General Electric Company

Anthony Salvatore Arrao

Richard Nils Dawson

Anthony James George

Evgeny Victorovich Kazmin

Dmitry Yurevich Semenov

Timothy Gerald Schmehl

Yury Danilovich Vinitsky

Daniel White Sexton

Harold Woodruff Tomlinson, Jr

James Jun Xu

Anand Shankar Tanavde

Matthew Robert Martin

Andrew J Travaly

Jayan Kaadaapuram George

Michael Brynn House

Daniel James Fitzmorris

Michael Christopher Villani

Mikhail Avramovich Avanesov

John G Nourse

David R Abbott

Jason Rueda

Yury Danilovich Vinitzky

Karina Elizabeth Padilla

Thomas C Barnes

Dmitry Salvatore Semenov

A generator connection ring support device includes a base, a first protruding member extending from the base, a second protruding member extending from the base substantially parallel to the first protruding member, a fastener hole extending through the base and the first protruding member, and a clamping hole extending through the base into the first slot. The clamping hole is configured to at least partly house a clamping element. The first and second protruding members define a first slot therebetween to receive a connection ring, each protruding member having a first end proximate the base and a second end distal the base, the first protruding member configured to be fastened to an end winding axial support at the distal end of the first protruding member, the first protruding member having a longitudinal axis, the fastener hole aligned with the longitudinal axis of the first protruding member.

Generator connection ring support device

A seal ring assembly includes a first seal ring axially disposed from a second seal ring. The first seal ring has an axial face opposing an axial face of the second seal ring. A radial oil channel is defined between the two axial faces. Both seal rings have a tapered surface configured to contact a spring. The spring biases the seal rings away from each other via the tapered surface. Both seal rings are disposed in a radially inwardly directed channel. At least one of the seal rings have a plurality of protrusions that extend beyond the axial face. The protrusions are configured to create a passageway to allow oil to flow through the passageway and to allow at least one of the seal rings to move into a desired position by reducing static friction between the axial faces.

Seal ring for hydrogen cooled generator

A compression seal bracket for sealing a thermally moveable end of a generator cooler is disclosed. The bracket may include a unitary body including a first portion at an angle to a second portion with an integral curvilinear portion therebetween. Each portion may have: a seal ring engaging member for engaging the seal ring to compress the seal against the seal seat, a shim member configured to be coupled to the seal seat between the seal ring engaging member and the seal seat, the shim member having a predetermined thickness. The seal ring engaging member and the shim member may include a plurality of corresponding fastener openings, each opening for receiving a fastener for coupling to the seal seat. A related bracket system is also disclosed.

Compression seal bracket and system for generator cooler

A ripple spring includes a body including a central portion having a substantially sinusoidal shaped surface and a substantially planar end portion extending from each end of the central portion. A stator bar may include an armor layer including a novalac epoxy resin impregnated glass composite.

Planar-ended ripple spring and hardened stator bar armor

A laminated rotor and an electric machine including the laminated rotor are disclosed. In an embodiment, a rotor comprises a plurality of stacked laminations, wherein each lamination includes a plurality of radially extending slots arranged about a circumference of each of the plurality of laminations, and the plurality of radially extending slots in successive laminations in the stack are aligned. A stud member passes longitudinally through at least one hole in the lamination stack, and a plurality of coils are positioned within the plurality of slots. Fewer than all of the plurality of slots have a coil positioned therein, leaving at least three slots empty. Balance members may be placed in the slots that do not have a coil positioned therein to balance the rotor.

Laminated rotor balancing provisions

A laminated rotor for an electric machine is disclosed. In an embodiment, the rotor comprises a plurality of stacked laminations. Each lamination includes a plurality of radially extending slots arranged about a circumference thereof, and a first chamfer on a surface of each of the slots, wherein the surface mates with a wedge. The first chamfer connects the surface and a first face of the lamination. A stud member passes longitudinally through a hole in the lamination stack, a first end flange member on a first end of the lamination stack, and a second end flange member on a second end of the lamination stack. A first fastener is affixed to a first end of each of the at least one stud member; and a second fastener affixed to a second end of each of the at least one stud member.

Laminated rotor machining enhancement

A system and method for establishing communications in a power plant comprises a power generation system having an interface for establishing wireless communication, at least one power plant auxiliary system having an interface for enabling wireless communication, and a wireless communications link, having at least two redundant wireless communications channels, established between the power generation system and the power plant auxiliary system. The two redundant wireless communications channels may be two redundant wireless radio frequency channels. The communications link may be established utilizing a network communications controller which wirelessly communicates with the power generation system and the power plant auxiliary system. One or more of the power plant auxiliary systems may communicate with the network communications controller through a repeater.

Radio frequency communications network for power plant control systems

A blade-to-blade vibration damper for a turbine rotor blade is disclosed. Each blade has airfoil, platform and root portions. A plurality of blades are circumferentially spaced about a rotor disk. An inclined recess extends into the platform portion of each blade from a first surface thereof, and toward its root portion. A U-shaped wire-form damping member has its in-turned marginal end portions slidably received in each recess. When the rotor disk is rotated at a sufficient angular speed, the damping members move outwardly by the centrifugal force acting thereon to engage the opposing surface of the platform portion of the adjacent blade. When so engaged, the members damp vibrations of such blades and seal the space between the opposing platform surfaces.

Blade-to-blade vibration damper

A retainer ring clamps, for example, a turbine cooling plate to a rotatable turbine disc. The retainer ring has a wedge-shaped channel that engages annular flanges on the cooling plate and the disc. The wedge-shaped channel converts radial forces on the ring to axial clamping forces which secure the cooling plate to the disc. Special tooling is not required to assemble the retainer ring to the cooling plate and turbine disc, and preloading of the cooling plate against the disc is not necessary. An angled or slanted gap in the ring eases assembly and disassembly of the retainer ring onto the annular flanges of the cooling plate and turbine disc and ensures that axial and radial movement of the retainer ring is required for disassembly of the ring from the flanges.

Growing community of inventors

Clifton Park, NY, United States of America

Anthony Salvatore Arrao