Abstract: A planet gear for use in an air turbine starter is formed of a first part having a set of gear teeth at a first axial location. A shaft extends axially away from the first set of gear teeth. A second part is interference fit on the first part, with the second part having a second set of gear teeth. The second part is mounted on the shaft of the first part. An outer diameter of the shaft is selected to be significantly larger than an inner diameter of a cylindrical portion of the second part which is interference fit on the shaft. A ratio of the outer diameter to the inner diameter is between 1.0005 and 1.0100. A planetary gear system, an air turbine starter and a method of installing a planet gear are also disclosed.

Abstract: An assembly includes an output shaft, an input shaft with an internal reservoir, and a clutch. The clutch is adapted to selectively engage and couple the input shaft to the output shaft. The clutch has a pressure chamber that communicates with the reservoir of the input shaft. The reservoir has a sufficient volume to provide the pressure chamber with a fluid pressure adequate to maintain engagement of the clutch during an interruption of a fluid supply to the input shaft and clutch.

Abstract: An aircraft includes a powerplant system operable to power a main rotor system and a secondary thrust system, the secondary thrust system is selectively driven through operation of a clutch system, and a clutch system synchronization time corresponds to a response time of the powerplant system.

Abstract: A method of manufacturing a gear cluster from a first gear body and a second gear body comprises producing a first set of gear teeth on the first gear body such that each tooth on the first set of gear teeth has a first pitch point. The second gear body is axially aligned with the first gear body. A timing position for a second set of gear teeth on the second gear body is determined by dimensioning from the first set of gear teeth. A second set of gear teeth on the second gear body is produced based on the timing position and each tooth on the second set of gear teeth has a second pitch point. The gear cluster is inspected for timing position by measuring a reference dimension between the first pitch point and the second pitch point.

Abstract: An assembly includes an output shaft, an input shaft with an internal reservoir, and a clutch. The clutch is adapted to selectively engage and couple the input shaft to the output shaft. The clutch has a pressure chamber that communicates with the reservoir of the input shaft. The reservoir has a sufficient volume to provide the pressure chamber with a fluid pressure adequate to maintain engagement of the clutch during an interruption of a fluid supply to the input shaft and clutch.

Abstract: A hydraulic clutch assembly includes a plurality of frictional clutch discs moveable between an engaged condition and a disengaged condition, wherein the engaged condition provides a transfer of rotational energy. Also included is a first toroidal hydraulic chamber configured to depress the plurality of frictional clutch discs into the engaged condition. Further included is a second toroidal hydraulic chamber opposing the first toroidal hydraulic chamber, wherein the second toroidal hydraulic chamber is configured to balance centrifugal expansion forces of the first toroidal hydraulic chamber. Yet further included is a lubrication circuit for supplying a hydraulic fluid from a fluid reservoir to the second toroidal hydraulic chamber and the plurality of frictional clutch discs, wherein the second toroidal hydraulic chamber is substantially filled prior to delivery of the hydraulic fluid to the plurality of frictional clutch discs.

Abstract: An aircraft includes a powerplant system operable to power a main rotor system and a secondary thrust system, the secondary thrust system is selectively driven through operation of a clutch system, and a clutch system synchronization time corresponds to a response time of the powerplant system.

Abstract: A planet gear for use in an air turbine starter is formed of a first part having a set of gear teeth at a first axial location. A shaft extends axially away from the first set of gear teeth. A second part is interference fit on the first part, with the second part having a second set of gear teeth. The second part is mounted on the shaft of the first part. An outer diameter of the shaft is selected to be significantly larger than an inner diameter of a cylindrical portion of the second part which is interference fit on the shaft. A ratio of the outer diameter to the inner diameter is between 1.0005 and 1.0100. A planetary gear system, an air turbine starter and a method of installing a planet gear are also disclosed.

Abstract: A hydraulic clutch apparatus includes a first hub, wherein the first hub includes a plurality of frictional clutch discs arranged therein, and a second hub arranged within the first hub and proximate the plurality of frictional clutch discs, wherein the second hub includes a first toroidal hydraulic chamber configured to depress the plurality of frictional clutch discs and a second toroidal hydraulic chamber opposing the first toroidal hydraulic chamber.

