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Adrian Flavia Viisoreanu

from Federal Way, WA
Age ~70
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Also known as:
Adrian F Viisoreanu
Phone and address:
30323 17Th Ave SW, Auburn, WA 98023
Related to:
Flavia Viisoreanu, 70Delia Viisoreanu, 46
Connected to:
Douglas U Viita, 65Abhishek Vij, 39Chhavi Vij, 38Deepak R Vij, 53Deepali Vij, 49Jagdish C Vij, 80Jagmohan L Vij, 55Manish Vij, 51Naresh Vij, 61Pankaj Vij, 49

Adrian Viisoreanu Phones & Addresses

  • 30323 17Th Ave SW, Federal Way, WA 98023
  • 1618 Carolyn St, Derby, KS 67037 (316) 789-8937
  • 330 43Rd St, Renton, WA 98055
  • Kent, WA
  • Aiken, SC
  • Wichita, KS
  • Kiona, WA
  • Falls Church, VA

Work

Position: Federal way, washington

Resumes

Resumes

Adrian Viisoreanu Photo 1

Federal Way, Washington

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Location:
Federal Way, WA
Work:

Federal Way, Washington

Publications

Us Patents

Composite Aircraft Structures With Hat Stiffeners

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US Patent:
7871040, Jan 18, 2011
Filed:
Nov 10, 2006
Appl. No.:
11/558735
Inventors:
Shin S. Lee - Bellevue WA, US
Adrian Viisoreanu - Kent WA, US
William J. Koch - Bellevue WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 1/12
US Classification:
244119
Abstract:
A composite panel structure for an aircraft includes a plurality of annular, hat-shaped frames disposed coaxially along a long axis of the aircraft in a spaced, parallel relationship, an inner skin having an inner surface bonded to an outer surface of the hat frames, a plurality of elongated, hat-shaped stringers disposed in a longitudinal direction along an outer surface of the inner skin in a spaced, parallel relationship, a solid or rigid foam offset bonded to an outer surface of each of the stringers, and an outer skin having an inner surface bonded to an upper surface of each of the offsets. The inner skin carries the loads of the structure and the outer skin defines an aerodynamic surface of the aircraft and provides impact and lighting protection. The frames, inner skin and stringers are formed on a single forming tool and cured and bonded with each other simultaneously.

Long Endurance Hydrogen Powered Vehicle

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US Patent:
20080006743, Jan 10, 2008
Filed:
Jul 5, 2006
Appl. No.:
11/428706
Inventors:
Gerald D. Miller - Mercer Island WA, US
Wesley Moore - Seattle WA, US
Adrian Viisoreanu - Kent WA, US
Russell W. Morris - Redmond WA, US
Ronald W. Davidson - St. Paul MO, US
Shailesh Atreya - Irving CA, US
Albert D. Olsen - Huntington Beach CA, US
William Bigbee-Hansen - Renton WA, US
International Classification:
B64D 33/00
US Classification:
244 53 R
Abstract:
Hydrogen powered air vehicles that in some embodiments can fly with very long endurance (10 or more days) at altitudes over 60,000 ft carrying payloads of up to 2,000 pounds. Embodiments may include features such as large wingspan relative to fuselage and an all composite or partial composite structure for light weight and strength. The aircraft of the invention use one or more internal combustion engines adapted for hydrogen combustion, each engine driving propellers. The hydrogen fuel is stored on board in containers, located within the fuselage, as a cryogenic liquid, and is vaporized in a heat exchanger before delivery to the internal combustion engine.

Flight Vehicle Fairing Having Vibration-Damping Blankets

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US Patent:
20120325966, Dec 27, 2012
Filed:
Jun 27, 2011
Appl. No.:
13/169295
Inventors:
Justin Christenson - Mountlake Terrace WA, US
Herbert L. Hoffman - Seattle WA, US
Gary R. Chewning - Woodinville WA, US
Alan Edgar Landmann - Woodinville WA, US
Adrian Viisoreanu - Kent WA, US
Hugh Poling - Seattle WA, US
Balamurugan R. Annamalai - Snohomish WA, US
Justin D. Kearns - Seattle WA, US
Jason Alexander Gordon - Long Beach CA, US
Assignee:
THE BOEING COMPANY - Irvine CA
International Classification:
B64C 1/00
B23P 11/00
B23P 6/00
US Classification:
2441291, 2940204, 29428
Abstract:
Vibration-damping blankets are attached to the back surfaces of fairing panels of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne transmitted energy, and cabin noise. In one case, the flight vehicle fairing has an exterior comprising exterior surfaces of a multiplicity of removable panels. A method of retrofitting the flight vehicle with vibration-damping blankets comprises: removing a panel from the flight vehicle exterior; attaching a vibration-damping blanket to a back surface of the removed panel; and installing the panel with attached vibration-damping blanket on the flight vehicle with the exterior surface of the panel forming part of the flight vehicle exterior. In one embodiment, the vibration-damping blanket comprises polymeric (e.g., aromatic polyamide) fibers in a nonwoven structure.

Structurally Integrated Antenna Aperture Electronics Attachment Design And Methodology

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US Patent:
20140320366, Oct 30, 2014
Filed:
Jan 13, 2014
Appl. No.:
14/154139
Inventors:
- Chicago IL, US
Joseph A. Marshall - Kent WA, US
Douglas A. McCarville - Orting WA, US
Otis F. Layton - Bonney Lake WA, US
Adrian Viisoreanu - Kent WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
H01Q 1/12
H01Q 9/16
US Classification:
343793, 29601, 343906
Abstract:
A method of manufacture of antenna electronics attachment is disclosed. A nutplate is coupled to a mounting plate via a plurality of embedded fastening structures such that mechanical-electronic coupling means allow in-service change-out of an electronic component coupled to the nutplate.
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Adrian Flavia Viisoreanu from Federal Way, WA, age ~70 Get Report