| Conax Florida Corporation Patent applications |
| Patent application number | Title | Published |
|---|
| 20120119033 | Retaining Mechanism for Buckle and Buckle Release System - Disclosed is a retaining mechanism for a buckle and buckle release system. The buckle release system is locked or unlocked via a manual release lever. A locking lever overlies the manual release lever and protects against the unintended release of the buckle. The retaining mechanism provides a further degree of protection. It includes a retaining bar that is pivotally interconnected to the locking lever. The retaining mechanism has a closed orientation wherein the locking lever cannot be actuated. The retaining mechanism can only be opened via a two part motion. First, the retaining bar is pivoted with respect to the locking lever. Second, the retaining bar and the locking lever are rotated together to permit access to the underlying manual release lever. | 05-17-2012 |
| 20120073677 | Water Actuated Pressurized Gas Release Device - Disclosed is a gas release device that is adapted to be secured to an inflatable article. The device includes an container, which can be a commercially available gas bottle, a salinity sensor, and an end cap. The salinity sensor operates an electrically fireable primer that serves to release an inflation gas from the container and inflate the article. The end cap includes a cylindrical through hole that accepts a rotatable D-ring. The D-ring is dimensioned to fit over the valve of the inflatable article. The D-ring includes a series of peripheral apertures that can be selectively aligned with a slot to create a fluid passage between the container and valve. The D-ring allows the device to be rotated between different angular positions while maintaining a pneumatic coupling between to the inflatable article and the container. | 03-29-2012 |
| 20120025027 | System for Air Borne Deployment of Palletized Cargo - Disclosed is a system for the airborne deployment and delivery of palletized cargo. The system includes a cargo pallet, one or more risers connected to the pallet, and an associated rigging. The risers are used in both stabilizing the cargo and in cushioning the impacts associated with transport and landing. The rigging is used to secure the pallet to one or more parachutes that are deployed as the pallet leaves the aircraft. | 02-02-2012 |
| 20120024627 | Restraint and Extraction Harness With Associated Release Mechanism - Disclosed is a harness system that can be used in both restraining and extracting a wearer. The harness takes the form of webbing that may be integrated into a crewmember worn vest. The webbing includes extraction loops for use in hoisting the crewmember and a release mechanism for releasably coupling the harness to an external restraint, such as an overhead reel. The system can be used within a vehicle, such as a land based vehicle, a water going vessel, or an aircraft. | 02-02-2012 |
| 20120000575 | Interface Assembly for Space Vehicles - Disclosed is a multipart valve assembly. The assembly can be used in selectively coupling two vehicles. The assembly includes inter-fitting male and female components and associated control valves. Coupling the male and female components establishes media (fluid or gas), communications, and electrical paths between space vehicles. This permits the passage of media from one vehicle to the other and likewise enables one vehicle to operate the control valve of the other vehicle. | 01-05-2012 |
| 20110180165 | Non-Magnetic Latching Servo Actuated Valve - A non-magnetic latching servo actuated valve under the control of a controller comprising a motor in rotational communication with a lead screw. The lead screw advances or retracts a valve stem connected to a valve stem cap. The valve stem cap has a valve stem cap passage. A valve end cap having a valve seat is provided and receives the valve stem cap such that the valve stem cap can contact the valve seat. A pressure relief device or shuttle assembly is positioned internal to the valve stem cap. The shuttle assembly is used for venting build-up downstream pressure through the non-magnetic latching servo actuated valve outlet, through the valve stem cap passage, around the shuttle assembly, through passages, into a pressure chamber, and to the nonmagnetic latching servo actuated valve exit where the fluid vents until the system is in balance. | 07-28-2011 |
| 20110148394 | Fluid Conductivity Sensor for Actuating and Testing an Electroexploding Device - Disclosed is an apparatus for sensing the electrical conductivity of fluid wherein when electrodes of the apparatus are exposed to fluid. When the electrodes are exposed to a fluid with a predetermined salinity, a voltage is developed on a capacitor which in turn fires a load, such as a resistive bridge wire. Also disclosed is a testing circuit, whereby the integrity of the circuit can be ascertained without the necessity of actually firing the circuit. | 06-23-2011 |
