Integral composite nozzle-shield assembly for a gas-cooled dynamoelectric machine

• US 4,208,599 A
• Filed: 06/07/1978
• Issued: 06/17/1980
• Est. Priority Date: 06/07/1978
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Armor, Anthony F., Archibald, James B., Darby, William L., Landrio, Frank R.
• Primary Examiner(s): Skudy, R.
• Application Number:
  US05/913,486
• Time in Patent Office: 741 Days
• Field of Search: 310/64, 310/55, 310/58, 310/61, 310/59, 310/57, 310/65, 310/53, 310/162, 310/63, 310/52
• US Class Current: 310/64
• CPC Class Codes: H02K 9/10 by gaseous cooling medium flowing in closed circuit, a part of which is external to the machine casing

Abstract

An integral nozzle-shield assembly for a gas-cooled dynamoelectric machine such as a large turbine-driven generator is described. The nozzle-shield assembly is formed of a non-conductive, non-magnetic material such as molded fiberglass and resin and serves to channel hydrogen gas between a heat exchanger and a rotor-mounted fan used to pump the gas through coolant passages in the dynamoelectric machine, and the assembly also provides a labyrinth seal over the fan blade tips. In one embodiment, the nozzle-shield assembly includes two 180-degree halves whose thickness varies circumferentially and which may be installed in a generator by bolting their outer edges to a stator frame member of the generator and bolting the halves together at the two radial joints between halves using flat metal plate connectors. Use of a material such as fiberglass and resin to form an integral nozzle-shield assembly results in a structure which is not susceptible to eddy current losses or damage due to arcing, and this integral assembly is readily fabricated and easy to install in a dynamoelectric machine.

Claims

1. In combination with a dynamoelectric machine having a stator including a stator core, a rotor disposed within said core and defining a gas gap with said core, a gas cooler, and a fan having a plurality of blades attached to said rotor for circulating coolant gas through said dynamoelectric machine, the improvement comprising an integral composite nozzle-shield assembly for guiding the flow of coolant gas between said cooler and said fan, said nozzle-shield assembly including:

a pair of 180-degree arcuate sections of non-electrically conductive non-magnetic material;

means for connecting the outer edge portion of each of said sections to said stator;

means for interconnecting said 180-degree arcuate sections along radial joints;

a rub strip within an annular recess in an inner edge portion of each of said arcuate sections and having a serrated surface, said serrated surface adapted to provide, when said arcuate sections are mounted in close proximity to said fan blades, a labyrinth seal to minimize leakage of coolant gas between said rub strip and said fan blades.

2. The combination according to claim 1 wherein said means for interconnecting said 180-degree sections comprises a flat metal plate and a plurality of bolts.

3. The combination according to claim 2 wherein the thickness of each of said 180-degree sections decreases from a maximum value near said radial joints, to a minimum value at a circumferential location between 60 and 90 degrees from said joints.

4. The combination according to claim 3 wherein said arcuate sections are fabricated from a resin plus a fibrous material selected from the group consisting of fiberglass, carbon fibers, and boron fibers.

5. The combination according to claim 4 wherein said rub strip is of trapezoidal cross section with first and second nonparallel sides adjacent to said serrated surface, said first nonparallel side oriented at an obtuse angle with respect to said serrated surface to facilitate permanent retention of said strip in said arcuate sections.

6. The combination according to claim 5 wherein said second nonparallel side of said rub strip includes dowels for permanently retaining said rub strip in said arcuate sections.