Abstract: A method of manufacturing a gear cluster from a first gear body and a second gear body comprises producing a first set of gear teeth on the first gear body such that each tooth on the first set of gear teeth has a first pitch point. The second gear body is axially aligned with the first gear body. A timing position for a second set of gear teeth on the second gear body is determined by dimensioning from the first set of gear teeth. A second set of gear teeth on the second gear body is produced based on the timing position and each tooth on the second set of gear teeth has a second pitch point. The gear cluster is inspected for timing position by measuring a reference dimension between the first pitch point and the second pitch point.

Abstract: A fuel cap assembly for use on fuel tanks on large vehicles such as straight trucks and buses for reducing and preventing fuel fumes and spills from reaching outside of the fuel tank during fuel filling operations. The cap assembly has interior facing threads that wrap about exterior facing threads on the fuel receiving receptacles on the fuel tanks. The cap assembly includes a lid having a normally biased closed door that only opens when a fuel nozzle is pressed into the door. The cap assembly can be elongated to allow for an interior chamber that allows for an extra catch to stop fuel from reaching outside the tank during the filling of the fuel tank. An O-ring type seal also helps lockably seal the cap assembly to the fuel tank receptacle.

Abstract: An engine system with a gear train to provide engine timing. A technique to minimize backlash and noise caused by the gear train is included. An anti-backlash gear assembly useful to reduce backlash in the gear train is also disclosed. One disclosed gear assembly has at least two gear wheels with the circular thickness of the teeth of one gear wheel being less than the circular thickness of the other gear wheel. A gear assembly is also disclosed that has a bias torque of at least about 100 foot-pounds. A device carried on an anti-lash gear assembly to generally align teeth of the assembly for installation is also provided.

Abstract: An engine includes a gear train to provide engine timing. There is a technique for minimizing the backlash and noise caused by the gear train. There is also an anti-backlash gear assembly useful to reduce backlash in the gear train. One gear assembly has at least two gear wheels with the circular thickness of the teeth of one gear wheel being less than the circular thickness of the other gear wheel. There is also a gear assembly having a bias torque of at least about 100 foot-pounds. There is also a device carried on an anti-lash gear assembly to generally align teeth of the assembly for installation.

Abstract: An improved torsional vibration isolator assembly for an engine is provided which includes a non-linear spring device which effectively minimizes the transmission of torsional vibrations to the engine's gear train throughout all engine operating frequencies and conditions while limiting relative movement between the engine's crankshaft and crank gear so as to maintain timing error within acceptable limits. The improved torsional vibration isolator is designed to absorb torsional vibrations transmitted from the crankshaft so as to substantially isolate the entire engine gear train, including the crank gear, from the torsional vibrations throughout all engine operating conditions and frequencies, including at and below the natural frequency, i.e. crank resonance, of the crankshaft. The crank gear isolator includes resilient elements positioned in cavities formed between engaging projections formed on inner and outer rings of the assembly.

Abstract: An engine system with a gear train to provide engine timing is disclosed. A technique to minimize backlash and noise caused by the gear train is included. An anti-backlash gear assembly useful to reduce backlash in the gear train is also disclosed. One disclosed gear assembly has at least two gear wheels with the circular thickness of the teeth of one gear wheel being less than the circular thickness of the other gear wheel. A gear assembly is also disclosed that has a bias torque of at least about 100 foot-pounds. A device carried on an anti-lash gear assembly to generally align teeth of the assembly for installation is also provided.

Abstract: The invention is directed to a portable wing extension for releasably securing to a roof ladder. The wing extension includes a horizontal wing section secured to slide through supports which are received within adjacent rungs of the ladder. A pair of lock pins releasably secure the wing extensions to the ladder. Wing extensions can be attached to either or both sides of the ladder. The attached wing extensions permit a firefighter to safely cut a ventilation hole in a roof beyond the width of the ladder at any location on the roof.

Abstract: The combination of a wooden stud wall and a diagonally positioned thin flat metal brace nailed to said wall and bent around diagonally opposite corners of the wall and nailed into the ends of the top plate and of the sole plate and to the stud adjoining the sole plate.