Professional Records
License Records
John C Pizzichemi
Address:
20011 27 Ave SE, Bothell, WA 98012
License #:
A5263191
Category:
Airmen
John Pizzichemi Phones & Addresses
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20011 27Th Ave, Bothell, WA 98012 (425) 481-5448
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Des Moines, WA
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Snohomish, WA
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20011 27Th Ave SE, Bothell, WA 98012 (206) 850-8618
Work
Company:
Boeing
Position:
Engineer
Industries
Aviation & Aerospace
Resumes
Resumes
Engineer
View pageLocation:
Bothell, WA
Industry:
Aviation & Aerospace
Work:
Boeing
Engineer
Engineer
Publications
Us Patents
Temperature Controlled Electronics Tray
View pageUS Patent:
20100089895, Apr 15, 2010
Filed:
Oct 14, 2008
Appl. No.:
12/251337
Inventors:
Myles E. Brown - Bothell WA, US
John C. Pizzichemi - Bothell WA, US
Florence L. Lopez - Mill Creek WA, US
Robert B. Stevenson - Lynnwood WA, US
John C. Pizzichemi - Bothell WA, US
Florence L. Lopez - Mill Creek WA, US
Robert B. Stevenson - Lynnwood WA, US
International Classification:
H05B 11/00
US Classification:
219209, 219494, 219530, 219531, 219501
Abstract:
Apparatus for housing electronic components comprising a heated enclosure comprising a bottom, a top, three sides, a substantially open front and a heating element for transmitting heat to enclosure surfaces. Perforations are located in the heated enclosure to facilitate the passage of air from one side of the heated enclosure to the other. A plenum is connected to the perforations, the plenum being configured to transmit air between the outside and inside of the heated enclosure. Completing the apparatus as control electronics comprising a power source and temperature monitoring and feedback circuitry, and insulation covering a heated portion of the heated enclosure.
Variable Chiller Exhaust With Crown Ventilation
View pageUS Patent:
20210339872, Nov 4, 2021
Filed:
Apr 29, 2020
Appl. No.:
16/862146
Inventors:
- Chicago IL, US
Brian C. Christenson - Arlington WA, US
John C. Pizzichemi - Bothell WA, US
Brian C. Christenson - Arlington WA, US
John C. Pizzichemi - Bothell WA, US
International Classification:
B64D 13/06
Abstract:
A variable chiller exhaust system incorporate a plurality of chillers, each chiller having an inlet receiving air from a crown in an aircraft fuselage and an outlet connected to a manifold. A plurality of check valves are connected to the manifold and configured to maintain a differential back pressure on the plurality of chillers of 2″ water pressure or less. The check valves vent into the crown. An exhaust conduit is connected to direct air from the manifold to a variable speed fan. An outflow valve exhausts air from the variable speed fan to an exterior of the fuselage.