Abstract: Disclosed is a method of and system for gathering off-body pressure signature data from a scaled model in a wind tunnel. The data is gathered using a probe having multiple longitudinally disposed static pressure ports. Because of the number of ports and their spacing, the probe is able to remain stationary in the tunnel for the entire range of Mach numbers and model positions to be tested. Thus, tunnel flow characteristics can be easily and effectively removed. The system also has an automated model positioning system which enables settings at different pitch, yaw, and roll angles. This enables the user to locate the model so that it can be traversed at a fixed distance above the probe while maintaining the desired angular orientation of the model. By repeatedly traversing the model at different angular orientations, a detailed and accurate off-body pressure distribution can be obtained. The wind tunnel test technique captures full off-body pressure signatures in a complete 360 degree azimuthal range.

Abstract: A system and method for a controlling an aircraft with flight control surfaces that are controlled both manually and by a computing device is disclosed. The present invention improves overall flight control operation by reducing the mechanical flight control surface components while providing sufficient back-up control capability in the event of either a mechanical or power-related failure. Through the present invention, natural feedback is provided to the operator from the mechanical flight control surface which operates independent of computer-aided flight control surfaces.

Abstract: An aircraft flight control disconnect mechanism between the pilot and co-pilot controls, including a pair of concentrically positioned opposed circular jaws, each jaw having either mating tapered teeth or mating tapered openings, which when the jaws are axially separated, disconnects one pilot control from the other and a rotating control sleeve concentrically aligned with and rotatably attached to one of said jaws, the sleeve including a helical cam slot surrounding a fixed roller whereby rotation of the control sleeve moves the said connected jaw toward or away from the adjacent jaw so that the two jaws are free to rotate independent of each other.

Abstract: An anti-corrosive sol-gel composition and process for coating an aerospace alloy substrate with the composition.

Abstract: A method of determining springback in metal forming with a fluid cell press through establishing a computational formulation to determine bend angle and compensated die radius based on factors of geometry of the part being formed, material properties of the sheet material and the forming process, and computing additional iterations of springback until a specific tolerance between the formed part angle and the desired part angle are reached.

Abstract: A method and an apparatus for inspecting parts for surface contamination including the steps of covering the part with a film of water, and then scanning the wetted part with a infrared camera to preserve the reflected image of the reflected infrared light thereby defining a water break area of contamination.

Abstract: A stowable chair armrest for a seat assembly which includes a armrest portion connected to the seat assembly through a restricted movement rotating joint which has limited rotation about a horizontal X and Y axes, the Y-axis being parallel to the length of the armrest portion and positioned above the plane of the seat cushion whereby the armrest portion is rotatable about the Y-axis approximately 180° from an elevated position of the armrest to a retracted position. When the armrest is in its use position, it cannot rotate downward about its Y-axis. However, the arm rest can be lifted upward 10° about its X-axis, wherein a flat blade connecting the armrest to a spherical pivot becomes aligned in a longitudinal chamber having a circular cross-section thus permitting the armrest portion to rotate 180° about its Y-axis to its stowed position.

Abstract: Method and apparatus of back riveting construction for sections of aircraft structure utilizing the flush riveting wherein the back bar tooling for all the rivets in the entire section is a single piece of stationary tooling which conforms to the exterior shape of the aircraft section. The rivet gun is a single impact pneumatic gun with a rivet driving hammer which is offset from the axis of the gun's piston and impact pin to upset rivet under C-channel flanges.

Abstract: Method and apparatus of back riveting construction for sections of aircraft structure utilizing the flush riveting wherein the back bar tooling for all the rivets in the entire section is a single piece of stationary tooling which conforms to the exterior shape of the aircraft section. The rivet gun is a single impact pneumatic gun with a rivet driving hammer which is offset from the axis of the gun's piston and impact pin to upset rivet under C-channel flanges.

Abstract: Method and apparatus of back riveting construction for sections of aircraft structure utilizing the flush riveting wherein the back bar tooling for all the rivets in the entire section is a single piece of stationary tooling which conforms to the exterior shape of the aircraft section. The rivet gun is a single impact pneumatic gun with a rivet driving hammer which is offset from the axis of the gun's piston and impact pin to upset rivet under C-channel flanges.

Abstract: A lightweight plastic bolt-like fastener which is used in pairs having a dual ratcheting function. The fastener includes a bolt having a stem which is semi-cylindrical in cross-section, with a head connected to one end of the stem and a semi-circular aperture in the head positioned coaxially aligned with the stem for receipt of a stem from a second bolt directed in opposite orientation. Positioned longitudinally along the flat side of the stem is a rack of serrated teeth which when the stem is inserted within the semi-circular aperture, a deflectable locking tab attached to the head end of the stem engages the rack of serrated teeth as a ratchet, and since the two fasteners each have stems sliding within the semi-circular aperture of the opposing stem, there is a double ratcheting action between both fasteners.

