DR. MICHAEL RICHARD ROBINSON, M.D.
Medical Practice at Pacific Coast Hwy, Huntington Beach, CA
License number
California 137097
Category
Medical Practice
Type
Ophthalmology
License number
California 164486
Category
Medical Practice
Type
Ophthalmology
Address
Address
200 Pacific Coast Hwy #147, Huntington Beach, CA 92648
Phone
(949) 419-5928
Personal information
See more information about MICHAEL RICHARD ROBINSON at radaris.comName
Address
Phone
4900 Overland Ave Unit 192, Culver City, CA 90230
4921 Hermosa Ct, Yucca Valley, CA 92284
4930 Harrison St, Chino, CA 91710
4946 Bay View Cir, Stockton, CA 95219
497 Desert Lakes Cir, Palm Springs, CA 92264
Professional information
Michael Robinson - Huntington Beach, CA
Work:
DECISIVE ANALYTICS CORPORATION
Space & Missile Systems Senior Engineer IV / Analyst Defense Intelligence Agency JRE West, USNR
Strategic Debriefer / Intelligence Analyst Science Applications international corporation (SAIC)
Space & Missile Systems Engineer / Systems Test / Program Security Coordinator United States Navy
Operations Intelligence Specialist
Space & Missile Systems Senior Engineer IV / Analyst Defense Intelligence Agency JRE West, USNR
Strategic Debriefer / Intelligence Analyst Science Applications international corporation (SAIC)
Space & Missile Systems Engineer / Systems Test / Program Security Coordinator United States Navy
Operations Intelligence Specialist
Education:
American Inter-continental University - London
Bachelor of Science in Criminal Justice Penn State University
Masters of Geographic Information Systems University of Maryland
BS
Bachelor of Science in Criminal Justice Penn State University
Masters of Geographic Information Systems University of Maryland
BS
Michael Robinson - Huntington Beach, CA
Work:
United States Navy reserve
Assistant Command Duty Officer Assigned to Commander US Naval Forces Europe Science Applications international corporation (SAIC)
Space & Missile Systems Engineer United States Navy
Assistant Command Duty Officer Assigned to Commander US Naval Forces Europe Science Applications international corporation (SAIC)
Space & Missile Systems Engineer United States Navy
Education:
American Inter-continental University - London
Bachelor of Science in Criminal Justice Penn State University
Masters of Geographic Information Systems University of Maryland
BS
Bachelor of Science in Criminal Justice Penn State University
Masters of Geographic Information Systems University of Maryland
BS
Michael Robinson - Huntington Beach, CA
Work:
decisive analytics corporation
Space & Missile Systems Senior Engineer IV / Analyst Strategic Debriefer science applications international corporation
Space & Missile Systems Engineer IV / System Test/ Project Manager Air Radar / Electronic Warfare
Space & Missile Systems Senior Engineer IV / Analyst Strategic Debriefer science applications international corporation
Space & Missile Systems Engineer IV / System Test/ Project Manager Air Radar / Electronic Warfare
Education:
Continental University
Bachelor of Science in Criminal Justice PENN STATE UNIVERSITY
Masters of Geographic Information Systems
Bachelor of Science in Criminal Justice PENN STATE UNIVERSITY
Masters of Geographic Information Systems
Fabric Preform Insert For A Composite Tank Y-Joint
US Patent:
2012001, Jan 26, 2012
Filed:
Jul 22, 2010
Appl. No.:
12/841502
Inventors:
Michael J. Robinson - Huntington Beach CA, US
Michael Leslie Hand - Huntington Beach CA, US
Michael Leslie Hand - Huntington Beach CA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B32B 3/06, B64G 1/22, B29C 65/00
US Classification:
2441723, 428 57, 156182
Abstract:
A method and apparatus for forming a joint. A composite insert may be placed into a joint region for a first structure. The composite insert may comprise a structure having a first portion, a second portion, and a third portion all extending from a junction; and a resin impregnated into the structure to form the composite insert. The second structure may be laid up. The composite insert may be bonded to the first structure and the second structure.
Fluid Separation Assembly And Method
US Patent:
2012031, Dec 13, 2012
Filed:
Mar 3, 2012
Appl. No.:
13/411548
Inventors:
Brent Kenneth Theodore - Rossmoor CA, US
James P. Huang - Irvine CA, US
Michael J. Robinson - Huntington Beach CA, US
Ivana Jojic - Bellevue WA, US
James P. Huang - Irvine CA, US
Michael J. Robinson - Huntington Beach CA, US
Ivana Jojic - Bellevue WA, US
Assignee:
The Boeing Company - Seal Beach CA
International Classification:
B01D 69/08, B01D 53/22
US Classification:
95 47, 96 8
Abstract:
In an embodiment there is provided a fluid separation assembly. The assembly has a hollow fiber bundle with a plurality of hollow fiber membranes. The assembly further has a first tubesheet and a second tubesheet encapsulating respective ends of the hollow fiber bundle, wherein one of the tubesheets has a plurality of radial through openings formed in the tubesheet. The assembly further has a housing surrounding the hollow fiber bundle and the first and second tubesheets, the housing having a feed inlet port, a permeate outlet port, and a non-permeate outlet port. The feed gas, permeate gas, or non-permeate gas are introduced into or removed from the hollow fiber membranes via the plurality of radial through openings formed in the tubesheet, such that the radial through openings of the tubesheet intersect each or substantially each of the hollow fiber membranes.
