Abstract: A disposable liquid bait station is configured in the form of a syphon with a bulbous end portion and a stem portion having a passage extending from the end of the stem into the bulbous end portion for syphoning liquid bait from a bottle containing the liquid bait. The stem is cut-off and the remaining portion serves as the bait station. The bait station is then placed in a horizontal position at the desired locations for permitting the ingress and egress of the ants intended to being exterminated. The bait station is thrown away once it has served its purpose.

Abstract: The radius of the hinged portion of the convergent/divergent axisymmetrical exhaust nozzle of a gas turbine engine is configured at the surface seeing the flow to be contoured at a critical radius so to enhance the flow characteristics of the nozzle and improve the low observable. The liner normally associated with the convergent flap is cut back at the juncture adjacent the hinged point connecting the divergent flap to be below the radar sight at the tail of the engine.

Abstract: An electromagnetic generator without moving parts includes a permanent magnet and a magnetic core including first and second magnetic paths. A first input coil and a first output coil extend around portions of the first magnetic path, while a second input coil and a second output coil extend around portions of the second magnetic path. The input coils are alternatively pulsed to provide induced current pulses in the output coils. Driving electrical current through each of the input coils reduces a level of flux from the permanent magnet within the magnet path around which the input coil extends. In an alternative embodiment of an electromagnetic generator, the magnetic core includes annular spaced-apart plates, with posts and permanent magnets extending in an alternating fashion between the plates. An output coil extends around each of these posts. Input coils extending around portions of the plates are pulsed to cause the induction of current within the output coils.

Abstract: In one embodiment a hand operated machine for making curly ribbon products comprises a rotary drum that includes a station to attach the uncurled ribbons (more than one), a cutting station to cut the curled ribbons, and a stapling station to staple the ribbons together or to a card, ribbon, or the like. A handle is provided to rotate the drum and a fixed curling mechanism mounted downstream of the drum serves to curl the ribbon as the drum rotates to place the ribbon in contact with the curling mechanism. In another embodiment the machine is automated and includes a drum that has the same stations. The attaching station includes a pair of jaws that are sequentially movable one relative to the other and together to attain attaching the ribbons to the drum for the first cycle, detaching the ribbon during the first cycle and attaching the succeeding ribbon used in the next cycle for mass producing the curly ribbon product.

Abstract: Brush seals formed in hemispherical rings are supported to the end of the convergent nozzle of the each of the clam shells of a multi-axis vector thrust nozzle of a gas turbine engine powering aircraft. The brush seal may be arced or straight and bear against the spherical surface of the collar formed on the end of the tail pipe and is mounted so that high pressure forces the bristles against the backing plate of the seals.

Abstract: A fuel/mixer injection system for a combustor of a gas turbine engine comprising two major assemblies including a burner-mounted swirler with two outer air passages surrounding a central passage and a piloted air fuel nozzle containing a main fuel injection orifice and a pilot fuel injection orifice the main fuel mixes with swirling air in the central passage and the pilot fuel mixes with the swirling air in the outer air passage. In another embodiment, the piloted fuel nozzle contains an airblast-atomized main fuel injector annulus and a concentric ring with a plurality of circumferentially spaced holes feeds air to the main fuel injector annulus.

Abstract: A deployable wing that is folded so as to fit into a carrier such as an airplane that is released and automatically with the aid of parachutes to deploy and fly a given distance without assistance other than steering to reach a given destination and a propeller driven by a gas powered engine is actuated to propel the wing an extended distance. A guard is disposed adjacent to the propeller to assure that the lines of the parachutes do not get tangled into the propeller blades.

Abstract: A shut-off system that is semi-automatic or fully automatic shuts off the mechanism for flowing resin, air and filler to a miniaturized convergent spray gun so as to stop the flow of the ingredients of being sprayed and purging the spray gun so that the residue ingredients do not cure and destroy the gun.

Abstract: A seal for the aft end of a turbine blade and disk assembly of a gas turbine engine to prevent leakage of the cooling air whose main body and cross section are U-shaped that freely fits into a groove formed in the disk lug adjacent the rim of the disk on the aft side thereof. When rotating the center of the base of the U bears against the buttress of the platform of the blade and centrifugal force forces the sides of the U to deform to bear against the walls of the groove.

Abstract: The end wall of the compressor adjacent the stator vanes and compressor blades is configured so that the annular region between the vanes and blades is held at a constant area and that the flow path convergence of the stator is increased to compensate for the loss of convergence due to the reduction of convergence in the annular region between vanes and blades.

