Abstract: Systems and methods for asymmetrical pumping in low speed, low volume fluid recovery. According to the system and method, fluid is recovered from a well using an asymmetrical recovery motion. A walking beam is actuated about a first pivot point between an upstroke motion and a downstroke motion in response to rotation of a crank wheel. The crank wheel rotates more than 180 degrees during the upstroke and rotates less than 180 degrees during the downstroke. Further, the walking beam and the crank wheel are in communication with one another by an arm extending there between, wherein the arm is positioned on an opposite side of the first pivot point from the well.

Abstract: Systems and methods for automatic belt tensioning in low speed, low volume fluid recovery. A required amount of tension is maintained across the recovery system's belt driven components under changing torque loads and operating speeds. This is accomplished by adjusting the distance between a motor output and a speed reducer input in response to a change in torque load between the motor and speed reducer. The required amount of tension is further achieved by adjusting the distance between an output of the speed reducer and a crank wheel in response to a change in torque load between the speed reducer and crank wheel.

Abstract: A traffic awareness system displays ground-track heading information on a traffic information screen for other aircraft within the proximity range of the host aircraft. Symbols identify other aircraft locations by position on the traffic information screen and show ground-track heading by display and orientation of a ground-track heading indicator.

Abstract: A traffic awareness system displays ground-track heading information on a traffic information screen for other aircraft within the proximity range of the host aircraft. Symbols identify other aircraft locations by position on the traffic information screen and show ground-track heading by display and orientation of a ground-track heading indicator.

Abstract: A fin disengagement device for limiting the range of a projectile uses an electronic safe and arm circuit to sense launch and spin levels. Once armed, the stored energy from the electronic safe and arm circuit is dumped into an initiator or directly to explosive bolts. The initiator ignites an energetic material to separate the fin from the projectile in-flight at a predetermined time. Alternatively, the explosive bolts separate the fin from the projectile in-flight at a predetermined time. In the embodiments using an initiator and energetic material, an opening or cavity in the rear portion of the projectile body or rod adapter acts as a pressure chamber. When enough pressure has built up from the burning of the energetic material, the front hub of the fin section expands enough to disengage the threads and separates the fin section from the projectile body.

Abstract: An apparatus, method and computer program product for correcting own aircraft heading and displaying proximate aircraft traffic data on a Traffic Information Service display. The apparatus, method and computer program minimize slewing of the other aircraft data across the display during aircraft maneuvers and provides a more reliable and consistent depiction of traffic relative to own aircraft position.

Abstract: An apparatus, method and computer program product for correcting own aircraft heading and displaying proximate aircraft traffic data on a Traffic Information Service display. The apparatus, method and computer program minimize slewing of the other aircraft data across the display during aircraft maneuvers and provides a more reliable and consistent depiction of traffic relative to own aircraft position.

Abstract: A fin disengagement device for limiting the range of a projectile uses an electronic safe and arm circuit to sense launch and spin levels. Once armed, the stored energy from the electronic safe and arm circuit is dumped into an initiator or directly to explosive bolts. The initiator ignites an energetic material to separate the fin from the projectile in-flight at a predetermined time. Alternatively, the explosive bolts separate the fin from the projectile in-flight at a predetermined time. In the embodiments using an initiator and energetic material, an opening or cavity in the rear portion of the projectile body or rod adapter acts as a pressure chamber. When enough pressure has built up from the burning of the energetic material, the front hub of the fin section expands enough to disengage the threads and separates the fin section from the projectile body.

Abstract: An improved lifting system is disclosed for pumping liquid such as oil from a subterranean pump using a band-and-pulley assembly. The device uses a single-piece band shaped in the form of an elongated loop. Both intermediate lengths of the looped band are draped together over a rotating pulley assembly mounted near the top of a derrick. The loop formed by one end of the band supports a first end-roller assembly coupled to the polished rod assembly, which is in turn coupled to the subterranean pump. The loop formed by the other end of the band supports a second end-roller assembly coupled to the counterweight assembly The counterweight assembly is reciprocated vertically by a drive motor, thereby driving the intermediate lengths of the band over the top, supporting pulley. The end rollers have sufficient diameter and rotational freedom to permit movement of the band, and the bearing of great weights, without damaging the band.

Abstract: A variable-speed drive controller and associated methods are disclosed for reciprocated lifting systems, particularly long-stroke, fluid-pumping systems such as certain oil-producing equipment. A variable-speed drive is controlled through an electronic feedback loop by a programmable controller, which varies the speed of the drive when sensors detect the passage of the reciprocating mechanism. The controller can be set to slow the drive when the reciprocating mechanism reaches the end of the stroke, to permit faster production of fluid without increased mechanical wear on the reciprocating mechanism or increased stress on the lifting string. The controller also can be set to slow the drive on the downstroke, such as to permit faster production of fluid when pumping viscous liquid.

Abstract: A composite, layered shield for protecting a vehicle housing explosives in an ammunition stowage compartment from the detonation of said explosives while in said compartment. Said shield comprises, in a layered fashion, a first layer of an energy absorbing rubber, a pusher plate layer, a crush element layer, and a second layer of an energy absorbing rubber. In order to protect the vehicle, the ammunition stowage compartment is lined with the composite, layered shield of the present invention. The shield is mounted in such a manner that the energy absorbing rubber is closest to the explosives, followed by the pusher plate, then the crush element, and finally the second energy absorbing rubber layer. The overall areal density of the shield is about 17.6 pounds per square foot. Said shield is light weight and provides effective blast and shock protection for the walls of the explosive containing stowage compartment as well as for the vehicle housing the stowage compartment.

Abstract: A pumping unit has a drive train comprising a very large mass including large diameter series connected sheaves, one of which is a large crank sheave. The crank sheave is directly connected to a pitman arm which oscillates a walking beam, which in turn reciprocates a horsehead attached to a bridle. The bridle is connected to a polished rod associated with a downhole pump. The crank wheel, pitman arm, and rocking beam are arranged respective to one another to cause the tail bearing to oscillate predominantly in the second quadrant, and to cause the center of gravity of the pitman arm to be located predominantly between the vertical axis of the crank wheel and the Samson post bearing. The geometry of the crank wheel, pitman arm, and rocking beam provides substantially constant, positional of the polish rod on the downstroke, with rapid positional occurring at peak polish rod velocity, which causes a longer downhole pump stroke because of the induced elongation of the sucker rod string.

Abstract: A pumping unit has very large series connected crank and flywheel sheaves. The crank sheave is connected to oscillate a walking beam which reciprocates a horsehead attached to a bridle. The bridle is connected to a polished rod associated with a downhole pump.