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Terry W Stratton

from Wichita, KS
Age ~59

Terry Stratton Phones & Addresses

  • 2423 High Point Cir, Wichita, KS 67205 (316) 729-9026
  • 2619 Glacier Ct, Wichita, KS 67215 (316) 729-9338
  • Maize, KS
  • 1009 Park Rd, Rose Hill, KS 67133 (316) 776-2420
  • Valley Center, KS

Work

Company: El cattle company lake Address: 12221 E Central Ave, Wichita, KS 67206 Phones: (316) 687-2220 Position: Manager Industries: Eating Places

Professional Records

Lawyers & Attorneys

Terry Stratton Photo 1

Terry Stratton - Lawyer

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Office:
Katz Nowinski P.C.
Specialties:
Elder Law & Advocacy
Real Estate
Tax
Estate Planning
Wills
Trusts
Probate
Decedent's Estate Administration
Conservatorships/Guardianships
Employee Benefits
Qualified Pension and Profit Sharing Plans
Corporations/Guardianships
Non-Profits and 501 (c) (3)'s
Business Law
Corporations
LLC's
ISLN:
903364940
Admitted:
1980
University:
Northern Arizona University, M.A., 1977; University of Iowa, B.S., 1974
Law School:
Pepperdine University School of Law, J.D., 1980
Terry Stratton Photo 2

Terry Stratton - Lawyer

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ISLN:
1000333618
Admitted:
2015
University:
Georgetown University Law Center

Business Records

Name / Title
Company / Classification
Phones & Addresses
Terry Stratton
Manager
El Cattle Company Lake
Eating Places
12221 E Central Ave, Wichita, KS 67206
Terry Stratton
Manager
El Cattle Company Lake
Eating Places
12221 E Central Ave, Wichita, KS 67206

Publications

Us Patents

Engine Nacelle Acoustic Panel With Integral Wedge Fairings And An Integral Forward Ring

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US Patent:
61738077, Jan 16, 2001
Filed:
Apr 13, 1998
Appl. No.:
9/059797
Inventors:
John M. Welch - Wichita KS
Thomas D. Popp - Wichita KS
Robert F. Wikstrom - Derby KS
Terry W. Stratton - Rose Hill KS
Brian R. Kitt - Wichita KS
Assignee:
The Boeing Company - Seattle WA
International Classification:
F02K 100
US Classification:
181213
Abstract:
An acoustic panel (26) for the nacelle (20) of a high bypass jet engine. The acoustic panel (26) has a perforated composite inner sheet (54), an outer composite sheet (96, 98), and a honeycomb-core material (74) sandwiched therebetween. The acoustic panel (26) includes an integral forward ring (36) and integral wedge fairings (44).

Reinforcing Structure For Engine Nacelle Acoustic Panel

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US Patent:
59752378, Nov 2, 1999
Filed:
Feb 19, 1998
Appl. No.:
9/026189
Inventors:
John M. Welch - Wichita KS
Thomas D. Popp - Wichita KS
Robert F. Wikstrom - Derby KS
Terry W. Stratton - Rose Hill KS
Brian R. Kitt - Wichita KS
Assignee:
The Boeing Company - Seattle WA
International Classification:
E04B 182
US Classification:
181290
Abstract:
An improved acoustic panel (26) for the nacelle (20) of a high bypass jet engine. The acoustic panel (26) has a perforated composite inner sheet (54), an outer composite sheet (96, 98), and a new reinforcement structure, or pre-cured doubler (62) therein. The pre-cured doubler (62) is arranged to receive a load applied to the acoustic panel (26), and includes a face sheet (64) connected to a structural attachment area (52) of the perforated composite inner sheet (54). A structurally-reinforced core (63) is connected the face sheet (64). Preferably, the width of the face sheet (64) in an air flow direction of the acoustic panel (26) is substantially equal to the width of the structurally reinforced core (63) in the air flow direction. The pre-cured doubler (62) provides increase acoustic area in parts of the acoustic panel adjacent to attachment fittings (46). Expanded epoxy (87a) is also used to reinforce side edges and selected areas of the acoustic core (60) for the acoustic panel (26).
Terry W Stratton from Wichita, KS, age ~59 Get Report