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Michael B Diverde, 60Granite Falls, WA

Michael Diverde Phones & Addresses

Granite Falls, WA   

3339 166Th St, Bellevue, WA 98008    425-4498343   

17172 Bolsa Chica St, Huntingtn Bch, CA 92649    714-3775606   

Huntington Beach, CA   

Ladera Ranch, CA   

97 Camino Del Oro, Rancho Santa Margarita, CA 92688    949-4591269   

28 Tomahawk St, Trabuco Canyon, CA 92679    949-4591269   

Tucson, AZ   

Westminster, CA   

Work

Position: Building and Grounds Cleaning and Maintenance Occupations

Education

Degree: Associate degree or higher

Mentions for Michael B Diverde

Michael Diverde resumes & CV records

Resumes

Michael Diverde Photo 14

Engineer At Boeing

Position:
Engineer at Boeing
Location:
Greater Seattle Area
Industry:
Aviation & Aerospace
Work:
Boeing
Engineer
Michael Diverde Photo 15

Michael Diverde

Publications & IP owners

Us Patents

Twin Lobe Spacecraft Dispenser Apparatus And Method

US Patent:
6357698, Mar 19, 2002
Filed:
Feb 2, 2000
Appl. No.:
09/496965
Inventors:
Michael B. DiVerde - Rancho Santa Margarita CA
Kenneth Norman Telford - Huntington Beach CA
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64G 122
US Classification:
244158R
Abstract:
A dispenser apparatus and method which includes a blended dispenser shell having a lower portion and a pair of integrally formed upper support portions defining two distinct support areas on which a pair of spacecrafts can be supported in a side-by-side configuration. The upper support portions are further disposed within an envelope defined by a lower edge of the lower portion of the dispenser shell. In one alternative embodiment a pair of adapter shells are disposed on the upper support portions to enable interfacing with a standardized interface ring of each spacecraft. The embodiments of the dispenser are each formed from a graphite epoxy material by conventional construction processes and significantly reduce the overall weight of the dispenser, as compared with dispensers which support a pair of spacecrafts in a vertical configuration. The dispenser of the present invention further reduces the overall cost associated with supporting a pair of spacecrafts and reduces the amount of orbital debris which would otherwise be produced with dispensers which support a pair of spacecrafts in a vertical configuration.

Satellite Dispenser

US Patent:
6416018, Jul 9, 2002
Filed:
Mar 22, 1999
Appl. No.:
09/273844
Inventors:
Michael B. DiVerde - Rancho Santa Margarita CA
Kenneth N. Telford - Huntington Beach CA
George J. Budris - Huntington Beach CA
Christopher M. Gil - Huntington Beach CA
John F. Steinmeyer - Orange CA
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64G 110
US Classification:
2441371, 244158 R, 244161
Abstract:
A satellite dispenser adapted to be coupled to a launch vehicle. The dispenser includes a single-piece, integrally formed tubular shell for supporting a plurality of independent satellites thereon. The tubular shell is significantly lighter than multi-piece dispenser shells that require a connecting ring for coupling the post portion and base portion of the shell together. The single piece shell also significantly reduces the cost and simplifies the manufacture of the dispenser shell. The dispenser shell, in certain preferred embodiments, includes a tapered post portion which enables satellites being carried on the upper portion of the post portion to extend further into a fairing disposed over the satellites and dispenser shell during flight, thus making more efficient use of the envelope defined by the interior area of the fairing. A frusto-conical base portion integrally formed with the post portion enables the load supported by the dispenser shell to be evenly distributed throughout the base portion. The single-piece design also significantly improves the bending stress resistance of the dispenser and its overall structural rigidity.

Spacecraft Dispensing System

US Patent:
6138951, Oct 31, 2000
Filed:
Aug 10, 1998
Appl. No.:
9/131475
Inventors:
George J. Budris - Huntington Beach CA
Peter A. McGrath - Tustin CA
Tony L. Toulouse - Irvine CA
Richard J. Catalano - Fountain Valley CA
Michael B. Diverde - Rancho Santa Margarita CA
Assignee:
McDonnell Douglas Corporation - Seal Beach CA
International Classification:
B64G 100
B64G 122
F42B 1258
US Classification:
244158R
Abstract:
A dispensing system for releasing a number of spacecraft from a launch vehicle. The dispensing system includes a base support structure securely fastened to a launch vehicle and a number of stacked frame assemblies. Each frame assembly includes a number of substantially parallel load bearing elongated post elements and a shear load transferring structure. The post elements are so arranged and spaced so as to define a geometry having a centerline. Each post element has a first end portion and a second end portion. Each first end portion is connected to either another frame assembly or the base support structure of the launch vehicle. The post elements support a number of spacecraft. The spacecraft are supported between adjacent post elements. The shear load transferring structure is connected to the post elements for transferring shear loads between the post elements. The dispensing system also includes a plurality of longitudinally spaced stabilizers connected to desired locations on the post elements to increase the buckling capability of the dispensing system.

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