Abstract: Apparatus and methods are provided to minimize the escape of fuel out of a fuel tank when a tank wall is penetrated by a bullet. In one embodiment, a pressure differential may be maintained between a pressure within a fuel tank cavity and another pressure outside the fuel tank cavity in order to minimize the loss of fuel upon penetration of the fuel tank. In another embodiment, a compressed rubber layer of fuel-reactive rubber may be provided which is adapted to be attached to a fuel tank wall and to swell upon contact with fuel in order to substantially seal a penetrated hole in the fuel tank wall.

Abstract: A launch device may be prepared for launch. The launch device may be assembled in a horizontal position on a mobile device. A lifting device attached to the mobile device may be coupled to the launch device. The launch device may be moved to a launch site using the mobile device. The launch device may be moved to a vertical position at the launch site using the lifting device. The launch device may be launched.

Abstract: In one embodiment, a device for hanging a ceiling panel may include a clevis for attachment to a support structure, and a hinge for attachment to the ceiling panel. The clevis may include a pin and a first locking member. The hinge may include an elongated slot and a second locking member. The elongated slot may be adapted to be slid over the pin of the clevis. The second locking member may be adapted to engage the first locking member to lock the hinge and the ceiling panel into position.

Abstract: A free-hand inspection apparatus for non-destructively inspecting a structure includes an array and an inertial sensor. The array includes a plurality of elements for transmitting and receiving inspection signals towards and from a structure being inspected. The inertial sensor measures acceleration and angular rotation rate in X, Y, and Z directions of the array.

Abstract: A method and apparatus for making a mesh reflector that may be used to produce a shaped reflector is provided. The mesh reflector may be an umbrella-style deployable mesh reflector capable of approximating both parabolic and arbitrarily shaped reflecting surfaces, including those with regions of reversed curvature. The reflecting surface may be provided by a soft mesh attached to a highly pre-tensioned net composed of two sets of substantially parallel chords forming a plurality of parallelogram-shaped facets. The net/mesh may be made to conform to the desired shape by pulling and/or pushing on it at each of its facet corners via a set of finely adjustable tension ties and/or compression rods, the distal ends of which react against a set of pre-tensioned catenary-shaped chords disposed on the aft side of the mesh.

Abstract: The invention discloses differing embodiments of finite element modeling methods utilizing mass distribution to model an object. In one embodiment, the finite element model of the object may be partitioned into sub-models. A determination may be made as to which elements in the finite element model are structural and as to which elements in the finite element model are non-structural. Mass properties for both the structural and non-structural elements in each sub-model may be determined. The significant non-structural masses within each sub-model may be selected and added to the finite element model. The remaining insignificant, non-structural masses may be incorporated onto the structural masses by scaling densities of the structural masses. The scaled structural masses may then be added to the finite element model. In other embodiments, objects are provided which were modeled utilizing finite element models under the invention.

Abstract: One embodiment of a method of manufacturing a textured surface may include providing a first thermally stable sheet, printing a pattern of material on the first sheet to form a three-dimensional textured surface, and curing the material, then using said first sheet to impart negative texture into Tedlar faced epoxy composite blanket, which is in turn used to impart texture into a decorative laminate.

Abstract: An apparatus for simultaneous calibration and communication of active arrays of a satellite may include a base transmitter, a satellite receiver, a satellite transmitter, a base receiver, and at least one computer. The apparatus may simultaneously transmit and receive a calibration carrier and a communication carrier at different frequencies in order to calibrate the apparatus using the calibration carrier without interrupting the communication carrier. The use of different frequencies may avoid interference between the calibration and communication carriers.

Abstract: A system for holding and aligning a radiation sensing device is described. The system includes a radiation sensing device having a sensor engagement member. The system also includes a holder having a retention member including first and second retention guides connected with opposing ends of a back plate. The first retention guide also includes a complementary holder engagement member configured to mate with the sensor engagement member at a preset position.

Abstract: In one embodiment, an apparatus is provided for preparing a cassette spool. The apparatus includes: a supply reel for supplying and unrolling tape material on original backing paper; at least one cutting member for cutting unrolled tape material while on original backing paper; a cutting surface defined in a plane; a pivoting path member adapted to move from a first position aligned in the plane to a second position aligned at least partially out of the plane; at least one removing member for removing uncut unrolled tape material from original backing paper; and a cassette spool for rolling up unrolled cut tape material on original backing paper. In further embodiments, methods are provided for preparing a cassette spool with cut tape material on original backing paper.

