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James A Dees

from Zephyrhills, FL
Age ~65
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Also known as:
James Dee, Jamesa Dees
Related to:
Justin WorkmanRandall DeesCarolyn Dees, 53Dees L GordonRandal H Dees, 59Denise H Sly, 66Gordon L Dees, 89
Connected to:
Altimese L Dees, 54Brad DeesCarey R Dees, 45Demarcus J Dees, 32Frank A Dees, 70Isabel A Dees, 43John L Dees, 63Kathy L Dees, 70Leland D Dees, 50Sabrina M Dees, 46

James Dees Phones & Addresses

  • Zephyrhills, FL
  • Hollywood, FL
  • Coatesville, PA
  • Miami, FL
  • Hallandale Beach, FL
  • Huber Heights, OH

Resumes

Resumes

James Dees Photo 1

James Dees

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Location:
10835 Indian Hills Ct, Largo, FL 33777
Industry:
Arts And Crafts
Skills:
Crafts
James Dees Photo 2

Compliance Specialist

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Work:

Compliance Specialist
James Dees Photo 3

Pastor

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Industry:
Religious Institutions
Work:
Clement Baptist Church
Pastor
James Dees Photo 4

Cap 1 Supervisor

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Work:
Walmart
Cap 1 Supervisor
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Form Carpenter

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Work:
Titeline Constuiom
Form Carpenter
James Dees Photo 6

James Dees

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James Dees Photo 7

James Dees

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James Dees Photo 8

James Dees

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Business Records

Name / Title
Company / Classification
Phones & Addresses
James W Dees
CREATIVE CONVERGENCE, LLC
James Dees
ABCHZ, LLC
James W Dees
ATM ON WHEELS, LLC
James W. Dees
MIDWEST ATM SERVICES, LLC
James E. Dees
President
James E. Dees, Inc
222 Dairy Rd, Auburndale, FL 33823
James W. Dees
President, Vice President
James W. Dees. Inc
9590 NW 52 Ct, Fort Lauderdale, FL 33351
James Dees
Director
International Medical Personnel, Inc
3111 Stirling Rd, Fort Lauderdale, FL 33312
James A. Dees
Managing
James Dees Carpentry LLC
Carpentry Contractor
5113 6 St, Zephyrhills, FL 33542

Publications

Us Patents

Propulsion System

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US Patent:
7997059, Aug 16, 2011
Filed:
Nov 23, 2010
Appl. No.:
12/952703
Inventors:
Gaofei Yan - Sunrise FL, US
James Dees - Sunrise FL, US
International Classification:
F02G 1/00
F02G 3/00
F02K 9/00
US Classification:
602001
Abstract:
A propulsion system for use in a liquid or gas fluid is provided including an axially-extending funnel-shaped conduit, a flow generator, a power source, and, optionally, an airfoil-shaped wing. The funnel-shaped conduit has outer walls forming an inner fluid passageway, an upper edge defining a fluid inlet, and a lower edge defining a fluid outlet. The optional airfoil-shaped wing is connected to and circumferentially surrounds the funnel-shaped conduit upper edge. The flow generator is rotatably mounted about the axis of the funnel-shaped conduit and is configured to force the fluid from the fluid inlet rearward through the fluid outlet. A forward force is produced by the combination of both thrust from the flow generator plus the lift force created as the flow generator draws the fluid across the annular airfoil-shaped wing and inwardly through the fluid inlet forcing the fluid rearward to exit out of the fluid outlet.

Self-Righting Frame And Aeronautical Vehicle

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US Patent:
8528854, Sep 10, 2013
Filed:
Apr 28, 2011
Appl. No.:
13/096168
Inventors:
Gaofei Yan - Sunrise FL, US
James Dees - Sunrise FL, US
International Classification:
B64C 27/08
US Classification:
244 1723, 244 1711, 244119, 446 36, 446 37
Abstract:
An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

Self-Righting Frame And Aeronautical Vehicle

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US Patent:
20140014767, Jan 16, 2014
Filed:
Sep 9, 2013
Appl. No.:
14/022213
Inventors:
Gaofei Yan - Hallandale FL, US
James Dees - Sunrise FL, US
International Classification:
B64C 1/00
B64C 27/10
US Classification:
244 1723, 244119
Abstract:
An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has an apex preferably at a top of a central vertical axis. The apex provides initial instability to begin a self-righting process when the vehicle is inverted on a surface. A lift and stabilization panel extends across an upper portion of said frame to provide lift, drag and/or stability. A propulsion system can be located within a central void of the frame assembly and oriented to provide a lifting force. An electronics assembly is also carried by the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a supporting surface. The frame provides self-righting functionality and protection of elements carried therein.

