Benjamin Harber resumes & CV records
Resumes
Configuration Design Engineer At Boeing
Location:
Orange County, California Area
Industry:
Aviation & Aerospace
Benjamin Andrew Harber, 42Guntersville, AL
Benjamin Harber Phones & Addresses
Guntersville, AL
63 Exeter, Irvine, CA 92612
63 Exeter #29, Irvine, CA 92612
338 Westbrook Pl, Costa Mesa, CA 92626 714-7512428
Santa Ana, CA
Social networks
Benjamin Andrew Harber
Linkedin
Industries
Aviation & Aerospace
Mentions for Benjamin Andrew Harber
Publications & IP owners
Us Patents
Wind Power System
US Patent:
8441141, May 14, 2013
Filed:
Mar 11, 2010
Appl. No.:
12/721628
Inventors:
Richard P. Ouellette - Lakewood CA, US
Benjamin A. Harber - Costa Mesa CA, US
Benjamin A. Harber - Costa Mesa CA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
H02P 9/04
US Classification:
290 55
Abstract:
A wind power system including a first pulley, a second pulley spaced from the first pulley, a continuous loop structure engaged with the first and second pulleys, a plurality of airfoils fixedly connected to the continuous loop structure, wherein the airfoils extend outward from the continuous loop structure, and a fairing positioned to direct airflow to the airfoils.
Direct Loading Apparatus For Pallet Related Systems
US Patent:
2007008, Apr 19, 2007
Filed:
Oct 18, 2005
Appl. No.:
11/252702
Inventors:
James Wells - Fountain Valley CA, US
Anibal Garcia - Chino CA, US
Myles Rohrlick - San Diego CA, US
John Simmons - Corona CA, US
Benjamin Harber - Costa Mesa CA, US
Thomas Reiner - Sherman Oaks CA, US
Anibal Garcia - Chino CA, US
Myles Rohrlick - San Diego CA, US
John Simmons - Corona CA, US
Benjamin Harber - Costa Mesa CA, US
Thomas Reiner - Sherman Oaks CA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B62B 5/00
US Classification:
280079110
Abstract:
An apparatus for transporting and handling a cargo platform is provided. The apparatus includes a frame having a cradle beam that receives the cargo platform. The cradle beam supports a lower surface of the cargo platform. The apparatus further includes a locking mechanism operably associated with the cradle beam and actuates to securely fasten the cargo platform to the frame when the cargo platform is rested upon the cradle beam. The apparatus also includes a plurality of wheel assemblies for wheeling the frame along a ground surface.
Flight Path Control System For Aircraft
US Patent:
2012024, Oct 4, 2012
Filed:
Mar 31, 2011
Appl. No.:
13/076739
Inventors:
Benjamin A. Harber - Costa Mesa CA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B64C 13/00
B64C 13/20
B64C 39/00
B64C 19/00
B64C 3/14
B64C 13/20
B64C 39/00
B64C 19/00
B64C 3/14
US Classification:
244 35 R, 244 93, 244189
Abstract:
A method and apparatus for changing a flight path of an air platform. A change for the flight path of the air platform is identified. A weight system associated with the air platform is moved during flight of the air platform such that a center of mass of the air platform changes in a manner that causes the flight path of the air platform to change.
Aircraft Having Embedded Engines
US Patent:
2020030, Oct 1, 2020
Filed:
Apr 1, 2019
Appl. No.:
16/372337
Inventors:
- Chicago IL, US
Robert H. Liebeck - Irvine CA, US
Edward L. Lawson - Long Beach CA, US
Benjamin A. Harber - Irvine CA, US
Robert H. Liebeck - Irvine CA, US
Edward L. Lawson - Long Beach CA, US
Benjamin A. Harber - Irvine CA, US
International Classification:
B64C 39/10
B64D 27/14
B64D 33/04
B64D 27/14
B64D 33/04
Abstract:
An aircraft having a blended-wing-body configuration includes a centerbody, a pair of wings, at least one pair of engines, a pair of air inlets, and a pair of exhaust outlets. The centerbody has an airfoil-shaped cross section, an aircraft centerline, an aft portion, an upper mold line, a lower mold line, and a pair of centerbody leading edge portions respectively on opposite sides of the aircraft centerline. The wings are integral with the centerbody. The pair of engines are located on opposite sides of the aircraft centerline and are mounted within the centerbody between the upper mold line and the lower mold line. The pair of air inlets are located respectively along the centerbody leading edge portions and are respectively fluidly coupled to the pair of engines. The pair of exhaust outlets our located in the aft portion of the centerbody and our respectively fluidly coupled to the pair of engines.
Dual-Rib Morphing Leading Edge
US Patent:
2016018, Jun 30, 2016
Filed:
Jun 4, 2014
Appl. No.:
14/295713
Inventors:
- Chicago IL, US
Benjamin A. Harber - Irvine CA, US
Neal A. Harrison - Lake Forest CA, US
Benjamin A. Harber - Irvine CA, US
Neal A. Harrison - Lake Forest CA, US
International Classification:
B64C 3/48
Abstract:
A mechanism for changing a shape of a leading edge of an airfoil may include a first rib and a second rib. The first rib may include a plurality of first rib segments. The first rib may move between a first folded shape and a first extended shape. The second rib may include a plurality of second rib segments. The second rib may move between a second folded shape and a second extended shape. An actuator may be coupled to the first rib, the second rib, or both, to move the first rib, the second rib, or both, between their respective folded and extended shapes.
NOTICE: You may not use BackgroundCheck or the information it provides to make decisions about employment, credit, housing or any other purpose that would require Fair Credit Reporting Act (FCRA) compliance. BackgroundCheck is not a Consumer Reporting Agency (CRA) as defined by the FCRA and does not provide consumer reports.