Christopher M Cagle

age ~64

from Yorktown, VA

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Also known as:

Christophe M Cagle
Chris M Cagle
Christo M Cagle
Christphr M Cagle
Mark Cagle
Melinda Cagle

Phone and address:: 209 Walden Dr, Yorktown, VA 23692
7578741407

Connected to:

Christopher Cagle Phones & Addresses

209 Walden Dr, Yorktown, VA 23692 • 7578741407
Grafton, VA
Hampton, VA
Williamsburg, VA
Newport News, VA

Work

Company:

Cantey Hanger LLP
Address:

Specialities

Business • Real Estate • Wills-Trusts-Probate • Securities Law

Us Patents

Adaptive Composite Skin Technology (Acts)
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US Patent:

20050151015, Jul 14, 2005
Filed:

Apr 9, 2004
Appl. No.:

10/828528
Inventors:

Christopher Cagle - Yorktown VA, US
Robin Schlecht - Newport News VA, US
Assignee:

United States of America as represented by the Administrator of the NASA - Washington DC
International Classification:

B64C001/00
US Classification:

244123000, 244130000
Abstract:

A tailorable elastic skin is provided for covering shape-changing, or “morphable,” structures. The skin comprises a two-dimensional “planar spring” embedded in an elastomeric material. The invention provides a smooth aerodynamic covering capable of global elongation exceeding 20% with a low input force. The design can be tailored for light-weight, lightly loaded applications, or for more heavily loaded aerodynamic or hydrodynamic conditions.

Jet Engine Exhaust Nozzle Flow Effector
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US Patent:

20080272232, Nov 6, 2008
Filed:

Jun 14, 2007
Appl. No.:

11/762827
Inventors:

Christopher M. Cagle - Yorktown VA, US
Randolph H. Cabell - Hampton VA, US
Travis L. Turner - Newport News VA, US
Roberto J. Cano - Yorktown VA, US
Richard J. Silcox - Poquoson VA, US
Ralph D. Buehrle - Williamsburg VA, US
George C. Hilton - Hampton VA, US
Assignee:

Administrator of the National Aeronautics and and Space Administration - Washington DC
International Classification:

B64C 13/00
US Classification:

244 998
Abstract:

A jet engine exhaust nozzle flow effector is a chevron formed with a radius of curvature with surfaces of the flow effector being defined and opposing one another. At least one shape memory alloy (SMA) member is embedded in the chevron closer to one of the chevron's opposing surfaces and substantially spanning from at least a portion of the chevron's root to the chevron's tip.

Flexible Volumetric Structure
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US Patent:

20100314810, Dec 16, 2010
Filed:

Jun 11, 2009
Appl. No.:

12/482503
Inventors:

Christopher M. Cagle - Yorktown VA, US
Robin W. Schlecht - Newport News VA, US
Assignee:

USA as represented by the Administrator of NASA - Washington DC
International Classification:

F16F 3/00
US Classification:

267110, 267112
Abstract:

A flexible volumetric structure has a first spring that defines a three-dimensional volume and includes a serpentine structure elongatable and compressible along a length thereof. A second spring is coupled to at least one outboard edge region of the first spring. The second spring is a sheet-like structure capable of elongation along an in-plane dimension thereof. The second spring is oriented such that its in-plane dimension is aligned with the length of the first spring's serpentine structure.

Jet Engine Exhaust Nozzle Flow Effector
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US Patent:

20110203288, Aug 25, 2011
Filed:

Apr 28, 2011
Appl. No.:

13/096305
Inventors:

Travis L. Turner - Yorktown VA, US
Roberto J. Cano - Yorktown VA, US
Richard J. Silox - Poquoson CA, US
Ralph D. Buehrle - Williamsburg VA, US
Christopher M. Cagle - Yorktown VA, US
Randolph H. Cabell - Hampton VA, US
George C. Hilton - Hampton VA, US
Assignee:

U. S. A. as represented by the Administrator of the National Aeronautics and Space Administration - Washington DC
International Classification:

F02K 1/10
US Classification:

60771
Abstract:

A jet engine exhaust nozzle flow effector is a chevron formed with a radius of curvature with surfaces of the flow effector being defined and opposing one another. At least one shape memory alloy (SMA) member is embedded in the chevron closer to one of the chevron's opposing surfaces and substantially spanning from at least a portion of the chevron's root to the chevron's tip.

Distributed Electric Propulsion Modular Wing Aircraft With Blown Wing And Extreme Flaps For Vtol And/Or Stol Flight
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US Patent:

20210331791, Oct 28, 2021
Filed:

Apr 24, 2020
Appl. No.:

16/857954
Inventors:

- Washington DC, US
David D. North - Williamburg VA, US
Robert G. McSwain - Yorktown VA, US
Michael D. Patterson - Yorktown VA, US
Gregory Howland - Yorktown VA, US
Jared S. Fell - Yorktown VA, US
Christopher M. Cagle - Yorktown VA, US
Xiaofan Fei - Bellevue WA, US
Siena K.S. Whiteside - Poquoson VA, US
David A. Hare - Smithfield VA, US
International Classification:

B64C 29/00
B64C 11/46
B64C 39/08
B64C 9/04
B64C 9/00
B64C 13/02
B64D 27/24
B64D 31/02
Abstract:

An aircraft wing configuration for a vertical or a short take-off and landing aircraft having a plurality of propeller-blown wings mounted at different longitudinal locations along a fuselage of the vertical take-off and landing aircraft, producing two or more lifting surfaces, fixed at a predetermined acute wing angle greater than 0 and substantially less than 90 relative to a horizontal plane, and having a plurality of flaps disposed behind the wings. The configuration has a plurality of propellers distributed in front of the plurality of wings producing two or more lifting surfaces and mounted such that the wings are externally blown by forced airstreams from the propellers. The propellers produce distributed thrust components, and the plurality of flaps are in the forced airstreams of the propellers when one or more of the flaps is in an extended position.