Abstract: The invention disclosed here is a pin hub that is to be used in conjunction with interchangeable wire reels for taking individual wire segments from a continuous wire feed. In use, an empty reel is first mounted to the pin hub. The pin hub has a plurality of pins which are arranged in a circular pattern, and are retracted relative to the hub at the time the reel is mounted. After mounting, the pins are extended through corresponding side openings in the reel, and thereby define a winding hub or circle within the reel itself. Instead of being wound directly against sidewall or hub structure of the reel itself, the wire is instead wound about the pins, and they take up the physical stresses associated with the winding process. After winding is completed, the pins are retracted, and the filled reel is thereafter removed from the pin hub.

Abstract: A starter plant (10) is planted in soil (17) in a bottomless container (18), which is placed on a support surface (28). The plant is allowed to grow in a controlled environment until a time in its growing season when its root system is sufficiently developed to hold the soil (17) in the container (18) when the container (18) is removed from the surface (28). Then, the plant and the container (18) are planted as a unit in soil (30) in a field. The plant is allowed to grow to full size in the field, where it develops a densely rooted basal plate (32) inside the container (18) and feeder roots (34) that extend below the bottom of the container (18) into the soil (30). The plant is harvested from the field by undercutting the feeder roots (34) and removing the container (18) and the plant as a unit from the soil (30). The foliage (12) may be trimmed to a volume no bigger than the container (18), and the trimmed plant (38) may be stored or shipped.

Abstract: A brush cutter work head (20) has a protective shroud (36) with a vertical side opening (40) to expose a portion of a circular cutting blade (42) to enable the blade (42) to cut brush. A spray nozzle (82) is mounted on a sliding member (74) that slides within a tubular housing (58) incorporated into the work head housing (28). The sliding member (74) has a retracted position in which the nozzle (82) is positioned above a portion of the housing (28), and a projecting use position in which the nozzle (82) is aligned with the opening (40) above and outward of the blade (42). A gripping thumb (44) is pivotally mounted on the work head housing (28) and is operated by an actuator (52) within the housing (28) to pivot between a flush nonuse position and a gripping position in which it opposes a jaw (38) formed by a lower portion of the shroud (36).

Abstract: An internal check valve for use in a linear hydraulic motor in the form of a piston-cylinder unit including a cylinder body (38) reciprocally slidable on a piston component (40). The piston component (40) includes a tubular piston rod (52) and a piston head (60) defining first and second working chambers (136, 140) within the cylinder body (38). The tubular piston rod (52) includes a center tube (102) located within the piston rod (52). The center tube (102) provides a fluid passageway (134) through its center which communicates with a first working chamber (136). An annular second passageway (142) is formed by and radially between the piston rod (52) and the center tube (102). A spring biased check valve (116) is positioned within the piston rod (52, 54) and is operatively connected with one of the passageways (134, 126, 130). The check valve (116) has a valve member displaceable from a valve seat (120) by hydraulic pressure to overcome the spring bias (122, 124) and allow flow in one direction.

Abstract: A valve plug is biased inwardly by a spring (90) to close an opening (10) in a cap (2) for a fuel tank filling and venting tube. A valve stem includes a first portion (62) which is engaged by the spring (90) and a second float cage portion (40) that is secured to and extends axially inwardly from the plug. A collapsible retainer (70) is secured to the cage (40) and has an abutment surface (74) which engages an abutment surface (68) on the first portion (62) to hold the cage (40) and the first portion (62) in position relative to each other and to transmit axial forces therebetween. A fusible material ring (88) is positioned radially between the retainer (70) and the cage (40) to prevent the retainer (70) from collapsing. At elevated temperatures, the ring (88) melts to allow the retainer (70) to collapse, the cage (40) and first stem portion (62) to separate from each other, and the valve plug and cage (40) to move away from the opening (10).

Abstract: A heater circuit in a vehicle engine cooling and passenger compartment heating system comprises a control valve (26), and a supply line (22) and a return line (24) both of which are separate from the radiator circuit of the system. A bypass passageway (48) extends between the supply line (22) upstream of the valve (26) and the return line (24) downstream of the valve (26). A bypass valve normally closes the passageway (48) and opens in response to a pressure differential between the supply line (22) and return line (24) exceeding a predetermined magnitude. The passageway (48) has first and second detachably connected portions that communicate with the supply and return lines (22, 24) via radial openings (44, 46). A spring (72) abuts a shoulder (54) in the second portion and a valve element (62) that seats against a flat surface surrounding the radial opening (44) in the supply line (22). The element (62) has laterally extending guide teeth (68) and a rear reduced diameter lug (70) engaged by the spring (72).

Abstract: The invention disclosed here is a wire reel that is designed to be used in connection with an automated wire handling system. The reel has a generally planar stiffback, and a circular flange that is releasably connected to the stiffback. The stiffback and flange together define a circular winding space for coiling a wire onto the reel. The stiffback also carries two, spaced-apart clamps which are positioned outwardly with respect to the outer perimeter of the flange. These clamps hold the opposite ends of the coiled wire. The stiffback is shaped so that it is suitable for gripping and handling by a robotic arm or the like.