Composite Tank Having Joint With Softening Strip And Method Of Making The Tank
US Patent:
2013019, Aug 1, 2013
Filed:
Jul 3, 2012
Appl. No.:
13/541560
Inventors:
Michael J. Robinson - Huntington Beach CA, US
Michael Leslie Hand - Huntington Beach CA, US
Creed Ernest Blevins - Aliso Viejo CA, US
Michael Leslie Hand - Huntington Beach CA, US
Creed Ernest Blevins - Aliso Viejo CA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B65D 90/02, B32B 37/14
US Classification:
220565, 220562, 156182
Abstract:
A composite resin tank includes a wall joined to a dome along a joint. A softening strip is located in the joint.
Method For Making Composite Truss Panel Having A Fluted Core
US Patent:
7998299, Aug 16, 2011
Filed:
Oct 1, 2008
Appl. No.:
12/243926
Inventors:
Douglas A. McCarville - Orting WA, US
Juan C. Guzman - Seattle WA, US
Michael L. Hand - Huntington Beach CA, US
Michael J. Robinson - Huntington Beach CA, US
Juan C. Guzman - Seattle WA, US
Michael L. Hand - Huntington Beach CA, US
Michael J. Robinson - Huntington Beach CA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B32B 37/00
US Classification:
156189, 156191
Abstract:
A composite truss structure employs a sandwich-in-sandwich construction in which a composite fluted core is sandwiched between two facesheets, and at least one structural foam stiffener is sandwiched within the core or between the facesheets and/or the core.
Thermal Protection System With Staggered Joints
US Patent:
2009008, Apr 2, 2009
Filed:
Sep 28, 2007
Appl. No.:
11/864619
Inventors:
Xavier D. Simon - Aliso Viejo CA, US
Michael J. Robinson - Huntington Beach CA, US
Thomas L. Andrews - Newport Beach CA, US
Michael J. Robinson - Huntington Beach CA, US
Thomas L. Andrews - Newport Beach CA, US
International Classification:
B64G 1/58
US Classification:
2441717
Abstract:
The thermal protection system disclosed herein is suitable for use with a spacecraft such as a reentry module or vehicle, where the spacecraft has a convex surface to be protected. An embodiment of the thermal protection system includes a plurality of heat resistant panels, each having an outer surface configured for exposure to atmosphere, an inner surface opposite the outer surface and configured for attachment to the convex surface of the spacecraft, and a joint edge defined between the outer surface and the inner surface. The joint edges of adjacent ones of the heat resistant panels are configured to mate with each other to form staggered joints that run between the peak of the convex surface and the base section of the convex surface.
Common Bulkhead For Composite Propellant Tanks
US Patent:
2012020, Aug 16, 2012
Filed:
Feb 15, 2011
Appl. No.:
13/027429
Inventors:
Michael James Robinson - Huntington Beach CA, US
Michael Leslie Hand - Huntington Beach CA, US
Michael Leslie Hand - Huntington Beach CA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B64G 1/66, B32B 37/00, B65D 90/12, B32B 3/30
US Classification:
2441722, 428166, 1563071, 220 15
Abstract:
An apparatus comprising a first structure, a second structure, a first layer, and a second layer. The first structure has a first plurality of channels extending towards a number of edges of the first structure. The second structure has a second plurality of channels extending towards a number of edges of the second structure. A first side of the first structure is connected to a first side of the second structure. The first plurality of channels and the second plurality of channels have an orientation with respect to each other. The first layer is connected to a second side of the first structure. The second layer is connected to a second side of the second structure.
Composite Truss Panel Having Fluted Core
US Patent:
2011030, Dec 8, 2011
Filed:
Aug 16, 2011
Appl. No.:
13/211166
Inventors:
Douglas A. McCarville - Orting WA, US
Juan C. Guzman - Seattle WA, US
Michael L. Hand - Huntington Beach CA, US
Michael J. Robinson - Huntington Beach CA, US
Juan C. Guzman - Seattle WA, US
Michael L. Hand - Huntington Beach CA, US
Michael J. Robinson - Huntington Beach CA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B32B 3/28, B32B 3/00
US Classification:
428174
Abstract:
A composite truss structure employs a sandwich-in-sandwich construction in which a composite fluted core is sandwiched between two facesheets, and at least one structural foam stiffener is sandwiched within the core or between the facesheets and/or the core.