Professional Records
License Records
Nathan Alphonse Secinaro
Address:
W9321 H Lucas Dr, Iron Mountain, MI 49801
License #:
A5197963
Category:
Airmen
Nathan Secinaro Phones & Addresses
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Bothell, WA
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Seattle, WA
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W9321 H Lucas Dr, Iron Mountain, MI 49801
Resumes
Resumes
Nathan Secinaro
View pageLocation:
1105 Spring St, Seattle, WA 98104
Industry:
Aviation & Aerospace
Work:
Detroit Aircraft May 2014 - Aug 2014
Engineering Intern
University of Michigan Jun 2010 - Aug 2013
Tour Guide
Engineering Intern
University of Michigan Jun 2010 - Aug 2013
Tour Guide
Education:
University of Michigan 2012 - 2016
Bachelors, Bachelor of Science, Aerospace Engineering Iron Mountain High School 2012
Bachelors, Bachelor of Science, Aerospace Engineering Iron Mountain High School 2012
Skills:
Solidworks
Matlab
Microsoft Office
Private Piloting
Technical Writing
Xfoil
Research
Mathematica
C++
Statistics
Matlab
Microsoft Office
Private Piloting
Technical Writing
Xfoil
Research
Mathematica
C++
Statistics
Nathan Secinaro
View pagePublications
Us Patents
Vortex Generator Passive Deployment System
View pageUS Patent:
20210061449, Mar 4, 2021
Filed:
Aug 30, 2019
Appl. No.:
16/557987
Inventors:
- Chicago IL, US
Nathan Alphonse Secinaro - Seattle WA, US
Nathan Alphonse Secinaro - Seattle WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 23/06
Abstract:
A system for passive deployment of a vortex generator is disclosed, including a housing mounted at a fixed location relative to an airfoil structure and a piston contained in the housing. A vortex generator is moveably mounted adjacent an exterior surface of the airfoil structure, and is moveable between a stowed position inside the airfoil structure and a deployed position outside the airfoil structure. The piston is configured to drive the vortex generator between the stowed position and the deployed position in response to a pressure differential between a first airstream over a first surface of the airfoil structure and a second airstream over a second surface of the airfoil structure.