Patents Assigned to Curtiss Wright Flight Systems, Inc.
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Patent number: 6375381Abstract: A joint assembly is provide between a machine element gear and a shaft or between two shafts. The joint is brought about by forming a predetermined configured surface on the exterior of the machine element and forming a similar configuration of the same general dimensions on a raised surface on the shaft. The shaft is initially inserted into the machine element in a light force fit so that the similar predetermined configurations on the machine element and the raised surface of the shaft are in alignment. A metal cylindrical torque ring is positioned over and surrounding the two mating and abutting predetermined surfaces. By the process of magneforming, the cylindrical torque ring is deformed inwardly to be tightly pressed against the predetermined surfaces, thereby spanning the exterior of those surfaces and providing a tight joint between the machine element and the shaft.Type: GrantFiled: January 6, 2000Date of Patent: April 23, 2002Assignee: Curtiss Wright Flight Systems, Inc.Inventors: Gary Steven Ruschke, Desi J. Fulenta
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Patent number: 5779587Abstract: A jam-tolerant geared rotary actuator, capable of performing in a normal operating mode and a jam-tolerant operating mode, which includes: an output spline member for releasably connecting the movable ring gear to the output ring; a decoupling member which includes an input shaft disposed within a hollow timing shaft, and a shear member for sensing excessive torque and initiating the jam-tolerant mode; a sun gear spline member for connecting the sun gear to the hollow timing shaft; an axial displacement member for engaging the output spline member with the movable ring gear and the output ring; and an input engagement member for releasably connecting the axial displacement member to the input shaft. The axial displacement member includes a decoupling bushing and a double threaded decoupling nut. The nut is disposed between the timing shaft and the decoupling bushing.Type: GrantFiled: August 30, 1996Date of Patent: July 14, 1998Assignee: Curtiss Wright Flight Systems, Inc.Inventor: William Reilly
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Patent number: 5195840Abstract: A torque transmission shaft assembly for connecting a drive shaft and driven shaft which are mutually spaced less than the length of the assembly. The assembly includes a rigid elongated hollow rod member having a body portion and first and second open end portions. Each end portion is adapted to receive either the drive or driven shafts, and is provided with internal involute splines for mating with corresponding external splines on the shafts to be connected by the assembly. The first end portion has an axially displaceable stop member and a biasing spring compressible by displacement of the stop member away from the open first end, for biasing the stop member against the shaft received in the first end portion. The second end portion has a rigid stop at the end of its internal splines, for abutting against the end of the shaft receivable therein.Type: GrantFiled: December 10, 1991Date of Patent: March 23, 1993Assignee: Curtiss Wright Flight Systems, Inc.Inventors: Gary S. Ruschke, Richard S. Smarz
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Patent number: 4979700Abstract: A rotary geared actuator for pivotally connecting a flap to a wing of an aircraft, includes at least two adjacent actuator slices rotatably coupled together, each actuator slice including a sun gear rotatably coupled to a drive shaft and having gear teeth with a curved profile to enable movement of the actuator slices with respect to each other in conformance with bending of the wing, planetary gears in surrounding and meshing engagement with the gear teeth of the sun gear, a movable ring gear in surrounding and meshing engagement with the planetary gears, and a fixed ring gear in surrounding and meshing engagement with the planetary gears on opposite sides of the movable ring gear, each fixed ring gear being in meshing engagement only with planetary gears of one actuator slice; at least one fixed side tie bar connecting each fixed ring gear with the wing; at least one movable flap side tie bar connecting each movable ring gear with the flap; securing pins for securing each fixed side tie bar to one fixed rinType: GrantFiled: October 28, 1988Date of Patent: December 25, 1990Assignee: Curtiss Wright Flight Systems, Inc.Inventors: Robert K. Tiedeman, Michael A. Palma
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Patent number: 4579201Abstract: The bidirectional, torque-limiting, drive and brake mechanism has an input and output drive shafts and a helical spring which is normally in interference fit with the mechanism housing and, in the torque transmitting mode of operation, is disengaged to permit torque transmission by a direct mechanical coupling between the input and output drive shafts. The torque-limiting component, which functions to interrupt transmission of rotation from the input drive shaft to the output drive shaft upon a predetermined torque load, is adjustable to a selected predetermined torque load in the field.Type: GrantFiled: May 16, 1983Date of Patent: April 1, 1986Assignee: Curtiss Wright Flight Systems, Inc.Inventor: Robert K. Tiedeman