Abstract: Barrel casing attached to the housing of a hand-held drill. A retractable guide arm is cantilevered from one end of the barrel casing. The cantilevered end of the guide arm has a passageway for the drill bit, and thereby guides it. A rate limiter is attached to the other end of the barrel casing and in axial alignment with it. On the inside of the barrel casing, the rate limiter is connected to the guide arm by abutment.

Abstract: A crushable, composite, columnar, self-stabilized structure for absorbing energy by progressively reacting compression forces along the axis of the structure. The compression failure initiates at one end and progresses to the second end of the stiffener in a controlled fashion in that at any cross section, the local compression strength at that point is less than the general stability strength of the remaining structure.

Abstract: Ejection seat rails that guide an ejection seat out of a vehicle, wherein the seat has rollers that travel along the rails. The rails are constructed such that the rollers simultaneously disengage from the rails, reducing the amount of tip-off that would occur if the rollers were to sequentially disengage.

Abstract: A duct for aircraft use which has ease of use and will resist degradation over time. Silicone impregnated cloth is supported by a nylon helix and covered with a protective braiding of KEVLAR.RTM., a commonly used polyamide fiber. The resulting tube can be strung through tight openings. The duct is equipped with a flexible flange for secure engagement. The flexible flange can be collapsed to reduce the cross sectional area for fitting through narrow openings.

Abstract: Disclosed is an advantageous system for heat rejection especially useful in the space environment.

Abstract: An integrated circuit chip interconnect combining tape automated bonding techniques and conventional wire bonding and adapted to communicate by wire bonding leads to the maximum number of terminal leads for a given chip size, and to accommodate a variety of different chips by the same configuration, the interconnect allowing individual testing of each chip prior to the interconnect's mounting in a multichip module.

Abstract: A method and the resulting structure for attaching a doubler to the skin of an airplane, using the original fastener holes, where the fastener countersinks are filled with interference fitted washers and the new fasteners have an interference fit with the airplane skin, doubler and washers.

Abstract: A vertically mounted deflector attached to a landing gear, that prevents debris from being thrown by the tires into the engine of an aircraft. The deflector has two vertically mounted plates that have oblique stepped surfaces facing the tires.

Abstract: A superplastically formed and diffusion bonded structure formed with two or more sheets and upset forging the material at the perimeter to provide the expulsive material between the inner most sheets so as to close the entrance angle formed between the expanded sheets at the line where the surfaces of the split forming fixture engage and the method of producing this structure. The upset forged material insures the structural integrity of the outside perimeter structure after removal of the flange which is normally present as a result of the holding fixture.

Abstract: An advantageous device and method enables a photomultiplier to be gated on and off at electronic rates. A single multi-winding pulse transformer is employed to enable the triggering of the photomultiplier tube.

Abstract: Velocity vector components of a relativistic high energy beam of atomic particles are measured by examination of the Doppler shifts of spontaneous photo emissions from the beam. Beam direction can be calculated directly from measurements made at the Doppler-free angle if beam velocity is known. Beam velocity can be calculated from measurements made at the Doppler free angle or at other convenient angles. A beam steering technique by nulling outputs from diametrically opposed sensors is also disclosed.

Abstract: The process and apparatus of at least two sensor configurations enable both the location and severity of an environmental disturbance on an optic path to be measured.

Abstract: An explosive source for a store ejector system, having a plurality of explosive cartridges that are sequentially detonated to provide a relatively constant force on the store, when the store is ejected. Operatively connected to each explosive cartridge, is a check valve that prevents a detonated cartridge from simultaneously self-detonating the other cartridges that have not been detonated.

Abstract: In this fastening system two or more layers of material are fastened together by inserting a hollow sleeved fastener such as a rivet or a bolt into the hole in a high interference fit to expand the hole radially. The sleeve is configured either as a collar and a straight shank or as an angled upper portion combined with a shank for counterbored applications. The intersections between either the collar and the shank or the angle portion and the staight shank are designed with an enlarged radius such that when the sleeve is expanded after the insertion of the fastener inside of it, this radius is expanded, which in turn stress coins the adjacent edge of the hole in the layers. This localized stress coining as well as the hoop stress in the hole surrounding the hole dramatically increases the fatigue strength of the fastened layers in a structure assembly.

Abstract: A device and method of back-up fly by wire control, especially useful in fly by wire systems when a failure mode is encountered. The problem of back-up system controllability with the type of compliant sidestick which has minimal displacement and returns to zero upon release of the control force is solved by reducing the authority of the sidestick to a fraction of full authority actuator position capability, to provide good control sensitivity. Full authority actuator position control is provided by automatically activating a trim integrator when the sidestick reaches its displacement stops.

Abstract: An apparatus and method for applying sealant to a countersunk fastener hole. The apparatus includes a sleeve, an adapter tube within the sleeve, a nozzle housing attached to the adapter tube, and a tip within the nozzle housing. A guide pin is attached to the adapter tube and follows an oblique slot in the sleeve. To operate, the sealant applicator is inserted into a countersunk fastener hole, engaging the tip with the countersink of the hole. The tip depresses into the nozzle housing, ejecting sealant onto the countersink. The adapter tube is pushed into the sleeve, moving the guide pin along the oblique slot in the sleeve. This guide pin movement rotates the adapter tube, nozzle housing and tip, causing the tip to uniformly spread the sealant around the countersink.

Abstract: A selectable chip carrier is disclosed which is adapted to receive an integrated circuit chip having a plurality of terminals disposed about its periphery and to allow for the connection of selected ones of these terminals to selected voltage potentials, ground, or signal lines using relatively short, non-overlapping leads.

Abstract: A thin multi-passage cooler that produces an isothermal heating surface, high heat transfer coefficients, without producing an excessive pressure drop across the coolant passages. The cooler having a plurality of first passages in fluid communication with a plurality of second passages. A coolant flows through the second passages and then through first passages which are in close proximity to a heating source. The first and second passages are oriented and connected such that the direction of coolant flow in the first passages is opposite to the direction of flow in the second passages. To promote high heat transfer coefficients the passages are constructed to have large length to width ratios and small hydraulic diameters.

Abstract: An apparatus and method for controlling the flight of a helicopter, in which the pilot commands vehicle state changes, embodies several significant advances to the helicopter control art. Among these are control decoupling to reduce undesired helicopter responses in other axes to pilot inputs in one axis, task oriented control modes which are selected automatically, and automatic control of engine torque and rotor speed constraints. Novel task oriented control modes include independent control of heading and ground track at low speed and turn rate and flight path angle control at higher speeds. Control decoupling is achieved through a combination of force/moment decoupling and open loop prediction methods. Vertical control, traditionally accomplished with collective only, is accomplished in this system with a combination of longitudinal cyclic and collective control, increasing vertical response performance and minimizing engine power change demands.