Search

Ronald Schlechtweg Phones & Addresses

  • Marco Island, FL
  • 6676 Quailrun Ct, Loveland, OH 45140 (513) 677-1383
  • 6676 Quailrun Ct, Loveland, OH 45140 (513) 405-3842

Work

Position: Sales Occupations

Emails

Public records

Vehicle Records

Ronald Schlechtweg

View page
Address:
6676 Quailrun Ct, Loveland, OH 45140
Phone:
(513) 677-1383
VIN:
JM1BK32F971722044
Make:
MAZDA
Model:
MAZDA3
Year:
2007

Publications

Us Patents

Boltless Rotor Blade Retainer

View page
US Patent:
48909815, Jan 2, 1990
Filed:
Dec 30, 1988
Appl. No.:
7/292084
Inventors:
Robert J. Corsmeier - Cincinnati OH
Ronald E. Schlechtweg - Loveland OH
Richard W. Albrecht - Fairfield OH
Dennis P. Dry - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 532
US Classification:
416220R
Abstract:
A boltless blade retainer for preventing forward axial movement of the rotor blades in a turbo machine relative to the rotor disk comprises an annular extension or hook formed on each dovetail post on the web of the rotor disk, an impeller or blade retainer formed with a flange which is carried against the web and dovetail posts and a retaining ring interposed between the hooks of the dovetail posts and the flange of the impeller. The retaining ring secures the impeller in a fixed axial position relative to the dovetail posts and rotor disk, and is positioned to engage the rotor blades carried in the axial slots between adjacent dovetail posts to prevent their movement in a forward axial direction.

Boltless Turbine Nozzle/Stationary Seal Mounting

View page
US Patent:
52115364, May 18, 1993
Filed:
May 13, 1991
Appl. No.:
7/699060
Inventors:
Robert I. Ackerman - Mason OH
Alan Walker - Wyoming OH
Ronald E. Schlechtweg - Loveland OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 2508
US Classification:
415177
Abstract:
The invention comprises the use of a split retaining ring cooperating with an inner nozzle support member to retain nozzle segments and a stationary seal without the use of threaded fasteners. Elimination of bolt heads from the rotor/stator cavity reduces windage losses and enables a shortening of the inner nozzle band overhang, reducing the requirement for high pressure cooling and cavity purge air.

High Pressure Turbine Rotor Two-Piece Blade Retainer

View page
US Patent:
44809581, Nov 6, 1984
Filed:
Feb 9, 1983
Appl. No.:
6/465213
Inventors:
Ronald E. Schlechtweg - Fairfield OH
Assignee:
The United States of America as represented by the Secretary of the Air
Force - Washington DC
International Classification:
F01D 532
US Classification:
416220R
Abstract:
A blade retainer for holding a turbine blade on a turbine rotor disc and sealing a cooling cavity formed between the disc and blade has a two-piece construction. The first piece performs the blade loading function, while the second piece performs the cavity sealing function. The two pieces are attached to the disc by a common set of fasteners, such as bolts.
Ronald E Schlechtweg from Marco Island, FL Get Report