Abstract: Utilization of a standard, portable oxygen tank and regulator in an emergency respiratory system including an endotracheal adaptor in fluid communication with the regulator and having a first, flexible tube insertable in the windpipe of a patient undergoing emergency treatment, and a second flexible, manually-operable tube attached to the adaptor in opposed relation to the first tube and compressible to direct the oxygen flowing between the regulator and adaptor into the patient's lungs by way of the first tube.

Abstract: A two-stage ramjet engine including an aft end, ejectable, boost stage-combustor/nozzle assembly for initially accelerating from low-to-mid-supersonic launching speeds to high supersonic speeds, and mounted in a tandem arrangement immediately aft of a separate, forward end-cruise stage-combustor/nozzle assembly positioned directly behind an inlet-diffuser section for subsequently further accelerating from high supersonic to hypersonic speeds after ejecting the entire boost stage.

Abstract: A process for forming a removable dental cast embedded with a plastic, threaded, cast ejector button, and apparatus for fabricating a plurality of cast ejector buttons comprised of a mold device including an upper plate containing a plurality of mold cavities, and a base plate incorporating coil spring means for resiliently maintaining the upper plate in a predetermined spaced-apart and open relation thereto and a plurality of rigid support elements attached, at their bottom ends, in vertically-upright relation on the base plate and slidably engaged, at their upper ends, in a bottom opening in each upper plate-mold cavity and extending in overlapping relation into the respective cavity. The upper ends of each rigid support element are threaded so that, when the mold cavities are poured with and filled by a suitable material, in the plastic flow form that is allowed to set for a specified period, a separate and internally threaded plastic cast ejector button is formed in each cavity.

Abstract: A helicopter rescue hoist-traction sheave assembly including a hoist cable engaging sheave and first housing, a drive motor having a drive shaft mounting the sheave and a second housing mounting the motor and positioned in adjustable relation to the sheave housing, a rocker arm fixed to the motor-mounted housing, an alarm switch located near the rocker arm, and a torque compensating spring attached to, and normally retaining the rocker arm in a neutral position out of engagement with the switch when the drive motor is applying a normal amount of traction to the cable through the sheave and automatically moving the rocker arm to an engaged position with, and closing the switch in the event of a malfunction resulting in a substantial reduction in the motor-applied traction.

Abstract: A visor-like, protective hood assembly consisting of a segmented shutter for covering an optical window and including three hemispherical shutter segments of increasing radii and pivoted about a common pivot for relocation between a retracted, open and nested relation and an extended, closed position. A drive motor, coupled with a Geneva mechanism, directly and intermittently drives the outermost shutter segment, and trailing edge lips on each segment engage with and respectively drive the intermediate and inner segments to their fully extended, closed positions in a protective relation over the window.

Abstract: A combined rocket/ramjet for propelling a missile including a missile payload module and an integral rocket/ramjet engine system strapped on the missile payload module, and incorporating a liquid fuel rocket engine and a ramjet engine having a combustion chamber common with the rocket engine, an exhaust nozzle, and multiple aft-mounted air inlets movable between a retracted position during rocket boost flight and an extended, pop-out position to receive and direct ram air in a reverse flow direction into the combustion chamber during ramjet flight.

Abstract: A wedge-shaped, high speed airfoil having a variable geometry configuration consisting of separate, upper and lower airfoil surfaces individually and/or collectively adjustable between inner, retracted and outer, extended positions to vary the amount of airfoil surface area exposed to the free stream flow to that required for effective aircraft stabilization and/or control at selected Mach numbers while minimizing the drag and aerodynamic heating normally resulting therefrom.

Abstract: A translating flap convergent/divergent-aircraft engine thrust nozzle and integrated thrust reverser including a cascade for reversing the flow of engine exhaust, an inner exhaust duct-translating segment and an outer cowl normally enclosing the cascade therebetween; a series of blocker doors positioned in a normal stowed, inactive relation in the aft end portion of the thrust nozzle; main, hydraulic actuators are interconnected with and operable to simultaneously translate the translating segment and cowl to open a reverse-exhaust flow path through the cascade; and a cam-operated device interconnected between the translating segment and the blocker doors to automatically reposition the blocker doors to an active position blocking the engine exhaust path through the thrust nozzle in concert with the translation of the translating segment and cowl to their reverse flow-producing positions.

Abstract: A process for forming a removable dental cast embedded with a plastic, threaded, cast ejector button, and apparatus for fabricating a plurality of cast ejector buttons comprised of a mold device including an upper plate containing a plurality of mold cavities, and a base plate incorporating coil spring means for resiliently maintaining the upper plate in a predetermined spaced-apart and open relation thereto and a plurality of rigid support elements attached, at their bottom ends, in vertically-upright relation on the base plate and slidably engaged, at their upper ends, in a bottom opening in each upper plate-mold cavity and extending in overlapping relation into the respective cavity. The upper ends of each rigid support element are threaded so that, when the mold cavities are poured with and filled by a suitable material, in the plastic flow form that is allowed to set for a specified period, a separate and internally threaded plastic cast ejector button is formed in each cavity.

Abstract: A high acceleration cockpit-ejection seat having an air bladder-liner element acting as a cushion/pad and inflatable to effectively provide a significant backward tilt to, and thus greatly increase the pilot's tolerance to the high g-loads associated with fighter aircraft maneuvering at high speeds.

Abstract: A pneumatic carcass tire having a replaceable tread belt modified by being molded with dual tread patterns of different configurations disposed on the outside and inside surfaces thereof to enable the more efficient and compatible use of the tread belt in alternate, reversible manner for different ground surface and prevailing weather conditions.

Abstract: A combined air flow deflector and diffuser assembly including a main flow deflector vane, a deflector base plate mountable adjacent the trailing edge of an open bomb bay or other cavity of a bomber aircraft, aerospace or other vehicle, and a plurality of support pylons interconnected between and supporting the deflector vane in space relation to the base plate immediately behind the bomb bay or other cavity-trailing edge in the path of, and diverting the airstream away from the vehicle body to thereby partially stabilize the turbulent flow at the shield area or airstream flow adjacent the cavity entrance and, simultaneously therewith, induce a substantial decrease of the excessive pressure oscillations that would otherwise occur within the cavity from the air stream flow passing the open cavity.