Benjamin Andrew Harber

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

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.

US Patent:

20070085288, 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

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.

US Patent:

20120248258, 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

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.

US Patent:

20200307789, 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

International Classification:

B64C 39/10
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.

US Patent:

20160185443, 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

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.