Abstract: Safety device (20) for a high-pressure fluid regulator for preventing risk of combustion caused by high velocity particles entering the regulator includes an inlet body (24) having a passage in fluid communication to receive the fluid prior to supply to the regulator, to which the device is connected. A filter (60) within the inlet body filters fluid passing through the passage. A fluid disrupter (62) is disposed between the filter and the regulator so that high velocity particles are kept by the filter and disrupter from entering the regulator.

Abstract: A split roller 150 may be removed from an axle 104 without requiring access to the axle end. A split wheel hub 152 supports a plurality of peripheral rollers 180, which may be arranged in two rows spaced along the hub axis. In a preferred embodiment, the wheel hub comprises two asymmetric hub halves 134, 136 which are fastened together around an axle. Each roller in the second row may be spaced circumferentially between a pair of rollers in the first row. According to the method of the invention, the hub halves are assembled, preferably with some rollers in each of the first and second rows already mounted thereon. Other rollers in each row are then mounted to the assembled hub halves.

Abstract: This invention relates generally to hydraulic and electrical systems for aircraft belt loaders and more particularly to such systems with interlocks to facilitate efficient and safe operation. The present invention provides a hydraulic and electrical system for battery powered aircraft belt loaders which precludes actuation of the electric traction drive motors when the brake is applied or set, or without the operator seat being occupied, which precludes actuation of the belt conveyor if the brake is not set, which controls conveyor run time and requires that the conveyor be reset to neutral before being actuated the hydraulic pump to permit power steering when the operator seat is occupied, and which requires that the directional control lever for traction drive be reset to neutral after demounting the seat before the electric traction drive motors can be energized.

Abstract: An aircraft loader having a mobile frame and hydraulically actuated components, includes a substantially rectangular frame hinged to and cantilevered from the mobile frame. The rectangular frame includes a pair of long tubes and a pair of short tubes which are sealingly connected to form a fuel tank. An internal combustion engine is mounted on the rectangular frame and drives a hydraulic pump which supplies hydraulic fluid under pressure to the components.

Abstract: An aircraft belt loader having electric motors to power the drive wheels and an electrically driven hydraulic pump for actuation of a hydraulic ram for elevation of a belt conveyor. A battery pack and the hydraulic compartment are positioned between the drive wheels and the steerable wheels and are spaced apart laterally to define a channel to accommodate the linkage including the hydraulic ram, supporting the conveyor.

Abstract: A side guide for an aircraft belt loader including a guide rail positioned laterally adjacent to the belt loader conveyor and pivotally supported on the belt loader conveyor frame by a plurality of links. A bell crank attached to the guide rail and the conveyor frame includes a control lever for manual rotation of the bell crank to move the guide rail between lowered and elevated positions relative to the belt loader conveyor.

Abstract: A hinge assembly having a polytetrafluorine block affixed to a support member with a guide rod having an enlarged head extending through a guide bore. A compression spring is trapped on the guide rod between the guide block and a nut affixed to the free end thereof. A tube is affixed to the head of a pin extending through the tube and aligned holes and a pair of ears positioned on each side of the tube and attached to the hinged member.

Abstract: A drive arrangement for an aircraft belt loader having a frame, an electric motor with a releasable mounting ring, a vertical support plate affixed to the frame with a circular opening, the center thereof being elevated above the frame, a flange positioned in the opening and secured to the support plate and releasably secured to the ring, and a planetary reducer with an output housing and a mounting plate, the reducer being driven by the motor; the mounting plate releasably secured to the flange and a drive wheel affixed to the housing.

Abstract: A multi-positionable rail for the conveyor of an aircraft belt loader having a rail supported by a plurality of parallel posts pivoted to the side wall of the conveyor and to the rail and collapsible under the force of gravity against a stop positioned on the conveyor side wall to a stowed position wherein the posts and rail are within the silhouette of the conveyor. A first support arm pivoted on the conveyor engages a first pin on a post to position the rail above the conveyor to function as a hand rail and a second support pivoted on the conveyor engage a second pin on a post to position the rail intermediate the stowed and hand rail position. A latch trapped on the post above the first pin is urged by gravity to engage the pin to prevent disengagement of the first arm from the first pin.