Abstract: An automated wire stripper has a forward wire-gripping assembly, a rearward insulation-pulling assembly, and a rotatable knife hub assembly positioned intermediate of the forward and rearward assemblies. The knife hub assembly includes a pair of thermal knife elements which are spring-biased to normally close upon the end of a wire. Pneumatic actuators open the knife elements against the bias of the springs. The rearward assembly is operable to clamp and pull a section of outer jacket or insulation covering from the wire after the knife hub has cut around the its circumference of the jacket.

Abstract: The piston rods (10, 12, 14) of three linear hydraulic motors (M1, M2, M3) are stationary and include fluid pressure passageways (40, 52, 42, 54, 44, 56) which direct fluid pressure into and out from working chambers (16, 34, 18, 36, 20, 38) on opposite sides of piston heads (22, 24, 26). Movable cylinder barrels (16, 18, 20) are connected to a load, e.g. floor members (FM1, FM2, FM3) of a reciprocating floor conveyor (FIG. 18 ). The outer ends of the piston rods (10, 12, 14) include balls and the balls include ports (46, 58, 48, 60, 50, 62) through which fluid pressure is delivered or removed. Associated with each port is a limit valve LV1, LV2, LV3, LV4, LV5, LV6. Limit valves (LV1, LV2, LV3) are pushed into an open position by a retraction of the motors (M1, M2, M3). Limit valves (LV4, LV5, LV6) are pulled into an open position by extension of motors (M1, M2, M3). The limit valves (LV1, LV2, LV3, LV4, LV5, LV6) include springs biasing them into closed positions.

Abstract: A fault-tolerant air data and inertial navigation reference system utilizes skewed axis inertial sensors and fault-tolerant redundant electronics to provide higher redundancy with fewer parts. Parallelly operating processor circuits each receive the individual outputs of six skewed-axis gyros and six skewed-axis accelerometers. Each processor independently processes parity equations using the outputs to identify malfunctioning sensors. Further, the output of each processor is transmitted to three parallelly operating voter circuits. The voters are operable to discard a processor if its output does not agree with the majority. The voter outputs are similarly fed back to the processor circuits, which compare these outputs, and discard any voter whose output disagrees with the majority, thus providing a completely integrated system.

Abstract: Dredging apparatus (10) is provided with a flow conduit (18), a first pump (28), a second pump (30), and two valves (34, 44). The flow conduit (18) comprises a first leg (20) extending downwardly to a lower portion (22) and a second leg (24) extending upwardly from the lower portion (22). A fluidizing nozzle (32) is carried by the first leg (20). An intake aperture (26) is provided on the lower portion (22) and is directed downwardly. The dredging apparatus (10) may be used to dredge up material when the material is in a water suspension (48), and to probe through material by scattering material. The valves (34, 44) are operated to switch the apparatus between various modes of operation and to increase the effectiveness of the apparatus.

Abstract: An improved convertible aircraft seating arrangement that is adapted to convert a row of seven economy class seats into a row of six business class seats, and vice versa. A pair of outboard seats (12, 20) are positioned on opposite sides of the passenger cabin (16), and a central set of seats (18) is positioned in between. In the economy class configuration, the central set consists of three seats (36, 38, 48), but is converted to two seats for the business class configuration. When making the conversion, the outboard pairs (12, 20) are slid inwardly a certain distance, and their inboard armrests (32) are extended further into the aisleway (22, 24) on each side of the central set (18). The outer, aisle seats (36, 38) against the centermost seat (48). There, they are joined to lateral sections of the centermost seat (78a, 78b), which are split apart from such seat to form wider, business class seats.

Abstract: A control system includes a dual actuator (2) and primary and secondary controllers (20, 22), each of which has two control channels. In a normal mode of operation, the primary controller (20) controls both valves (32, 38) of the actuator (2). Each primary channel generates a model signal and a monitoring signal corresponding to expected and actual operation of the actuator, respectively. The two signals from each channel are communicated to the other channel. Each channel monitors itself as well as the other channel by comparing model and monitoring signals; and is also similarly redundantly monitored by the other channel of the controller (20). Each channel independently compares its own signals with the signals from the other channel. Each of the two channels has a deactivating switch responsive to a fault status signal from either of the two channels to thereby allow deactivation of a failed channel even when the failure in such channel prevents it from deactivating itself.

Abstract: One or more decoys (22) are towed by an aircraft (18) to confuse hostile radar. The tow lines (20) to the decoys (22) include fiber optic components which optically transmit to the decoys (22) both radio frequency signals for retransmission to hostile radar (24), and direct current power. The fiber optic components absorb strain forces imposed by towing the decoys (22). Multiple decoys (22) are deployed at varying distances from the aircraft (18) to increase the overall range of frequencies covered by the system, simulate a plurality of false targets, or accomplish angle gate deception. The deception may be accomplished by transmitting signals from the decoys in sequence and can be enhanced by dynamically varying the power levels of the decoy transmitting antennas. The fiber optic components may be separate optical fibers deployed separately or joined together for simultaneous deployment. The preferred configuration is a single optical fiber with coaxial inner and outer cores.