Abstract: Method and apparatus of back riveting construction for sections of aircraft structure utilizing the flush riveting wherein the back bar tooling for all the rivets in the entire section is a single piece of stationary tooling which conforms to the exterior shape of the aircraft section. The rivet gun is a single impact pneumatic gun with a rivet driving hammer which is offset from the axis of the gun's piston and impact pin to upset rivet under C-channel flanges.

Abstract: A tail support stand for aircraft which sounds an alarm when the tail lowers relative to the stand including a stationary vertical stand which rests on the ground having a passage therethrough, a slidable sleeve positioned in said passage with an aircraft engaging surface on the upper end thereof, the sleeve having a series of longitudinally spaced holes and a removable pin to insert in said holes. A stationary plate attached to the top of the stationary stand with an opening surrounding the sleeve, a movable plate with an opening concentrically positioned over the stationary plate with biasing means positioned between the plates resisting movement of the movable plate and audible aerosol actuated horn positioned between the movable and stationary plates which is activated when the said pin engages and moves the movable plate toward the stationary plate.

Abstract: A modular camera support and extension structure which removably mounts on the seat tracks of a conventional aircraft and extends through a cargo pod door during usage, including a box structure containing a plurality of vertical rails which support a tracking plate positioned inside the box structure with linear bearings around its periphery, slidably mounted on said rails for vertical movement from a retracted position to an extended position; a camera rotatably mounted on the bottom of said tracking plate about a vertical axis; a pair of actuating sprockets connected by a drive chain mounted on the box structure, the drive chain is connected to the tracking plate for moving the FLIR camera from its retracted position to its extended position; a box frame structure mounted on the aircraft skin which includes stops on the box frame which lockingly engage the tracking plate in its extended position.

Abstract: The invention provides a quick disconnect mounting system for cabinets and partitions which entails only the removal of one or two bolt fasteners on the bottom of the cabinet and a pair of retractable pin fasteners on the upper portions of the cabinet, with an optional retractable pin fastener in the center rear of the cabinet. Each of these acoustical mounts are insulated, thus preventing vibration in the structural portion of the fuselage from entering the passenger compartment.

Abstract: An electronic self-powered propeller governor driven off the aircraft engine includes a drive shaft which drives a hydraulic pump to produce pressurized oil to move a hydraulically controlled piston connected to the propeller blade for changing the blade pitch. A hydraulic control valve which controls the position of the piston includes a spool which is positioned within the drive shaft and supplies pressure to the piston for changing the pitch of the propeller blade. The drive shaft also drives an AC generator producing an electrical RPM signal which is supplied to a linear control circuit. A manually operated RPM control produces an electrical signal supplied to said linear control circuit which is compared with the RPM signal produced by the generator and in turn the linear control circuit signals an actuator.

Abstract: An adjustable aircraft control stick comprising a vertically-positioned column pivoted about the pitch axis for controlling the elevators and a yoke member pivotally mounted to the upper end of the control column about an axis parallel to the roll axis of the aircraft for control of the ailerons. The yoke member including a series of socket openings positioned longitudinally on the yoke and a hand grip member releasably engageable with any of said sockets to adjust for different arm length pilots.

Abstract: A fuel injection type aircraft fuel system for piston aircraft engines including a gravity flow fuel tank in the aircraft; a pressurized fuel metering unit on the aircraft engine; a fuel line connecting the metering unit to the fuel tank; an engine driven pump in said fuel line positioned in the engine compartment; a vapor separator in said fuel line between the engine driven pump and the fuel metering unit; a first vapor vent line connecting the vapor separator to the fuel tank; a fuel reservoir in said fuel line between the fuel tank and the engine driven pump; a submerged auxiliary pump in said reservoir to charge said system; an auxiliary pump bypass valve connected and parallel to said auxiliary pump; and a second vapor vent line connecting the reservoir to the fuel tank.

Abstract: A two piece connecting rod assembly for a axial cylinder, internal combustion engine with each rod half having a bearing sleeve at each end for pivotal engagement with the universal joint turnion. The two rods are connected to each other at their centers and spaced apart concentric relations through a pair of raised bosses with mating surfaces and a bolt for retention of the two rod halves as a unified structure.

Abstract: A detonation detection system for internal combustion piston engines which senses pressure within each cylinder through a piezoelectric force transducers installed under each spark plug producing pressure charged signals which signal is converted from inline charge to voltage. The signal is then passed through a gating comparator which segregates out the low pressure signals associated with intake and exhaust strokes. The signal then passes through a high-pass filter which removes normal combustion pressures. The filtered signal is then processed through an RMS (root mean square) to a DC converter which continuously computes the instantaneous square of the input signal, averages it, and takes the square root of the result to provide a DC voltage proportional to the RMS of the input. The DC signal is then processed through a peak and hold circuit which holds the peak signal for an adjustable reset-time period.