Propulsion System

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US Patent:
7836678, Nov 23, 2010
Filed:
Mar 25, 2008
Appl. No.:
12/054627
Inventors:
Gaofei Yan - Sunrise FL, US
James Dees - Sunrise FL, US
International Classification:
F02G 1/00
F02G 3/00
F02K 9/68
US Classification:
602001
Abstract:
A propulsion system for use in a liquid or gas fluid is provided including an axially-extending funnel-shaped conduit, a flow generator, a power source, and, optionally, an airfoil-shaped wing. The funnel-shaped conduit has outer walls forming an inner fluid passageway, an upper edge defining a fluid inlet, and a lower edge defining a fluid outlet. The optional airfoil-shaped wing is connected to and circumferentially surrounds the funnel-shaped conduit upper edge. The flow generator is rotatably mounted about the axis of the funnel-shaped conduit and is configured to force the fluid from the fluid inlet rearward through the fluid outlet. A forward force is produced by the combination of both thrust from the flow generator plus the lift force created as the flow generator draws the fluid across the annular airfoil-shaped wing and inwardly through the fluid inlet forcing the fluid rearward to exit out of the fluid outlet.

Self-Righting Aeronautical Vehicle And Method Of Use

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US Patent:
20230060888, Mar 2, 2023
Filed:
Sep 20, 2022
Appl. No.:
17/948500
Inventors:
Gaofei YAN - Hallandale FL, US
James DEES - Hallandale FL, US
International Classification:
B64C 1/06
A63H 33/00
A63H 27/00
A63H 15/06
B64C 17/00
B64C 1/08
A63H 30/04
B64C 27/10
B64C 1/00
B64C 17/02
B64C 39/02
B64D 47/08
G05D 1/08
B64C 27/20
G05D 1/00
Abstract:
An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

Self-Righting Aeronautical Vehicle And Method Of Use

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US Patent:
20200247522, Aug 6, 2020
Filed:
Feb 24, 2020
Appl. No.:
16/799799
Inventors:
Gaofei YAN - Hallandale FL, US
James Dees - Hallandale FL, US
International Classification:
B64C 1/06
G05D 1/00
B64C 27/20
G05D 1/08
B64D 47/08
B64C 39/02
B64C 17/02
B64C 1/00
B64C 27/10
A63H 30/04
B64C 1/08
B64C 17/00
A63H 15/06
A63H 27/00
A63H 33/00
Abstract:
An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

Self-Righting Aeronautical Vehicle And Method Of Use

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US Patent:
20190202542, Jul 4, 2019
Filed:
Oct 30, 2018
Appl. No.:
16/174353
Inventors:
Gaofei YAN - Hallandale FL, US
James Dees - Hallandale FL, US
International Classification:
B64C 1/06
B64C 1/00
G05D 1/00
A63H 30/04
B64C 1/08
B64C 17/00
A63H 15/06
A63H 27/00
A63H 33/00
B64C 27/20
G05D 1/08
B64C 27/10
B64C 17/02
B64D 47/08
B64C 39/02
Abstract:
An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

Self-Righting Aeronautical Vehicle And Method Of Use

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US Patent:
20180057135, Mar 1, 2018
Filed:
Aug 8, 2017
Appl. No.:
15/672262
Inventors:
Gaofei YAN - Hallandale FL, US
James Dees - Hallandale FL, US
International Classification:
B64C 1/06
A63H 33/00
A63H 27/00
A63H 15/06
B64C 17/00
B64C 1/00
A63H 30/04
B64C 27/10
B64C 1/08
Abstract:
A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to self-right the vehicle. The frame can include sealed, hollowed sections for use in bodies of water. The frame can be spherical in shape enabling inspection of internal surface of partially or fully enclosed structures. Inspection equipment can be integrated into the vehicle and acquired data can be stored or wireles sly communicated to a server. A controlled or other mass can be pivotally assembled to a pivot axle spanning across the interior of the frame. The pivot axis can rotate about a vertical axis (an axis perpendicular to the elongated axis). The propulsion mechanisms can be adapted for use as a terrestrial vehicle when enclosed in a sealed spherical shell.

Wikipedia

James Parker Dees

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James Parker Dees was the founder and first bishop of the Anglican Orthodox Church and the Orthodox Anglican Communion. Dees was born in Greenville, North

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James A Dees from Zephyrhills, FL, age ~65 Get Report