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Herman M Drees

from Thousand Oaks, CA
Age ~74
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Also known as:
Herman H Drees, Karen M Drees, Herman M Dress, Herman Rees, Dress Herman
Phone and address:
2570 Manchester Ct, Thousand Oaks, CA 91362
(805) 493-9045
Related to:
Jan B Drees, 43Jearle M Karen, 67Jan DreesSherri A Jeakle, 65Willem Drees, 42Carolyn Drees, 72
Connected to:
Bryan S Drees, 28Carrie A Drees, 42Cristi Drees, 50Danielle N Drees, 34Diana C Drees, 84Douglas A Drees, 53Glenn R Drees, 56Jeffrey J Drees, 50Joyce M Drees, 62Judith A Drees, 61

Herman Drees Phones & Addresses

  • 2570 Manchester Ct, Thousand Oaks, CA 91362 (805) 493-9045
  • Westlake Village, CA
  • Austin, TX
  • Simi Valley, CA
  • Milledgeville, GA
  • Federal Way, WA
  • Lovettsville, VA

Work

Company: Nerak inc. Position: President

Industries

Information Services

Resumes

Resumes

Herman Drees Photo 1

President

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Location:
2570 Manchester Ct, Thousand Oaks, CA 91362
Industry:
Information Services
Work:
NERAK Inc.
President

Business Records

Name / Title
Company / Classification
Phones & Addresses
Herman Drees
President
NERAK, INC
Nonclassifiable Establishments
1800 Bridgegate St STE 102, Westlake Village, CA 91361
Herman Drees
Secretary
DUTCH ENERGY CORPORATION
Farm Management Services
1800 Bridgegate St #102, Westlake Village, CA 91361
12121 Wilshire Blvd, Los Angeles, CA 90025
1840 Bridgegate St, Westlake Village, CA 91361
(805) 497-7107

Publications

Us Patents

Passively Stable Hovering System

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US Patent:
50820796, Jan 21, 1992
Filed:
May 4, 1990
Appl. No.:
7/519015
Inventors:
Peter B. S. Lissaman - Altadena CA
Herman M. Drees - Simi Valley CA
Charles J. Sink - Simi Valley CA
William D. Watson - Simi Valley CA
Assignee:
Aerovironment, Inc. - Monrovia CA
International Classification:
B60V 111
B64C 2900
US Classification:
180118
Abstract:
A flight system capable of passively stable hover comprises an apparatus defining a vertical axis, and including multiple upright ducts spaced about the axis; fluid momentum generators in the ducts to effect flow of fluid downwardly in the ducts; and fluid flow deflector structure in the path of the downwardly flowing fluid, and angled to deflect the fluid flow away from the axis, in such manner as to provide stability in hover of the apparatus.

Rotary Aircraft Passively Stable In Hover

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US Patent:
52977595, Mar 29, 1994
Filed:
Apr 6, 1992
Appl. No.:
7/863998
Inventors:
Neil Tilbor - Medford NJ
Herman M. Drees - Simi Valley CA
William D. Watson - Simi Valley CA
Charles J. Sink - Simi Valley CA
Jeffrey Corsiglia - Malibu CA
Warren E. Bosch - Mount Laurel NJ
International Classification:
B64C 2700
US Classification:
244 1711
Abstract:
A rotary aircraft includes a cylindrically tubular hub mounting a plurality of outwardly extending, resiliently flexible blades. The blades are uniformly spaced around the hub and its central axis and fixed in pitch. Outer tips on each of the blades are downwardly turned and outwardly turned sufficiently to balance the lift generated by the blades from air striking the aircraft horizontally when the aircraft is in hover to provide passive stability to the aircraft. A pair of propellered electric motors are mounted on a diametrically opposing pair of the blades, pitched transversely to the central axis of the hub and to a plane perpendicular to the central axis, to simultaneously provide both lift and rotation. A battery supplies all power used by the aircraft while radio control circuitry in the hub permits variation of the power supplied to the motors for altitude control of the aircraft.

Passively Stable Hovering System

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US Patent:
50709550, Dec 10, 1991
Filed:
Sep 17, 1990
Appl. No.:
7/583477
Inventors:
Peter B. S. Lissaman - Altadena CA
Herman M. Drees - Simi Valley CA
Charles J. Sink - Simi Valley CA
William D. Watson - Simi Valley CA
Assignee:
Aerovironment, Inc. - Monrovia CA
International Classification:
B60V 111
B60V 114
US Classification:
180117
Abstract:
A flight system capable of passively stable hover and horizontal translatory flight, comprises an apparatus defining a vertical axis, and including multiple ducts with substantially vertical axes in hover mode, spaced the axis; fluid momentum generators in the ducts to effect flow of fluid downwardly in the ducts in hover; and fluid flow deflector structure in the path of the flowing duct fluid, and angled to deflect the fluid flow away from the axis, in such manner as to provide stability in hover of the apparatus, as well as stability when the entire device is tilted through approximately 90. degree. to execute horizontal translatory flight.
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Herman M Drees from Thousand Oaks, CA, age ~74 Get Report