Roland E Wheeler

age ~65

from Green Valley, AZ

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Also known as:

Roland Erich Wheeler
Ronald E Wheeler

Phone and address:: 1750 N Rio Trinidad, Green Valley, AZ 85614
(909)4824544

Connected to:

Roland Wheeler Phones & Addresses

1750 N Rio Trinidad, Green Valley, AZ 85614 • (909)4824544
Los Angeles, CA
Claremont, CA
Fontana, CA
1815 Roanoke Rd, Claremont, CA 91711 • (909)7546362

Work

Company:

Northeast correctional center
May 2009
Position:

Cashier/clerk

Education

School / High School:

Metro Business College
1985
Specialities:

Mechanics Training

Emails

r***[email protected]

Resumes

Managing Realtor

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Location:

Los Angeles, CA

Work:

Managing Realtor

Roland Wheeler

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Roland Wheeler St. Louis, MO

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Work:

Northeast Correctional Center

May 2009 to Dec 2013
Cashier/Clerk Farmington Correctional Center

Nov 2008 to May 2009
Clerk/Utility Eastern Reception, Diagnostic Correctional Center

Oct 2005 to Nov 2005
Janitor/Utility Eastern Reception, Diagnostic Correctional Center

Oct 2004 to Oct 2005
Student Days A Week

2000 to 2000
Supervisor Manchester Marker

Nov 1995 to Nov 1996
Cashier City of St. Louis Division of Parks & Recreation

May 1994 to Oct 1995
CDL Driver City of St. Louis Division of Streets

May 1990 to Sep 1993
CDL Driver Jefferson Barracks Med.Ctr

Feb 2014 to Present
Clerk/Utility

Education:

Metro Business College
1985
Mechanics Training

Us Patents

Lightweight Fastener
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US Patent:

50392654, Aug 13, 1991
Filed:

Feb 28, 1990
Appl. No.:

7/486114
Inventors:

Jack Rath - Los Angeles CA
Roland A. Wheeler - Los Angeles CA
Assignee:

VSI Corporation - Culver City CA
International Classification:

F16B 3500
F16B 3716
B21D 5320
B21K 144
US Classification:

411366
Abstract:

An aerospace fastener comprises a blot with a roll-formed thread, and a nut with a similar thread having a uniform pitch P. The bolt has a cylindrical shank, a threaded tip and a run-out zone between the shank and tip. The thread root in the run-out follows a smooth S-shaped curve with the concave portion preferably having a radius in the range of from 2P to 2. 7P. The run-out extends from 1. 4P to 2. 3P from the maximum grip plane of the bolt, and preferably extends from 1. 6P to 2P from the maximum grip plane. The root of the thread in the run-out lies within an envelope defined by boundaries which take into account the maximum and minimum material conditions of the bolt. The nut has a run-in truncating the crest of the nut thread complementary to the run-out to clear the root of the bolt thread when the nut is assembled on the bolt in the minimum grip condition. This permits the nut to be assembled on the bolt further than in a conventional combination, and shortening of the nut and bolt by at least 1P to save weight.

Lightweight Fastener
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US Patent:

48424668, Jun 27, 1989
Filed:

Apr 1, 1986
Appl. No.:

6/846940
Inventors:

Roland A. Wheeler - Los Angeles CA
Jack Rath - Los Angeles CA
Assignee:

VSI Corporation - Culver City CA
International Classification:

F16B 3500
US Classification:

411366
Abstract:

An aerospace fastener comprises a bolt with a roll formed thread, and a nut with a similar thread having a uniform pitch P. The bolt has a cylindrical shank, a threaded tip and a run-out zone between the shank and tip. In the run-out, which is no longer than 2P, and in preferred embodiments is in the range of from 1. 6P to 1. 9P, the root of the roll formed bolt thread increases diameter continuously from the minor diameter of the tip thread to the diameter of the shank. The nut has a conical run-in truncating the crest of the nut thread parallel to the run-out to clear the root of the bolt thread when the nut is assembled on the bolt in the minimum grip condition. This permits the nut to be assembled on the bolt further than in a conventional combination, and shortening of the nut and bolt to save weight. Preferably the crest of the bolt thread is at the major diameter of the tip thread at distances beyond 0. 75P from the maximum grip plane of the bolt.

Self-Locking Fastener, Fastener System, And Process
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US Patent:

50927264, Mar 3, 1992
Filed:

Jul 21, 1989
Appl. No.:

7/384132
Inventors:

Roland A. Wheeler - Los Angeles CA
Peter M. Downie - Los Angeles CA
Assignee:

VSI Corporation - Chantilly VA
International Classification:

F16B 3922
US Classification:

411277
Abstract:

Wrenching lobes of an internally threaded nut are separated by circumferential, tapered walls so that the lobes and contiguous portions of the walls deform in radial compression upon reaching a predetermined preload and displace radially inwardly while the central portions of the walls deform radially outwardly, but do not interfere with the tool that sets the nut.

Lightweight Fastener
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US Patent:

49155598, Apr 10, 1990
Filed:

May 29, 1987
Appl. No.:

7/056456
Inventors:

Roland A. Wheeler - Los Angeles CA
Jack Rath - Los Angeles CA
Assignee:

VSI Corporation - Culver City CA
International Classification:

F16B 3500
F16B 3716
B21D 5320
B21K 144
US Classification:

411366
Abstract:

An aerospace fastener comprises a bolt with a roll-formed thread, and a nut with a similar thread having a uniform pitch P. The bolt has a cylindrical shank, a threaded tip and a run-out zone between the shank and tip. The thread root in the run-out follows a concave curve having a radius in the range of from 2. 0P to 2. 7P and extends 1. 58P to 1. 8P from the maximum grip plane of the bolt. The nut has a convexly curved run-in truncating the crest of the nut thread complementary to the run-out to clear the root of the bolt thread when the nut is assembled on the bolt in the minimum grip condition. This permits the nut to be assembled on the bolt further than in a conventional combination, and shortening of the nut and bolt by at least 1P to save weight.