1
Arvin Shmilovich, Yoram Yadlin: Low noise wing slat system with rigid cove-filled slat. The Boeing Company, Hope Baldauff Hartman, April 23, 2013: US08424810 (20 worldwide citation)

Concepts and technologies described herein provide for a low noise aircraft wing slat system. According to one aspect of the disclosure provided herein, a cove-filled wing slat is used in conjunction with a moveable panel rotatably attached to the wing slat to provide a high lift system. The moveabl ...


2
Arvin Shmilovich, Yoram Yadlin, David M Smith, Roger W Clark: Active system for wide area suppression of engine vortex. The Boeing Company, Alston & Bird, July 20, 2004: US06763651 (18 worldwide citation)

The active system for the wide area suppression of a ground vortex generated by the engine of an aircraft includes an actuator assembly in fluid communication with a fluid source; and, at least one nozzle assembly, including at least one movable nozzle. The movable nozzle is in fluid communication w ...


3
Arvin Shmilovich, Yoram Yadlin, Robert D Gregg III, Roger W Clark: Systems and methods for control of engine exhaust flow. The Boeing Company, Tung & Associates, November 2, 2010: US07823840 (16 worldwide citation)

Coanda Effect and lift produced along a surface of an airfoil are increased by ducting compressed fluid from the engine to the surface of the airfoil. An engine produces exhaust gases that are predominantly directed toward an aft end of the aircraft by a cowling or other structure as an exhaust plum ...


4
Arvin Shmilovich, Yoram Yadlin, Robert D Gregg III, Roger W Clark: Method and apparatus for enhancing engine-powered lift in an aircraft. The Boeing Company, Tung & Associates, February 1, 2011: US07878458 (15 worldwide citation)

Lift produced by an airfoil of an aircraft is increased by suppressing fluid detachment from the surface of the airfoil. An engine cowling extends outwardly from the surface of the airfoil that has an exit plane configured for directing exhaust gases toward a rear of the aircraft. Fences extending o ...


5
Arvin Shmilovich, Yoram Yadlin, Roger Clark, Donald Leopold: Apparatus and method for the control of trailing wake flows. The Boeing Company, Robert B Hughes, Hughes Law Firm PLLC, September 5, 2006: US07100875 (14 worldwide citation)

A system and method for dissipating vortices that form at the wingtips on aircraft and from other airfoils. A jet air stream is discharged in a location at or proximate to the outer end portion of the airfoil into the vortex flow, and the jet air stream is moved cyclically back and forth. The cyclic ...


6
Arvin Shmilovich, Yoram Yadlin, Roger W Clark: Lift augmentation system and associated method. The Boeing Company, Alston & Bird, October 11, 2011: US08033510 (10 worldwide citation)

A system and method for generating lift provided by a multi-element aircraft wing are provided. The system includes a main wing element, a slat interconnected to the main wing element, and a flap interconnected to the main wing element. The system also includes at least one port defined in at least ...


7
Arvin Shmilovich, Yoram Yadlin: Low noise wing slat system with deployable wing leading edge elements. The Boeing Company, Hope Baldauff Hartman, October 2, 2012: US08276852 (10 worldwide citation)

Concepts and technologies described herein provide for a low noise aircraft wing slat system. According to one aspect of the disclosure provided herein, a cove-filled wing slat is used in conjunction with a moveable leading edge element of an aircraft wing to provide a high lift system. The moveable ...


8
Arvin Shmilovich, Yoram Yadlin, Roger W Clark, Donald H Leopold: Systems and methods for destabilizing an airfoil vortex. The Boeing Company, Perkins Coie, February 16, 2010: US07661629 (7 worldwide citation)

Apparatuses and methods for the controlled trailing wake flows. An apparatus in accordance with one embodiment is directed to an aircraft system that includes an airfoil having first and second oppositely facing flow surfaces and a tip. The system can further include a vortex dissipation device carr ...


9
Arvin Shmilovich, Yoram Yadlin, Roger W Clark, Robert D Gregg III: Propulsion system and method for efficient lift generation. The Boeing Company, Tung & Associates, January 3, 2012: US08087618 (6 worldwide citation)

A propulsion system for an aircraft includes an airfoil, an engine having an engine cowling carried by the airfoil and configured to produce exhaust gases that are predominantly directed toward an aft end of the airfoil by the engine cowling as engine exhaust, a propulsion flap carried by the airfoi ...


10
Arvin Shmilovich, Yoram Yadlin, Roger W Clark: Active systems and methods for controlling an airfoil vortex. The Boeing Company, Perkins Coie, September 13, 2011: US08016244 (5 worldwide citation)

Active systems and methods for controlling aircraft vortices are disclosed. An apparatus in accordance with one embodiment is directed to an aircraft system that includes an airfoil having first and second oppositely facing flow surfaces and a tip. The system can further include a vortex dissipation ...



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