Resumes
Resumes
Robert Budica
View pageIndustry:
Aviation & Aerospace
Robert Budica Phones & Addresses
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27152 Woodbluff Rd, Laguna Hills, CA 92653
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1007 Appleton Rd, Simi Valley, CA 93065 (805) 581-5320
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Costa Mesa, CA
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Philadelphia, PA
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1149 Wrightstown Rd, Newtown, PA 18940 (215) 860-4799
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1349 Wrightstown Rd, Newtown, PA 18940 (215) 860-4722 (215) 860-4799
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Las Vegas, NV
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Brea, CA
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Cherry Hill, NJ
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Moorpark, CA
Industries
Aviation & Aerospace
Business Records
Name / Title
Company / Classification
Phones & Addresses
Manager
METRIC PRECISION MACHINE & ENGINEERING, INC
350 W Compton Blvd, Gardena, CA 90248
2390 E Camelback Rd, Phoenix, AZ 85016
535 Griswold St STE 2050, Detroit, MI 48226
2390 E Camelback Rd, Phoenix, AZ 85016
535 Griswold St STE 2050, Detroit, MI 48226
Chairman
AGUSTAWESTLAND PHILADELPHIA CORPORATION
Mfg Aircraft Whol Transportation Equipment
Mfg Aircraft Whol Transportation Equipment
3050 Red Lion Rd, Philadelphia, PA 19114
(215) 281-1400
(215) 281-1400
Publications
Us Patents
Methods And Systems For Light Energy Augmented Power
View pageUS Patent:
20130140916, Jun 6, 2013
Filed:
Dec 6, 2011
Appl. No.:
13/311609
Inventors:
Philip S. Dunlap - Rancho Palos Verdes CA, US
Robert J. Budica - Laguna Hills CA, US
Robert J. Budica - Laguna Hills CA, US
International Classification:
H02J 17/00
US Classification:
307149
Abstract:
A method for transmitting power over long distances to a remote device is described. The method includes positioning a lens between a photon source and a photon receiver, the lens, photon source and photon receiver being physically separate systems, focusing a plurality of photons originating from the photon source using the lens, collecting the photons at a receiver, and utilizing the collected photons to generate electrical power.
High Heat Transfer Rate Reusable Thermal Protection System
View pageUS Patent:
20150354907, Dec 10, 2015
Filed:
Nov 28, 2012
Appl. No.:
13/688195
Inventors:
- Chicago IL, US
Robert J. Budica - Laguna Hills CA, US
Frank O. Chandler - Huntington Beach CA, US
Joseph W. Haney - Huntington Beach CA, US
Robert J. Budica - Laguna Hills CA, US
Frank O. Chandler - Huntington Beach CA, US
Joseph W. Haney - Huntington Beach CA, US
International Classification:
F28F 13/06
B23P 15/26
B23P 15/26
Abstract:
A system and methods for high heat transfer rate reusable thermal protection are presented. A porous skin comprises an exposed exterior surface and a non-exposed surface, and a coolant reservoir comprises perforations coupled to the non-exposed surface, and valves. The valves regulate a flow of coolant from the coolant reservoir to the porous skin in response to a temperature of the porous skin.
Propulsion System And Launch Vehicle
View pageUS Patent:
20150275823, Oct 1, 2015
Filed:
Mar 28, 2014
Appl. No.:
14/228306
Inventors:
- Chicago IL, US
Robert J. Budica - Laguna Hills CA, US
Frank O. Chandler - Huntington Beach CA, US
Robert J. Budica - Laguna Hills CA, US
Frank O. Chandler - Huntington Beach CA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
F02K 9/62
F02K 9/80
F02K 9/84
F02K 9/46
F02K 9/80
F02K 9/84
F02K 9/46
Abstract:
A rocket engine having a co-axial, bidirectional flow arrangement is described herein. The rocket engine receives fuel and an oxidizer into the rocket engine in a first direction, whereby a portion of the fuel is combusted in a pre-burner. The flow direction of the partially combusted fuel/oxidizer mixture is reversed, whereby the mixture is introduced into a combustion chamber. The fuel and oxidizer are combusted in the combustion chamber. The combustion products exit a throat and an expansion plenum in a direction similar to the first direction, whereby the combustion products exit a nozzle of the rocket engine, providing thrust.