Honeywell International Inc.

Dave Elpern

Frank Lin

Robert P Chen

Sam Shiao

Terry L Morris

Fidel M Joco

Stephen Vaccarezza

Alvin Powell

Bob Dietrich

A method is provided for repairing a turbine nozzle assembly with an insert and a support structure. The method includes positioning the insert on the support structure of the turbine nozzle assembly; and plug welding the insert to the support structure of the turbine nozzle assembly.

Turbine nozzle assemblies and methods for repairing turbine nozzle assemblies

A permanent magnet rotor for an electric motor may include a rotor assembly that will hold the magnets in place. A pair of rings is added to the sleeve to tightly engage and press against the end plates and the magnets. This configuration provides additional securement against axial and radially shifting of the magnets.

Sleeve in end rings for permanent magnet rotor

A centrifugal compressor is modified by forming a bypass between the leading edge of the compressor diffuser and a point downstream from the throat of the diffuser. The bypass may be unidirectional or bi-directional. In a bi-directional embodiment, an operable flow range of the compressor can be widened in both directions of a compressor map, i.e., extending both the surge and choke margins of a compressor at the expense of normal operating efficiencies. In a unidirectional bypass embodiment the flow range may be increased only in one direction, but there is no diminishment of efficiency of the compressor at normal operating conditions. The modification provides a simple expedient for increasing flow range without a need to redesign a compressor.

Wide flow compressor with diffuser bypass

Growing community of inventors

Los Angeles, CA, United States of America

Dave Elpern