and a heat transfer element. The heat-generating structure generates thermal energy. The first heat sink is in thermal communication with the heat-generating structure. The heat transfer element is configured to be selectively positioned between the first heat sink and the second heat sink to establish a path for the transfer of thermal energy between the first heat sink and the second heat sink. Upon positioning the heat transfer element between the first heat sink and the second heat sink, at least a portion of the thermal energy from the heat-generating structure is allowed to travel through the first heat sink and through the heat transfer element to the second heat sink.

System and method for a switchable heat sink

A release mechanism passively releases a mechanical coupling as a result of a temperature rise. The release mechanism includes a breakable element, such as a shape memory alloy (SMA) element, that is configured to break when the element is heated to a predetermined temperature. The breakage of the breakable element releases a mechanical coupling, such as a coupling holding a lid onto a container. The release mechanism may be part of a handle or other device to close the container. The release mechanism may have a mechanical load on it prior to release, a load that in part passes through the breakable element. Most of the load may pass through one or more other members of the release mechanism, providing the force for separation after the release mechanism is triggered. The release mechanism may be used to provide a passive way of releasing a mechanical coupling in response to heating.

Heat-actuated release mechanism

A container includes a housing and a cover which may be wholly or partially removed to open the container. A foil seal is used to seal the joint between the housing and the cover. The foil seal is internal to the container. The foil seal separates during opening of the cover, respective parts of the foil seal remaining with the housing and the cover. The foil seal may be a metal or metal-containing foil, for example being an aluminum, steel, or titanium foil, or a metalized plastic foil. A cutter, such as a serrated edge, may be positioned to facilitate cutting of the foil seal during cover opening. The container may be part of a seeker assembly with the housing being a seeker housing, and the cover being a removable or hinged cover that protects an optical seeker during some portions of flight, such as during launch of a spacecraft.

Container with foil seal

An optical element mount is effective in high G environments to protect brittle optical elements in which tensile stresses are generated on surface Swithout degrading optical performance. A flexible spacer formed of a relatively low-stiffness material supports an optical element having a tapered outer periphery in an optical seat having a complementary tapered surface. When the optical assembly is exposed to the high G environment, the inertial loading drives the optical element in the aft direction into the flexible spacer and seat. This puts the optical element into a plate bending condition thereby inducing tensile stress on Swhich is at least partially offset by a compressive stress caused by the reaction force normal to the tapered interface. The stresses, both compressive and tensile, placed on the optical element in the high G environment can be very large. In the absence of the tapered mount and flexible spacer, the tensile stress placed on Swould likely fracture or shatter the brittle optical element. When the inertial loading is removed, the optical element returns to its initial unstressed position.

Optical element mount and method thereof for a gun-launched projectile

A programmable optical system that dynamically corrects or induces aberrations into the optical path of a missile seeker. The system is dynamic in that the amount and type of aberration may be changed while the missile is in flight. The dynamic correction is accomplished by means of deformations applied to a low-mass mirror or mirrors in the optical path of the missile seeker. The missile includes an aspheric dome, and the optical system is dynamically compensated for aberrations introduced by the dome as the seeker system is moved through the field of regard.

Sensor system with dynamic optical corrector

Growing community of inventors

Tucson, AZ, United States of America

Douglas M Beard