Search

Thomas Vranas Phones & Addresses

  • Apex, NC
  • 12589 Ryegrass Loop, Parrish, FL 34219
  • 1944 Country Meadows Way, Sarasota, FL 34235 (941) 378-4195 (941) 378-8852
  • 4557 Parnell Dr, Sarasota, FL 34232
  • 2556 10Th St, Sarasota, FL 34237 (941) 365-8069
  • Newport News, VA
  • 103 Lorigan Ln, Hampton, VA 23664 (757) 851-5177

Resumes

Resumes

Thomas Vranas Photo 1

Automation Engineer

View page
Location:
2913 Sawyers Mill Dr, Apex, NC 27539
Industry:
Computer Software
Work:
Privis Health
Automation Engineer

Kobie Marketing 2017 - May 2018
Senior Qa Lead

Vertex Pharmaceuticals Nov 1997 - Aug 2016
Senior Test Designer

Mic Apr 1992 - Nov 1997
Software Developer

Chaney Computer Associates Mar 1989 - Jan 1992
It Technician
Skills:
Test Automation
C#
Silktest
Microsoft Sql Server
Database Design
Windows Server
Iis Server
Hp Quality Center
Virtualization
Tortoise Svn
Leadership
Rest
Json
Ubuntu
Hypervisor
Lamp
Ansible
Mysql
Project Management
Python
Bash Scripting
Selenium
Php
Javascript
Sql
Certifications:
Istqb Certification
Scrum Master Accredited Certification
License 22701004981063
International Scrum Institute, License 22701004981063
Thomas Vranas Photo 2

Thomas Vranas

View page
Location:
Parrish, FL
Industry:
Photography
Work:
Tlv Photo
Owner
Skills:
Photography
Photoshop
Thomas Vranas Photo 3

Thomas Vranas

View page
Thomas Vranas Photo 4

Qa Lead

View page
Location:
Parrish, FL
Work:
Kobie Marketing
Qa Lead

Publications

Us Patents

Hot Foil Transducer Skin Friction Sensor

View page
US Patent:
43171028, Feb 23, 1982
Filed:
Aug 14, 1980
Appl. No.:
6/178195
Inventors:
Thomas Vranas - Hampton VA
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
H01C 702
US Classification:
338 25
Abstract:
An improved hot wire transducer skin friction sensor 10 and 19. The device utilizes foil transducers 11 and 18 with only one edge exposed to the fluid flow. The surface 28 and 31 are polished producing a foil transducer 11 and 18 that does not generate turbulence while sufficiently thick to carry the required electrical current for high temperature fluid flow. The assembly utilized a precut layered metal sandwich 20 with attached electrodes eliminating a need for welding and individual sensor calibration.

High Temperature Strain Gage Calibration Fixture

View page
US Patent:
39569195, May 18, 1976
Filed:
Dec 19, 1974
Appl. No.:
5/534266
Inventors:
Thomas Vranas - Hampton VA
Assignee:
The United States of America as represented by the United States
National Aeronautics and Space Administration Office of General
Counsel-Code GP - Washington DC
International Classification:
G01L 2500
US Classification:
73 1B
Abstract:
An apparatus and method for calibrating high temperature strain gases which serve for both dead weight and constant deflection measurements. A cantilever support arm allows the test unit to slide into a furnace while one end is subjected to bending strain either by hanging weights upon it or by deflecting it with a push rod. The dual nature of the fixture permits both tests to be run without change of the test specimen or removal from the furnace.

Compound Wing Vertical Takeoff And Landing Small Unmanned Aircraft System

View page
US Patent:
20160272315, Sep 22, 2016
Filed:
Feb 19, 2015
Appl. No.:
14/625806
Inventors:
- Washington DC, US
Mark A. Motter - Williamsburg VA, US
Richard Deloach - Hampton VA, US
Thomas L. Vranas - Hampton VA, US
Joseph M. Prendergast - Boulder CO, US
Brittney N. Lipp - Playa Del Rey CA, US
International Classification:
B64C 39/00
B64C 29/00
B64C 39/02
B64C 39/08
B64C 27/82
B64C 5/06
Abstract:
Systems, methods, and devices are provided that enable robust operations of a small unmanned aircraft system (sUAS) using a compound wing. The various embodiments may provide a sUAS with vertical takeoff and landing capability, long endurance, and the capability to operate in adverse environmental conditions. In the various embodiments a sUAS may include a fuselage and a compound wing comprising a fixed portion coupled to the fuselage, a wing lifting portion outboard of the fixed portion comprising a rigid cross member and a controllable articulating portion configured to rotate controllable through a range of motion from a horizontal position to a vertical position, and a freely rotating wing portion outboard of the wing lifting portion and configured to rotate freely based on wind forces incident on the freely rotating wing portion.

Amazon

Searching For Super: What Every Board Should Know Before Starting The Superintendent Search Process

Searching for SUPER: What Every Board Should Know Before Starting the Superintendent Search Process

View page

Leadership matters. The most important decision any school board will ever make is selecting the district's chief executive officer, most commonly referred to as the superintendent. Over the next five years, over half of the school boards in the country will be faced with this critical decision. A r...

Author

Gary Solomon, Michelle E. Keith, Dr. Timothy G. Quinn , Thomas Vranas

Binding

Kindle Edition

Pages

68

ISBN #

1

Thomas Lee Vranas from Apex, NC, age ~54 Get Report