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Narinder Attri Phones & Addresses

  • 3004 Crooked Stick Dr, Plano, TX 75093 (972) 306-2410 (972) 307-2216
  • 3820 Belton Dr, Dallas, TX 75287 (972) 307-0924
  • Renton, WA
  • Auburn, WA

Work

Company: Boeing Position: Retired executive

Education

Degree: Bachelors, Masters, Master of Science In Mechanical Engineering, Bachelor of Science In Mechanical Engineering, Bachelor of Science Specialities: Mathematics, Physics

Skills

Airlines • Aviation

Industries

Airlines/Aviation

Resumes

Resumes

Narinder Attri Photo 1

Narinder Attri

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Location:
Dallas, TX
Industry:
Airlines/Aviation
Work:
Boeing
Retired Executive
Skills:
Airlines
Aviation

Business Records

Name / Title
Company / Classification
Phones & Addresses
Narinder Attri
Treasurer , Director , Secretary
HILLS OF PRESTONWOOD SOUTH HOMEOWNERS ASSOCIATION
Membership Organization
17130 Dallas Pkwy STE 220, Dallas, TX 75248
7548 Preston Rd, Frisco, TX 75034
8360 Lyndon B Johnson Fwy, Dallas, TX 75243
Narinder Attri
Treasurer , Director , Secretary
HILLS OF PRESTONWOOD MASTER HOMEOWNERS ASSOCIATION
Membership Organization
17130 Dallas Pkwy STE 220, Dallas, TX 75248
7548 Preston Rd, Frisco, TX 75034
8360 Lyndon B Johnson Fwy, Dallas, TX 75243

Publications

Us Patents

Limited-Slip Brake Control System

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US Patent:
40788458, Mar 14, 1978
Filed:
Aug 13, 1976
Appl. No.:
5/714425
Inventors:
Robert Leo Amberg - Seattle WA
Narinder Singh Attri - Renton WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B60T 810
US Classification:
303107
Abstract:
A brake control system which limits the operation of the braking forces applied to the tires, to the non-slip portion of the tire brake force and wheel velocity characteristic curve, i. e. , the front or positive slope side of the characteristic Mu/slip curve; and thereby, minimizes both tire and brake wear. In particular, two embodiments of the invention are disclosed. All of which contain three aspects: a basic deceleration control circuit; a large deviation control circuit; and an energy balance system. The basic deceleration control circuit produces an average deceleration by summing the decelerations from all of the wheels, through a filtered differentiation of the wheel speed, and dividing it by the number of wheels. The average deceleration is then compared to the pilot selected deceleration rate for Dry, Wet, or Icy conditions and an error signal is generated. This error signal is then applied to a hysteresis circuit which outputs a constant level positive or negative signal.
Narinder Singh Attri from Plano, TX, age ~92 Get Report