Abstract: A frangible fastener system configured to secure a second retained member to a first retained member until the frangible fastener system receives a breaking force is described. The frangible fastener system comprises a first fastener and a second fastener. The first fastener comprises a flange configured to cause retention of the first retained member toward a base member. The first fastener is configured to engage the base member and to receive the second fastener along a first axis of the frangible faster system. The second fastener comprises a frangible portion configured to separate responsive to receiving the breaking force, and a head portion connected to the frangible portion. The head portion is configured to cause retention of the second retained member toward the first retained member until the frangible portion separates responsive to receiving the breaking force.

Abstract: This disclosure relates to a frangible fastener configured such that a first end of the fastener separates from a second end of the fastener responsive to a breaking force. The fastener may comprise a head portion, a frangible portion, a tool engagement portion, a threaded portion, and/or other portions. The frangible portion may include a frangible body. The frangible body may form a plurality of through wall cuts. The frangible portion may be configured such that the breaking force is proportional to a quantity of through wall cuts, a cross sectional area of through wall cuts, and/or a shape of through wall cuts. The frangible portion may be configured such that the breaking force is proportional to a wall thickness of the frangible body. The location of the tool engagement portion may minimize and/or eliminate torsional loading of the frangible portion during tightening with a tightening tool.

Abstract: This disclosure relates to a frangible fastener configured such that a first end of the fastener separates from a second end of the fastener responsive to a breaking force. The fastener may comprise a head portion, a frangible portion, a tool engagement portion, a threaded portion, and/or other portions. The frangible portion may include a frangible body. The frangible body may form a plurality of through wall cuts. The frangible portion may be configured such that the breaking force is proportional to a quantity of through wall cuts, a cross sectional area of through wall cuts, and/or a shape of through wall cuts. The frangible portion may be configured such that the breaking force is proportional to a wall thickness of the frangible body. The location of the tool engagement portion may minimize and/or eliminate torsional loading of the frangible portion during tightening with a tightening tool.

Abstract: An emergency floatation system for an aircraft includes an actuator box assembly that activates the floatation system either electrically or manually. The actuator box assembly is separated from a valve assembly of an inflation reservoir and provides an interface between an electromechanical trigger system and a redundant mechanical trigger system. The actuator box includes a pivot member that provides an interface for the redundant trigger systems and an output actuator. For normal operation a button in the cockpit is pressed which sends an electrical signal to an electromechanical actuator in the actuator box assembly. The electromechanical actuator rotates the pivot member, which operates the output actuator and opens the valve assembly. Alternatively, should the electrical system of the aircraft fail, the pilot or other occupant may activate the mechanical trigger system, thereby rotating the pivot member and activating the output actuator to open the valve assembly.

Abstract: An emergency floatation system for attachment to a helicopter that includes a support frame, a float pack assembly and an inflation system. The float pack assembly includes a float in a packed configuration, a sleeve integrated into the float and a rigid support that at least partially extends through the sleeve. The float pack assembly is configured so that it may be installed and/or removed from the support frame separate from the inflation system.

Abstract: A door pod assembly includes a housing that defines a cavity for emergency equipment, a pod door, and a latch retaining the pod door in a closed position relative to the housing. The assembly is configured such that the latches, upon activation free the release door thereby exposing the emergency equipment and allowing it to be deployed. The door pod assembly maybe coupled to an interior surface of a baggage compartment door and is configured so that the baggage compartment may continue to be used for its originally intended purpose.

Abstract: An inspection device for visually inspecting an image sensor of a digital recording device, such as a digital camera. The inspection device includes a tubular housing and a lens mounted therein. The housing is configured to engage a lens interface of a camera body. A lighting assembly is provided that is configured to illuminate the image sensor when the inspection device is coupled to a digital camera body so that the image sensor may be visually inspected for contamination.

Abstract: A high-pressure hose hinge assembly provides a continuous fluid path between first and second components that move relative to each other. The hose hinge assembly includes a plurality of rotatable swivel fittings that couple a plurality rigid pipe sections. A first swivel fitting is fixedly coupled to the first component and another swivel fitting is coupled to the second component. At least one swivel fitting and two rigid pipe sections extend between the swivel fittings coupled to the first and second components to provide a continuous fluid path.

Abstract: An emergency power supply for an electrical device that provides power sufficient to operate the emergency flotation system for a predetermined period of time after a malfunction of a primary power source. The emergency power supply includes at least one capacitor and a control circuit that are disposed in a housing that is sealed to prevent ingress of liquids. The emergency power supply remains functional even when it is partially submerged.

Abstract: A pressure activated latch includes a latch housing, a fluid inlet, a fluid outlet, an internal biasing member and a sliding latch pin that is configured to engage a latch tab that is substantially adjacent to the latch housing. The latch pin is slidable between a first position in which the latch pin prevents fluid communication between the fluid inlet and the fluid outlet and engages the latch tab and a second position in which the latch pin is disengaged from the latch tab and fluid communication is permitted between the fluid inlet and the fluid outlet. The internal biasing member is configured to apply a force upon the latch pin to bias it into the first position.

Abstract: A floatation system for attachment to a helicopter landing skid includes a girt dimensioned to be attached to a landing skid and a plurality of floats attached to the elongate girt, wherein the plurality of floats are adapted to be converted from a packed configuration to an deployed configuration, and wherein at least one of the plurality of floats extends beneath the elongate girt when the plurality of floats is in the deployed configuration.

Abstract: A connector for releasably attaching a pair of conduits includes male and female components having proximal and distal ends and a lumen, and a swivel connection releasably connecting the male and female components. The swivel connection permits fluid communication between the male and female components and also permits free rotation between the male and female components.

Abstract: An emergency floatation system for a helicopter includes a safety trigger device for inflating at least one raft during the course of an emergency. The safety trigger device includes a plurality of handles such that pulling any one of the plurality of handles triggers the inflation of the at least one raft.

Abstract: A floatation system for attachment to a helicopter landing skid includes a girt dimensioned to be attached to a landing skid and a plurality of floats attached to the elongate girt, wherein the plurality of floats are adapted to be converted from a packed configuration to an deployed configuration, and wherein at least one of the plurality of floats extends beneath the elongate girt when the plurality of floats is in the deployed configuration.

Abstract: A quick connector including a first connecting member attached to an object, a second connecting member releasably attached to the first connecting member and a release mechanism for detaching the first and second connecting members, wherein the release mechanism automatically disconnects the first connecting member from the second connecting members when the connecting members are pulled away from the object.

Abstract: An emergency floatation system includes at least one inflatable float and an inflatable emergency life raft contained within a single cover, wherein the system is adapted to be converted from a packed configuration to a partially deployed configuration by use of a first actuating member, and wherein the system is adapted to be converted from the partially deployed configuration into a fully deployed configuration by use of a second actuating member.

Abstract: A floatation system for attachment to a helicopter landing skid includes a girt dimensioned to be attached to a landing skid and a plurality of floats attached to the elongate girt, wherein the plurality of floats are adapted to be converted from a packed configuration to an deployed configuration, and wherein at least one of the plurality of floats extends beneath the elongate girt when the plurality of floats is in the deployed configuration.