Climax Portable Machine Tools, Inc.

David Michael Briggs

David Loyd Sorensen

David S Strait

Andrew Gordon Thompson

Garrett Lindon Headrick

John Winfrey Dillman

Timothy S Clements

John Rogers Brooks

Brady Lynn Byers

Karl Boyd Williams

Daniel Morgan Jensen

Darren Paul Weidman

Hitesh K Patel

Joseba Brit Elola

Dominic M Bertram

Keith Richard Davis

David Ethan Ross

Jeremy Carl Conser

Pressure testing systems comprise a clamp assembly for clamping a device for testing with a test fluid, and a control assembly for controlling application of a clamp pressure to the device. The control assembly comprises a clamp control structure with an activated configuration and an inactivated configuration. In the activated configuration, the clamp control structure permits the clamp pressure to be applied to the device. In the inactivated configuration, the clamp control structure permits the clamp pressure to be released from the device. The control assembly also comprises a safety structure that is actuated by the test fluid between an interlocked configuration and a disengaged configuration. In the interlocked configuration, the safety structure physically prevents the clamp control structure from reconfiguring from the activated configuration to the inactivated configuration. In the disengaged configuration, the safety structure permits the clamp control structure to be reconfigured from the activated configuration to the inactivated configuration.

Pressure testing systems with safety interlock

Test flange assemblies comprise a flange body and a piston. The piston is configured to translate relative to the flange body and has an outer surface facing away from the flange body and an inner surface facing toward the flange body. The outer surface defines a circular seal channel for receiving a seal structure between the piston and a flange surface of a flanged component. The outer surface radially inward from the circular seal channel has a surface area that is less than a surface area of the inner surface. Methods of testing pressure containing structures comprise operatively positioning the test flange assembly, positioning a seal structure within the circular seal channel of the piston, coupling the flange body to a flanged component, and pressurizing a volume between the piston and the flange body so that the piston compresses the seal structure between the piston and the flanged component.

Test flange assemblies and related methods

Various embodiments herein provide a remotely adjustable feed system for remotely controlling the movement of a tool head on a machining tool along an axis of motion by means of converting reciprocal linear motion, i.e., back and forth linear motion, into rotary motion. The rate of movement of the tool head along the axis of motion may be controlled by varying the distance of linear motion in each cycle of linear reciprocal motion and/or by varying the rate of linear reciprocal motion cycles per unit time. Alternatively, or in addition, the rate of movement of the tool head along the axis of motion may be controlled by varying the amount of rotary motion that results from a given amount of reciprocal linear motion. Additionally, in some embodiments, the movement of the tool head may be controlled by directly controlling the rotary motion that drives the tool head along the axis of motion. The rotary motion may be controlled by adjusting the speed of continuous rotation and/or adjusting the frequency of pulsed rotations.

Remotely adjustable feed system

Machine tools and methods for machining turbine rotor assemblies are disclosed. Some machine tools include a drill arm that pushes off of a turbine stage that is adjacent to a turbine stage to be machined. Some machine tools include a clamping arm that secures the machine tool to a turbine stage to be machined and an adjacent turbine stage. Some methods include pushing-off of a turbine stage that is adjacent to a turbine stage to be machined. Some methods include securing a machine tool to a turbine stage that is adjacent to a turbine stage to be machined. Some methods include monitoring at least one of a current delivered to a first motor and a voltage applied to the first motor and controlling a second motor in response to the monitoring. Some methods include sequentially machining a turbine stage with cutting tools having increasing lengths and/or diameters.

Machine tools and methods for machining turbine rotor assemblies

Embodiments of the present disclosure provide systems, apparatus, and methods to remove a pin from a hole including a rotor blade pin from a rotor turbine.

Turbine pin removal

Embodiments of the present invention provide a machining tool including two spaced apart flange members adapted to be coupled with a turbine rotor while the rotor is in a first portion of a turbine casing. A carousel may be coupled to the flange members and adapted to rotate relative to the flange members, and adapted to couple with a cutting tool to complete a machining operation. Position of the cutting tool may be sensed and information on the position may be transmitted wirelessly to an operator readable display.

Machine for boring, turning, and face grooving

Growing community of inventors

Carlton, OR, United States of America

David Michael Briggs