| 20110043016 | Adjustable Articulating Crew Seat - A vehicle occupant restraint system includes a seat base pivotally connected to a seat mounting point and seat back pivotally connecting to the seat base. The seat base pivot reside proximal to a forward edge of the seat base and the seat back pivot resides proximal to a rearward edge of the seat base. Each pivot includes a toothed rack, and an engaging member for locking the pivot. The teeth define a radius about the pivots. The engaging members are attached to the seat base and are actuated by levers attached to the seat base. A harness is attached to the seat to prevent injury of an occupant in the event of a unanticipated maneuver, crash, rough terrain, or turbulence. The restraint system comprises a robust mechanism to withstand crash loads and offer sufficient adjustment between sitting and standing positions to accommodate an occupant's duties. | 02-24-2011 |
| 20110024569 | ATTENUATED LANDING SYSTEM - Disclosed is an attenuated landing system. The landing system includes one or more inflatable structures that are mounted to the underside of a cargo platform. A terrain sensor is likewise mounted to the underside of the cargo platform and is activated upon being air-dropped. Once terrain is detected, pressurized gas vessels are pyrotechnically activated to inflate the structures. Once fully inflated, the structures effectively cushion the landing of the cargo platform and, thereby, protect sensitive on-board equipment. | 02-03-2011 |
| 20110010901 | Ejector Mechanism for Rotary Buckle Assembly - Disclosed is a rotary buckle assembly for harness. The assembly is adapted to selectively secure or eject the tongue plates for the straps of the harness. Although the invention finds particular application for use with a five point harness, it can be adapted for use with other harness arrangements. | 01-20-2011 |
| 20100320740 | Combat Vehicle Restraint System - A combat vehicle restraint system accommodates a wide range of soldiers, both with and without battle, arctic, or chemical gear. The restraint system includes lengthened belts and an adjustable buckle position. The belts include loops for locating and grasping the belts, and separate lap and shoulder belts with small narrowing ends to prevent catching on gear. The belts are extendable from Inertial reels which are calibrated for off-road operation. The buckle engages each belt separately and includes a single action release. The buckle position is easily adjusted using an oversized knob so that a soldier may easily find and adjust buckle length in the dark, wearing heavy gloves, or with muddy slippery fingers. The latch/unlatch mechanism and associated hardware is an open frame type to reduce or eliminate affects of mud, dust, water or other contaminants on operation. | 12-23-2010 |
| 20100299837 | VACUUM PACKED INFLATABLE STRETCHER WITH FRANGIBLE OVERWRAP AND METHOD OF DEPLOYING SAME - Disclosed is an inflatable stretcher. The stretcher is stored in a deflated state within a frangible outer covering. A lanyard is connected to the internal gas vessel via an “external to internal” mechanical link which does not violate the vacuum seal of the stretcher's outer covering. Pulling the lanyard activates the vessel to rapidly inflate the stretcher. This inflation causes an overpressure condition within the covering that results in a progressive tear and the eventual separation of the outer covering. The stretcher can thereafter be used to transport a patient. | 12-02-2010 |
| 20100186204 | Twin Buckle Assembly with Dual Release Positions - Disclosed is a twin buckle assembly with dual release positions. More particularly, the invention relates to a buckle assembly that can lockingly secure two buckle tongues. The buckle assembly includes a single, pivotal latch mechanism that can separately secure one or both of the buckle tongues. Pivotal movement of the latch occurs upon rotation of the buckle cover. Thus, one tongue is released at a first rotational position of the cover and both tongues are released at a second rotational position of the cover. The buckle assembly, thereby, allows the independent removal of lap and shoulder belts. | 07-29-2010 |
| 20100146749 | Housing for a Dual Release Twin Buckle Assembly - Disclosed is a housing assembly for twin latching mechanisms. The housing assembly includes two handles that can be pivoted to separately unlatch two belt connectors. The latching mechanisms are positioned within the housing such that when the handles are pivoted upwardly, their leading edges engage plunger mechanisms associated with the latching mechanisms. By engaging the plunger mechanisms, individual latches are disengaged and the associated belt connectors are ejected. A flange interconnects the two handles such that one or both handles are pivoted depending upon which handle is lifted by the operator. The housing provides a secure enclosure for the latch mechanisms and also shields the working components from the environment. | 06-17-2010 |
| 20090314978 | Self Sealing Disconnect Valve - Disclosed is a self sealing disconnect for use in connection with an environmental control system. The disconnect includes two mating halves each of which houses an internal butterfly valve. When the halves are engaged, the butterfly valves are opened to complete a fluid circuit. Conversely, when the halves are disengaged, the butterfly valves are close so as to prevent the flow of fluids. | 12-24-2009 |
