Abstract: A fastener locating and retention structure which includes a dog house attached to a part. The doghouse includes at least three walls and an opening in the fourth wall large enough for allowing a T-stud shaft portion to enter. A top surface it provided for extending inward from the walls. The top surface has an aperture formed there in by two pairs of spring retention legs which oppose each other engage the shaft portion of the T-stud on either side of the shaft thereof.

Abstract: A molded vehicle component (10) having a skin (14) and a lower density core (16) formed by a co-injection molding process. In a first phase, a first material for forming the skin of class A surface material is injected into a mold to partially fill the mold cavity (104). Thereafter, in a second phase, a second material is injected into the same cavity (104) to complete filling of the mold cavity (104). The second material can flow only to portions of the part where the first material is still molten and displaces the molten core of the first phase, pushing it away from co-injection gates until the mold cavity is full. The second material is pre-treated with a chemical blowing agent in order to reduce part weight by foaming the core material. The finished co-injection molded part (10) has one material on all visible class A surfaces (14) and a core (16) that is a different, less dense material.

Abstract: A fastener locating and retention structure which includes a dog house attached to a part. The doghouse includes at least three walls and an opening in the fourth wall large enough for allowing a T-stud shaft portion to enter. A top surface it provided for extending inward from the walls. The top surface has an aperture formed there in by two pairs of spring retention legs which oppose each other engage the shaft portion of the T-stud on either side of the shaft thereof.

Abstract: A molded vehicle component (10) having a skin (14) and a lower density core (16) formed by a co-injection molding process. In a first phase, a first material for forming the skin of class A surface material is injected into a mold to partially fill the mold cavity (104). Thereafter, in a second phase, a second material is injected into the same cavity (104) to complete filling of the mold cavity (104). The second material can flow only to portions of the part where the first material is still molten and displaces the molten core of the first phase, pushing it away from co-injection gates until the mold cavity is full. The second material is pre-treated with a chemical blowing agent in order to reduce part weight by foaming the core material. The finished co-injection molded part (10) has one material on all visible class A surfaces (14) and a core (16) that is a different, less dense material.

Abstract: Unequal loading in multiple load path transmissions having independent gear trains 18, 20, interconnecting an input and an output shaft 12 and 14, respectively, is avoided through the use of a torsionally compliant gear 22 located in each gear train 18 and 20. Each torsionally compliant gear 22 includes a hub 40 and a ring 46 having external gear teeth 48 about the hub 40 in concentric spaced relation. A body 50 of elastomeric material is disposed between the hub 40 and the ring 46 and spring fingers 68 carried by the ring 46 at least somewhat radially extend toward the hub 40. Stops 84 are carried by the hub 40 and are positioned to be normally spaced from the spring fingers 68 when low loads are transmitted by the gear and to engage the spring fingers 68 when predetermined higher loads are to be transmitted by the gear.

Abstract: An interior actuation system for controlling an exterior control surface of a torpedo or the like which has an afterbody with radial inlet vanes defining inlet liquid passages to the propellers of the torpedo. A linear actuator is mounted in the afterbody. A bell crank is connected at one end to the linear actuator and extends radially outwardly therefrom through one of the inlet vanes. A driving connection, including a link arm connected at one end to the opposite end of the bell crank, extends longitudinally from the bell crank through the afterbody outside the liquid passages and operatively interconnects the control surface to the linear actuator.

Abstract: The size of a bearing 34 required to journal a propeller 16 may be reduced by mounting the bearing 34 on a piston 44 received in a cylinder 46 and by locating a piston 62 in a groove 52 on the hub 18 of the propeller 16. The groove 52 acts as a second cylinder and opens oppositely of the cylinder 46. The two are interconnected by bores and ports 64, 66, 68, 70 and filled with an incompressible fluid.

Abstract: A propulsion mechanism for an underwater device and, more particularly, a mobile mine having directional control provided by a pair of positionable fins each independently positionable by an associated fluid cylinder having a piston rod extending therefrom with a rack engaging with a pinion gear on a rotatable shaft supporting the fin. Control valve structure independently controls delivery of fluid under pressure to the two fluid cylinders for separate movement of the fins to produce the desired direction of travel. The propulsion mechanism utilizes a gas turbine which is supplied with hot gas under pressure from a gas propellant chamber which burns solid fuel and the gas turbine is located to enable substantially straight flow-through of gas from the gas propellant chamber through the turbine and through a tubular propeller shaft for exhaust aft of the mobile mine.