Abstract: A navigation system takes a graphical input and translates it into an alpha-numeric entry generally including latitude and longitude information. The system interprets the graphical entry, determines if a waypoint already exists or is depicted at the geographical location identified by the graphical entry and creates a new waypoint if no waypoint already exists or is depicted at the geographical location.

Abstract: The invention relates to versatile cargo trailer decks, and to methods for moving cargo onto such cargo trailer decks. In embodiment, a cargo trailer deck may have first and second moving apparatus attached to a deck member. The first moving apparatus may be adapted to move cargo between the back end of the deck member and the front end of the deck member, while the second moving apparatus may be adapted to rotate cargo from one orientation on the deck member to a second orientation on the deck member. The deck member may be adapted to move in backward, forward, left, right, vertical, and tilt directions, in order to align the deck member for loading and/or unloading cargo.

Abstract: The invention relates to systems and methods which may be used to determine when an uncured composite part is ready to be cured. In one embodiment, a system under the invention may comprise an infrared camera adapted to take infrared images of an uncured composite part, a heating device adapted to heat an uncured composite part, an image capture device adapted to capture infrared images taken by the infrared camera, and a computer adapted to analyze infrared images taken by the infrared camera in order to evaluate temperatures of an uncured composite part. The infrared images may be used to determine that the composite part is substantially covered, and/or completely covered, with resin and ready to be cured.

Abstract: A relay socket may include an opening for insertion of a relay into the opening, and a plurality of integral locking members for attaching and locking the relay socket to at least one of a structure surface and a relay without the use of attachment hardware.

Abstract: In one embodiment, an aircraft comprises a plurality of hoop frame support members and a landing gear enclosure comprising a curved surface. The plurality of hoop frame support members abut against and extend over the curved surface to provide support to the landing gear enclosure. In another embodiment, loads are transferred from a landing gear strut through a strut fitting, through at least one inner surface of the landing gear enclosure, through at least one outer surface of the landing gear enclosure, and into the plurality of hoop frame support members.

Abstract: An emergency descent system is provided for automatically performing an emergency descent in a vehicle. The system monitors cabin pressure altitude and if the cabin pressure altitude exceeds a preset value, the emergency descent system, may direct the autopilot to descend the aircraft to the minimum safe altitude (MSA). The emergency descent system may also communicate with ground facilities informing them of the descent.

Abstract: In one embodiment, a holding fixture is disclosed for locating and stabilizing substantially identical repeated units during joining of the repeated units. In another embodiment, a method is disclosed for manufacturing a structure comprising substantially identical repeated units. In still another embodiment, a welded structure is provided comprising a plurality of welded together substantially identical repeated units.

Abstract: A vertical situation display system for use in a vehicle such as, for example, an aircraft, is provided. A side view of an intended route of flight may be shown with altitude restrictions, airspace and instrument approach information, a projected flight path and range to airspeed symbol. The system may show terrain, weather, and traffic information along the intended route of flight. The system may be used in conjunction with a navigational display to enhance situational awareness. The system includes a computer, an electronic display device, an electronic entry device, a memory and a database. The database may contain terrain, airspace and flight planning data and may be updatable.

Abstract: A system for measuring a hole of a surface may include at least one light emitting member for emitting varied intensity flashes of light towards the hole of the surface. The system may further include a projector for projecting light beams onto the surface. The system may additionally include at least one camera for taking at least one picture of the hole of the surface each time the at least one light emitting member emits a flash of light towards the hole of the surface, and each time the projector projects light beams onto the surface. The system may also include a computer for determining measurements of the hole of the surface utilizing the at least one picture of the hole and Photogrammetry.

Abstract: An assembly may include at least two structures having angled edges disposed adjacent to one another forming a first gap between the at least two structures. A plurality of angled joining members may be linear friction welded adjacent to one another between the adjacent angled edges of the at least two structures in the first gap. A second gap may be disposed between the plurality of linear friction welded angled joining members. At least one hole may be disposed at a location of the second gap. The at least one hole may extend into and between adjacent edges of the welded angled joining members, and may extend into and between the adjacent angled edges of the at least two structures. A plug member may be rotary friction welded at least partially into the at least one hole.