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Glenn Grosso Phones & Addresses

  • 2249 Dugan Rd, Olean, NY 14760 (716) 378-6427
  • 2449 Dugan Rd, Olean, NY 14760
  • Knapp Creek, NY
  • 2249 Dugan Rd, Olean, NY 14760

Work

Position: Professional/Technical

Education

Degree: Associate degree or higher

Emails

Resumes

Resumes

Glenn Grosso Photo 1

Manager

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Location:
2249 Dugan Rd, Olean, NY 14760
Industry:
Machinery
Work:
Dresser-Rand
Manager - Centrifugal Products Technical Support and Dresser-Rand Engineering Fellow

Ingersoll Rand Jun 1978 - Jun 1987
Project and Product Design Engineer

Jun 1978 - Jun 1987
Manager
Education:
Rutgers University 1974 - 1978
Bachelor of Science In Mechanical Engineering, Bachelors, Mechanical Engineering
Skills:
Air Compressors
Engineering
Turbomachinery
Centrifugal Compressors
Gas Turbines
Mechanical Engineering
Rotating Equipment
Project Engineering
Turbines
Steam Turbines
Pumps
Continuous Improvement
Engineering Design
Product Design
Finite Element Analysis
Power Generation
Rotordynamics
Engineering Management
Machining
Bearings
Design Engineering
Valves
Seals
Root Cause Analysis
Cfd
Ansys
Stress Analysis
Asme
Oil/Gas
Unigraphics
Heat Transfer
Thermodynamics
Design For Manufacturing
Pro Engineer
Reliability Engineering
Hydraulics
Fluid Mechanics
Maintenance Management
Heat Exchangers
Fluid Dynamics
Glenn Grosso Photo 2

Glenn Grosso

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Publications

Us Patents

Dry Gas Blow Down Seal

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US Patent:
20100254811, Oct 7, 2010
Filed:
Apr 6, 2009
Appl. No.:
12/419086
Inventors:
Mark Joseph Kuzdzal - Allegany NY, US
Harry Francis Miller - Allegany NY, US
Glenn R. Grosso - Olean NY, US
Martin D. Maier - Allegany NY, US
David J. Peer - Olean NY, US
Assignee:
Dresser-Rand Co. - Olean NY
International Classification:
F01D 11/04
F16J 15/447
US Classification:
415230, 277303
Abstract:
A sealing assembly configured to seal a rotating shaft of a turbo machine having a high pressure process gas, comprising a housing defining a bore configured to receive the rotating shaft and sealing assembly, wherein the housing is mounted to a casing of the turbo machine; a first sealing stage comprising a single dry gas seal and configured to blow down the high pressure process gas to a lower pressure; a labyrinth seal mounted longitudinally outward from the first sealing stage; and a second sealing stage mounted longitudinally outward from the labyrinth seal, wherein the second sealing stage comprises a tandem dry gas seal having a primary dry gas seal and a secondary dry gas seal axially spaced with an intermediate labyrinth seal.

Reduced Leakage Balance Piston Seal

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US Patent:
20130149101, Jun 13, 2013
Filed:
Nov 13, 2012
Appl. No.:
13/675368
Inventors:
Mark J. Kuzdzal - Allegany NY, US
Glenn R. Grosso - Olean NY, US
David J. Peer - Olean NY, US
Assignee:
DRESSER-RAND COMPANY - Olean NY
International Classification:
F01D 3/04
US Classification:
415 1, 415107
Abstract:
Balance piston assembly, apparatus, and methods are provided. The assembly includes a balance piston coupled to a rotatable shaft and configured to rotate therewith, the balance piston including a first shelf and a second shelf, the first and second shelves being axially-overlapping and radially-offset. The assembly also includes a seal including a first sealing surface configured to seal with the first shelf and a second sealing surface configured to seal with the second shelf.

Thermal Barrier Coating For Bearing Journal Surfaces Of Rotary Shafts

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US Patent:
20150043848, Feb 12, 2015
Filed:
Jun 26, 2014
Appl. No.:
14/315674
Inventors:
Glenn R. Grosso - Olean NY, US
Assignee:
DRESSER-RAND COMPANY - Olean NY
International Classification:
F16C 33/10
F16C 33/02
F16C 37/00
F16C 17/02
US Classification:
384316, 384317
Abstract:
A rotary shaft and method for reducing non-uniform heating thereof are provided. The rotary shaft may include a tubular body having a longitudinal axis extending therethrough. An outer surface of the tubular body may define a groove at least partially extending radially inward from the outer radial surface toward the longitudinal axis of the tubular body to define a depth thereof. The rotary shaft may include a thermal barrier at least partially disposed in the groove and configured to absorb at least a portion of heat generated from rotation thereof.

Interlocking Hole Pattern Seal

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US Patent:
20140191475, Jul 10, 2014
Filed:
Mar 23, 2012
Appl. No.:
14/005592
Inventors:
Manoj K. Gupta - Houston TX, US
Steven Nove - Houston TX, US
Thomas Soulas - Houston TX, US
Krishnaswamy Ramesh - Katy TX, US
Glenn Grosso - Olean NY, US
Assignee:
DRESSER-RAND COMPANY - Olean NY
International Classification:
F01D 11/02
US Classification:
277301, 277411
Abstract:
A seal for a turbomachine is disclosed. The seal assembly includes a rotatable shaft having a stepped outer circumferential surface that defines one or more annular protrusions axially-spaced thereon. A seal is radially-offset dially-offset from the rotatable shaft and has one or more annular recesses that extend radially-outward from the inner circumferential surface of the seal. A plurality of holes are defined in both the inner circumferential surface and the one or more annular recesses of the seal, the one or more annular recesses being axially-spaced from each other and configured to receive the one or more annular protrusions in an interlocking fit.
Glenn R Grosso from Olean, NY, age ~68 Get Report