Paul Diep resumes & CV records
Resumes
Paul Diep
Paul Diep
Paul Bao Diep, Age 647225 Lotus Ave APT D, San Gabriel, CA 91775
Paul Diep Phones & Addresses
7225 Lotus Ave APT D, San Gabriel, CA 91775 (626) 297-9432
Montebello, CA
City of Industry, CA
Cudahy, CA
Woodside, NY
206 E Angeleno Ave, San Gabriel, CA 91776
Mentions for Paul Bao Diep
Publications & IP owners
Us Patents
Aircraft Tail Assembly
US Patent:
2021030, Sep 30, 2021
Filed:
Mar 27, 2020
Appl. No.:
16/832176
Inventors:
- Chicago IL, US
Max Tyler Breedlove - Seal Beach CA, US
Paul Diep - Bothell WA, US
Peter John Newnham - Mukilteo WA, US
Max Tyler Breedlove - Seal Beach CA, US
Paul Diep - Bothell WA, US
Peter John Newnham - Mukilteo WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 1/06
B64C 1/10
B64F 5/10
B64C 1/10
B64F 5/10
Abstract:
An aircraft tail assembly includes an aft fuselage section secured to a forward fuselage section, and includes a stiffener-reinforced pivot bulkhead defined by separate parts secured together by a first set of splices. A longeron extends longitudinally along the aft and forward fuselage sections, and includes a discontinuity adjacent a peripheral edge of the pivot bulkhead. The aircraft tail assembly includes a second set of splices that overlie the discontinuity. One of the second set of splices extends laterally over the longeron to bridge the discontinuity adjacent the peripheral edge of the pivot bulkhead, and another of the second set of splices extends longitudinally along the longeron to secure the longeron to the pivot bulkhead adjacent the discontinuity. A chord engages the peripheral edge of the pivot bulkhead to facilitate transfers of force loads from the bulkhead along a load path that includes the longerons and the splices.
Pivot Fittings Back Up Beam Architecture
US Patent:
2021028, Sep 16, 2021
Filed:
Mar 16, 2020
Appl. No.:
16/820147
Inventors:
- Chicago IL, US
MAX T. BREEDLOVE - Seal Beach CA, US
BERNHARD DOPKER - Bellevue WA, US
PAUL B. DIEP - Bothell WA, US
STEVEN EDWARD PEARSON - Lynnwood WA, US
MAX T. BREEDLOVE - Seal Beach CA, US
BERNHARD DOPKER - Bellevue WA, US
PAUL B. DIEP - Bothell WA, US
STEVEN EDWARD PEARSON - Lynnwood WA, US
International Classification:
B64C 1/06
B64F 5/10
B64F 5/10
Abstract:
A vehicle, such as an aircraft, structural architecture for supporting a horizontal stabilizer with a back up beam having an upper longeron fitting connected to the front side and secured with a back up fitting on the back side, a lower longeron fitting connected to the front side and secured with a back up fitting on the back side, and a pivot fitting connected to the front side of the first back up beam in between the upper longeron fitting and the lower longeron fitting and secured with a third back up fitting on the back side of the back up beam.
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