ROBIN LANE YOUNG
Pilots at Conrey St, Wichita, KS

License number
Kansas A4304301
Issued Date
Feb 2013
Expiration Date
Feb 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
8312 W Conrey St, Wichita, KS 67205

Professional information

Robin Young Photo 1

Liquid Based Ice Protection Test Systems And Methods

US Patent:
8506160, Aug 13, 2013
Filed:
Sep 1, 2009
Appl. No.:
12/552122
Inventors:
Vicki S. Johnson - Bel Aire KS, US
Derek W. Rounds - Wichita KS, US
Lawrence R. Nelson - Wichita KS, US
Jeffrey G. Wyckoff - Wellington KS, US
Robin L. Young - Wichita KS, US
Assignee:
Textron Innovations Inc. - Providence RI
International Classification:
G01N 25/02
US Classification:
374 16, 374109, 374 7, 374 3, 374141
Abstract:
A liquid based ice protection test method tests an aircraft part that includes at least a first heating element mounted on an inside surface of an aircraft skin. The method includes bringing the aircraft skin into contact with a low temperature bath and taking one or more temperature readings of the aircraft skin. A liquid based deicing test system includes a container that holds a low temperature bath, a fixture to suspend the aircraft part within the container, and a temperature sensing device for reading temperatures on an outside surface of the aircraft part. A liquid based ice protection test method includes sealing off ends of an aircraft part, attaching at least one temperature sensing device on the aircraft part and at least partially submerging it in a low temperature bath, and obtaining temperature information from the temperature sensing device.


Robin Young Photo 2

Liquid Based Ice Protection Test Systems And Methods

US Patent:
2013032, Dec 12, 2013
Filed:
Aug 12, 2013
Appl. No.:
13/964837
Inventors:
- , unknown
Derek W. Rounds - Wichita KS, US
Lawrence R. Nelson - Wichita KS, US
Jeffrey G. Wyckoff - Wellington KS, US
Robin L. Young - Wichita KS, US
International Classification:
G01K 13/00
US Classification:
7311803
Abstract:
A liquid based ice protection test system for testing an aircraft part having a first heating element comprises a tub configured for retaining a low temperature bath. The system also includes a first support member for suspending the aircraft part in the tub and a first temperature sensing device for sensing temperatures from one or more locations of a skin of the aircraft part.