Martin L. Gomez - Fairfax VA, US Robert Parks - San Jose CA, US Adam J. Woodworth - Melrose MA, US
Assignee:
Aurora Flight Sciences Corporation - Manassas VA
International Classification:
B64C 37/02 B64C 23/06 B64D 5/00
US Classification:
244 2, 244 1 TD, 2441993
Abstract:
A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure.
Martin L. Gomez - Fairfax VA, US Robert Parks - San Jose CA, US Adam J. Woodworth - Melrose MA, US
Assignee:
Aurora Flight Sciences Corporation - Manassas VA
International Classification:
B64C 37/02 B64C 23/06
US Classification:
244 2, 2441993, 244 3, 244 1 TD
Abstract:
A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure.
Martin L. Gomez - Fairfax VA, US Robert Parks - San Jose CA, US Adam J. Woodworth - Melrose MA, US
Assignee:
Aurora Flight Sciences Corporation - Manassas VA
International Classification:
B64C 37/02 B64C 23/06 B64D 5/00
US Classification:
244 2, 244 3, 2441992, 2441993, 244 1 TD
Abstract:
A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure.
Deployment Of Telescoping Aircraft Structures By Drogue Parachute Riser Tension
Tom Clancy - Washington DC, US Robert Parks - San Jose CA, US
Assignee:
Aurora Flight Sciences Corporation - Manassas VA
International Classification:
B64C 1/00 B64C 3/56 B64C 25/10
US Classification:
244 1TD, 244 49, 244102 R, 24115 R
Abstract:
A system for deploying a deployable structure in an aircraft, comprising a drogue parachute, at least one deployable structure, a riser line attached to the drogue parachute and the at least one deployable structure, wherein when the drogue parachute is deployed, a tension is applied to the riser line, and a parachute deployment system, wherein the parachute deployment system is configured to utilize the applied tension to deploy the at least one deployable structure.
Christopher James Evans - Gaithersburg MD Robert Edson Parks - Tucson AZ
Assignee:
The United States of America as represented by the Secretary of Commerce - Washington DC
International Classification:
B24B 1100
US Classification:
451 41
Abstract:
A polishing lap which is resistant to attack from corrosive and reactive ishing media and which has a surface which is sufficiently resilient to provide good finishes without hindering dimensional controlling and accuracy of the texturing comprises: a lap substrate wherein the surface of the lap substrate has an overall shape and a localized texture; and a replaceable lap film applied to the lap substrate surface and which is deformed to correspond to the localized texture of the lap substrate surface. The polishing lap can be easily reconditioned if contaminated or easily modified for use with different abrasives and polishing media.
Interferometric Thickness Variation Test Method For Windows And Silicon Wafers Using A Diverging Wavefront
Christopher James Evans - Gaithersburg MD Robert Edson Parks - Tucson AZ
Assignee:
The United States of America as represented by the Secretary of Commerce - Washington DC
International Classification:
G01B 902
US Classification:
356357
Abstract:
An interferometric apparatus and method are provided for determining a ceal thickness and thickness variations of silicon wafers and other window-like optics. The method includes the steps of (1) emitting a beam of electromagnetic radiation having a diverging wavefront, at an object which is transparent to the radiation, (2) splitting the beam into a reference beam and a test beam, (3) positioning the object in a first position in the test beam to irradiate a central portion of the object, (4) directing the test beam through the central portion, (5) causing the reference beam to interfere with the test beam which has passed through the central portion to form a first interferometric fringe pattern, (6) changing the length of the test beam which has passed through the object until the first interferometric pattern is changed into a desired second interferometric fringe pattern, (7) determining a central thickness of the object in accordance with an amount by which the length of the test beam was changed, (8) moving the object in said test beam to a location in the test beam to irradiate a second portion of the object which is larger than the central portion, (9) causing the reference beam to interfere with the test beam which has passed through the second portion to form a third interferometric fringe pattern, and (10) determining variations relative to the central thickness in accordance with the third interferometric fringe pattern. The method can also be used for measuring thickness variations by taking into account a bow in the object. An interferometer is also provided for carrying out the method.
Dr. Parks graduated from the Columbia University College of Physicians and Surgeons in 1990. He works in Fishkill, NY and 1 other location and specializes in Otolaryngology. Dr. Parks is affiliated with New York Presbyterian Hudson Valley Hospital Center and Northern Westchester Hospital.
B & V Repair Damascus, MD 2011 to 2013 Owner and Master TechnicianMidas Bethesda Bethesda, MD 2008 to 2009 Master Technician & Store ManagerAuto Therapy Gaithersburg, MD 2006 to 2008 MechanicAltered Atmosphere Motorsports Gaithersburg, MD 2004 to 2006 MechanicMeineke Germantown, MD 2000 to 2004 Mechanic
Education:
Thomas Jefferson High School 1999 High school diploma