Abstract: A primary valve orifice (26) divides a check valve cavity into first and second portions (4, 6). A valve member (34) closes the orifice (26) in response to higher pressure in the first portion (4) and is unseated to open orifice (26) in response to higher pressure in the second portion (6). An axial passageway (44) extends through the valve member (34). A control rod (50) extends into the cavity (4, 6) and through the passageway (44). The rod (50) carries a secondary valve plug (52) that is biased by a spring (60) to close one end of the passageway (44), and a pull block (78) that engages the opposite end of the valve member (34). A stem (40) extends from the valve plug portion (36) of the valve member (34) through the orifice (26) and is telescopically received in a sleeve (62). The control rod (50) is pulled to cause the secondary valve plug (52) to unseat and the pull block (78) to engage the sleeve (62). This opens the passageway (44) to equalize pressure on the two ends of the valve member (34).

Abstract: A pilot's ensemble provides protection against cold water immersion and hostile threats, such as chemical and biological agents, while minimizing bulk and weight of the ensemble and impacts to and burdens on the pilot. The ensemble includes a garment (40) having an outer shell (14) impermeable to liquids and gases and a lining (58) bonded to an inner surface of a torso portion of the shell (14). Air is supplied to the lining (58) through a ventilation port (42) to control body temperature. Ensemble headgear includes a helmet (76) with upper and lower pairs of mounting members (78, 80, 82, 84). A permeable hood (70) is worn under the helmet (76) and has chemical vapor absorbing neck portions. A breathing mask (92) is removably attachable to the lower pair of mounting members (82, 84). Goggles (96) are removably attachable to the upper pair (78, 80). The goggles (96) seal the ocular cavity of the pilot and overlap the mask (92) and hood (70) to completely cover the pilot's face.

Abstract: The position of an aircraft control surface actuator is determined by a combination of a linear transducer and light radar. A link has a first end attached to a magnet and a second end attached to the actuator. Movement of the actuator causes the magnet to move axially along the outer cylindrical surface of a hermetically sealed housing. The transducer includes a magnetic coupling between the magnet end and a ferromagnetic follower inside the sealed housing. Preferably, the magnet is a ring magnet, and the ferromagnetic follower is a tubular cylinder. The follower carries a corner cube reflector that receives light from, and reflects light back to, the end of an optical fiber. The transit time of the light is measured and is used to calculate the distance between the fiber end and the reflector to thereby determine the position of the actuator.

Abstract: An exception processing system for use in conjunction with manufacturing facilities, and automated manufacturing cells in particular is provided. The exception processor is adapted to receive alarms from a cell controller indicating that an unplanned event or exception has occurred in cell operation. The exception processor implements an automated recovery procedure that responds to the alarm, corrects the exception, and returns the cell to normal operation. The exception processor also statistically monitors cell operation in order to avoid exceptions before they occur, and to provide better control over cell processes.

Abstract: A split sleeve (96) is seated in a fastener hole (10) in the web (8) of a rail section (2). The tapered portion (26) of a mandrel (20) is firmly seated in the hole (10) inside the sleeve (96). A puller mechanism jaw (40) and a nosecap (78) are moved downwardly over the projecting rear end portion of the mandrel (20) to position the rear end portion in aligned U-shaped slots (50, 84) in the jaw (40) and nosecap (78). During the downward movement, guide surfaces (72) carried by the jaw (40) guide a chamfer (32) on the mandrel (20) into seating engagement with a tapered surface (56) on the jaw (40). The guide surfaces (72) may be formed by cylindrical pins (70) received into angled openings (58) in the jaw body. The front surface (88) of the nosecap (78) securely abuts the Web (8). With the mandrel ( 20) seated and the nosecap (78) abutting, the jaw (40) is moved rearwardly to pull the mandrel (20) through the hole (10) and cold expand the hole (10).

Abstract: A valve plug (22, 22a, 22b) is biased inwardly by a spring (78, 78a, 78b) to close an opening (6, 6a, 6b) in a tank. A stem (32, 32a, 32b) extends axially inwardly from the plug (22, 22a, 22b). The stem (32, 32a, 32b) has an inner portion (36, 36a, 36b) which is mechanically interlocked with an outer portion (52, 52a, 52b) to directly transmit axial forces created by the spring (78, 78a, 78b). Fusible material (66, 66a, 66b) holds the stem portions (36, 36a, 36b, 52, 52a, 52b) in an interlocking position but carries only relatively small loads. The plug (22, 22a, 22b) and stem (32, 32a, 32b) move against the force of the spring (78, 78a, 78b) to relieve pressure. At elevated temperatures, the fusible material (66, 66a, 66b) melts to allow the stem portions (36, 36a, 36b, 52, 52a, 52b) to separate and the plug (22, 22a, 22b) and outer stem portion (52, 52a, 52b) to move away from the opening (6, 6a, 6b).