Abstract: An aircraft structure includes a duct having an inlet for fluid flow into the duct and a first outlet for fluid flow out of the duct. The duct is configured to guide fluid flow out of the duct through the first outlet in an at least partially reversed direction relative to fluid flow into the duct to thereby reverse thrust.

Abstract: A method for using an end effector for inspecting a structure is provided. An end effector includes a magnetically coupled attachment member for connecting the end effector to a control system bridge. An end effector also includes a telescoping arm at least partially disposed inside a tube. A force mechanism provides a force to extend the arm from the tube. A probe attachment, connected to the end of the arm opposite the tube, provides motion in at least one axis relative to the arm for an inspection probe attached to the end effector. Cut-off switches can be used to alert a control system to a separation of the end effector from the bridge and proximity of the bridge to a structure under inspection.

Abstract: An end effector for inspecting a structure is provided. An end effector includes a magnetically coupled attachment member for connecting the end effector to a control system bridge. An end effector also includes a telescoping arm at least partially disposed inside a tube. A force mechanism provides a force to extend the arm from the tube. A probe attachment, connected to the end of the arm opposite the tube, provides motion in at least one axis relative to the arm for an inspection probe attached to the end effector. Cut-off switches can be used to alert a control system to a separation of the end effector from the bridge and proximity of the bridge to a structure under inspection.

Abstract: An apparatus and method for inspecting a structure are provided which include probes with sensing elements and are disposed proximate opposite surfaces of a structure, where only one of the probes need be driven. A tracking probe may be magnetically coupled to a driven probe and move in coordination therewith. Ring magnets may be used in the driven and tracking probes to provide the magnetic coupling and align sensing elements disposed in the centers of the ring magnets. The probes may include a fluid bearing, such as a water bearing or an air bearing, for supporting the structure and maintaining the desired orientation and spacing of the probes relative to the structure. The fluid of a fluid bearing may be used as a couplant between an ultrasonic transducer and a structure. A flow moderating skirt may be used to with a probe employing a fluid bearing for support.

Abstract: There is provided an ultrasonic inspection device that provides a locking mechanism for inspecting components at preset angles. The inspection device can inspect a component along an arc by inspecting the component at each preset angle, which provides complete and repeatable inspection results. The inspection device comprises a housing with a channel for the passage of an ultrasonic signal and an ultrasonic transducer to transmit and receive the ultrasonic signals. The housing also includes a rotating reflector to reflect the ultrasonic signal. Using a handle on the housing rotatably attached to the rotating reflector, a technician can rotatably position and lock the rotating reflector at a preset angle. The rotating reflector can be rotatably locked by a spring-loaded ball that is selectively received in detents defined by the rotating reflector or handle.

Abstract: An insulated gate field effect transistor (IGFET) memory or logic circuit is implemented at higher density levels by employing thick oxide IGFET's as load elements. Additionally, the gate electrode structure of the IGFET load devices and their channel lengths with respect to the channel length of parasitic IGFET devices are selectively controlled in order to insure that the parasitic devices remain nonconductive.