Abstract: The blade firtree bearing surface and/or the disk broached slot bearing surface is “crowned” to reduce the stresses at the edges thereof and more uniformly distribute the load. The width of the bearing surface is increased over the conventional flat bearing surface of the blade firtree and/or the bearing surfaces of the disk broach by judiciously moving the contact point to a discrete location.

Abstract: The cooling of the exhaust nozzle of a fan jet engine powering aircraft is enhanced by providing an extension cooling concept that includes an extension piece extending axially downstream of the nozzles variable throat that utilizes fan air to cool the forward portion of the divergent nozzle surfaces adjacent to the gas path of the engine and ram air to cool the surfaces downstream of the ejector. A variable vane varies the area of the ejector slot as a function of Aj for compensating for flow losses at off-design points of the nozzle positions during the flight envelope of the aircraft so as to avoid overtemperature of the components.

Abstract: The horsepower requirements for the actuation system for a convergent/divergent exhaust nozzle for a gas turbine engine is reduced by the judicious selection of the crank arms and their location on a torque shaft that rotates to move a connecting link attached to the convergent flap of the nozzle. A pressure balancing hood is attached to the top surface on the forward end of the convergent flap to augment the lowering of the horsepower requirements. In another embodiment a tie rod/end cup arrangement and two piece torque shaft are utilized for ease of removal of the actuation system from the exhaust nozzle assembly.

Abstract: A drilling rig is constructed into modules for ease of mounting and removing from the bed of a vehicle such as a truck and includes a sled module that horizontally moves the drill fore and aft of the bed, and an integrated boom support tower that includes platens that pivotally mount the boom for storing and deployment. The controls are mounted on the support tower in a convenient location for ease of operating the drill.

Abstract: The openings in the fabric ribs of a deployable wing made from fabric sail material is automatically closed by use of a zipper mounted adjacent each of the openings that is actuated by movement of the cross spars of the deployable wing which serves to prevent the airfoil surface to the wing to bulge and cause a drag to the deployable wing when in flight.

Abstract: The present invention relates to a protective sleeve for a chronically-implanted intravenous (IV) site. The sleeve is made of a prophylactic waterproof material, and is normally worn by a person while showering to prevent moisture from invading the IV site. The sleeve in one embodiment has two elastomeric beads which form a watertight seal between a person's arm and the beads, and the sleeve billows in its mid-section so that it does not snag the catheter. The sleeve in another embodiment has a binding at one end and at least a binding at the other end integrally formed in the sleeve or in another embodiment a plurality of indentations axially spaced on a tapered portion of the sleeve.

Abstract: The effectiveness of a radial inlet air swirler for the fuel nozzle in the combustor of a gas turbine engine is enhanced by reducing the pressure loss associated with compressor discharge air as it enters the combustor cowl. A circumferential uniform feed pressure is created by an aerodynamically contoured projection on the pressure plate supporting the fuel nozzle and a cooperating dynamic swirler scoop at the inlet of the swirler. The increased flow and fuel/air mixing reduces smoke production without adversely affecting combustor or engine performance.

Abstract: A bridge monitoring system uses laser light reflected from structural members of a bridge to create velocity and displacement time signals of the bridge's vibratory response to quiescent conditions, and converts the sensed velocity and displacement time data to frequency domain data to provide a “signature” waveform for the bridge indicative of its structural characteristics.

Abstract: A display device displays the effects of variations in the level of an individual parameter within a matrix of transformed parameters of a type which is processed through an inverse transform to form a video signal. A signal representing the single parameter, with other parameters set to zero, is scaled using differing constants to form a left intermediate signal and a right intermediate signal, each of which is processed through an inverse transform to form video data, which is then displayed on a left and right display screen. The images on the two screen are compared by a human user to determine whether there is a difference between the images as viewed through human eyes.

Abstract: A system for distributing weather information accepts differing types of such information for storage in a number of databases. Data representing levels of precipitation are stored in an overall database, to be overwritten as new data becomes available. Data representing storm warnings and lightening strikes are stored in a time-sensitive database, to be erased according to a predetermined schedule. Data representing a satellite photograph of cloud cover are stored in a cloud map database. These databases are read to obtain data which is transmitted to terminals within various regions, so that each terminal receives weather information for an area surrounding its region.