JEFFREY ALAN TURNER
Pilots at Monterey St, Chandler, AZ

License number
Arizona A2255466
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
4195 W Monterey St, Chandler, AZ 85226

Professional information

Jeffrey Turner Photo 1

Non-Streaking Drainmast

US Patent:
7651055, Jan 26, 2010
Filed:
May 5, 2005
Appl. No.:
11/122354
Inventors:
Jeffrey A. Turner - Chandler AZ, US
Andrew Appleby - Phoenix AZ, US
Robert L. Hoover - Phoenix AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
B64D 1/00
US Classification:
244136, 2441291
Abstract:
A drainmast for discharging fluid from a body in motion, such as an aircraft in flight, may include a barrier disposed at a distal portion of the drainmast. The barrier may extend downstream from the drainmast trailing edge, and may be disposed at a negative angle of attack to a local free-stream airflow, thereby forming a downdraft over the barrier to prevent migration of discharged fluid towards an aircraft skin. In some embodiments, the drainmast may include one or more vanes, disposed internally within a discharge conduit of the drainmast, for deflecting fluid flow within the drainmast towards a direction of free-stream airflow outside the drainmast. Methods for channeling fluid away from an external surface of an aircraft in flight are also disclosed.


Jeffrey Turner Photo 2

Turbine Engine Diffusing Exhaust Muffler

US Patent:
7762374, Jul 27, 2010
Filed:
Nov 22, 2006
Appl. No.:
11/603424
Inventors:
Jeffrey A. Turner - Chandler AZ, US
Yogendra Y. Sheoran - Scottsdale AZ, US
Bruce D. Bouldin - Phoenix AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F01N 13/04
US Classification:
181239, 181213, 181238, 415119, 244 1 N
Abstract:
An exhaust muffler is provided for a turbine engine with at least first and second exhaust outlets. The exhaust muffler includes a first arm configured to be coupled to the first exhaust outlet of the turbine engine. The first arm includes an outer surface, and an inner surface that defines a first exhaust cavity. The first arm further includes a plurality of perforations extending between the inner and outer surfaces. The exhaust muffler further includes a second arm coupled to the first arm and configured to be coupled to the second exhaust outlet of the turbine engine. The second arm includes an outer surface, and an inner surface that defines a second exhaust cavity. The second arm also includes a plurality of perforations extending between the inner and outer surfaces.