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Larry L Anspach, 5517870 Clover Rd, Morrison, IL 61270

Larry Anspach Phones & Addresses

Morrison, IL   

Rock Falls, IL   

117 Birch St, Prophetstown, IL 61277    815-4410600   

1711 Woodcrest St NE, Cedar Rapids, IA 52402    319-3783910   

Rockwell, IA   

Mason City, IA   

Leland, IA   

Hampton, IA   

Independence, IA   

231 Crandall Dr NE, Cedar Rapids, IA 52402    319-2301562   

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Larry L Anspach

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Work

Company: Scotts company - Morrison, IL Feb 2014 Position: Forklift operator

Education

School / High School: Rock Falls High School- Rock Falls, IL 1988 Specialities: General studies

Mentions for Larry L Anspach

Larry Anspach resumes & CV records

Resumes

Larry Anspach Photo 11

Larry Anspach

Larry Anspach Photo 12

Larry Anspach - Rock Falls, IL

Work:
Scotts Company - Morrison, IL Feb 2014 to May 2014
Forklift Operator
Ryder Intregrated Logistics - Rochelle, IL Dec 2011 to Oct 2013
Hi- Reach Forklift operator
The Staffing Agency - Rochelle, IL Aug 2011 to Nov 2011
laborer
Grummerts Hardware and Rental - Rock Falls, IL May 2009 to Jun 2010
sales/rental department
Prinsco Incorporated - Jesup, IA Jan 2008 to Jul 2008
4x4 diesel forklift operator
Winnebago Industries - Forest City, IA Sep 2006 to Jul 2007
RV line worker
Education:
Rock Falls High School - Rock Falls, IL 1988
General studies

Publications & IP owners

Us Patents

Limiting Aircraft Vertical Acceleration Response

US Patent:
4787042, Nov 22, 1988
Filed:
Nov 18, 1985
Appl. No.:
6/799222
Inventors:
Roger D. Burns - Cedar Rapids IA
Larry A. Anspach - Cedar Rapids IA
Assignee:
Rockwell International Corporation - El Segundo CA
International Classification:
G05D 106
US Classification:
364433
Abstract:
The presently-disclosed invention utilizes sensed pitched rate and sensed vertical acceleration to prevent aberrant pitch rate command outputs as a function of lead compensated sensed acceleration, controlling the vertical acceleration by sensing when a maximum is approached. When the lead compensated acceleration exceeds a first predetermined acceleration factor, the presently-sensed pitch rate replaces the pre-programmed maximum pitch rate factor as the temporary maximum rate, to temporarily prevent additional vertical acceleration due to increasing pitch rate. This apparatus requires no airspeed input and does not interfere with flight performance characteristics during normal flight operations, allowing higher torque servos to be used, and thus improves overall performance.

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