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Allen Gerbino Phones & Addresses

  • Lakewood, CA
  • Adelanto, CA
  • 4235 Donald Douglas Dr, Long Beach, CA 90808
  • Signal Hill, CA
  • Burbank, CA
  • Irvine, CA
  • San Bernardino, CA

Business Records

Name / Title
Company / Classification
Phones & Addresses
Allen J. Gerbino
Director, President
Grey Fox Group
2549 N Palm Dr, Long Beach, CA 90755
Allen J. Gerbino
President
DARKHORSE GROUP
4235 Donald Douglas Dr, Long Beach, CA 90808
Allen J. Gerbino
Director, President, Secretary, Treasurer
Aarc-Seair, Inc
4235 E Donald Douglas Dr, Long Beach, CA 90808
2549 N Palm Dr, Long Beach, CA 90755
Allen G. Gerbino
Secretary, Treasurer
Tri-Star Helicopters, Inc
6492 S St, Lakewood, CA 90713
Allen J. Gerbino
Director, President, Secretary, Treasurer
Swing Wing Central
4235 E Donald Douglas Dr, Long Beach, CA 90808
2549 N Palm Dr, Long Beach, CA 90755
Allen J. Gerbino
Director, President, Secretary, Treasurer
Helicopters "R" US
2549 N Palm Dr, Long Beach, CA 90755
4235 E Donald Douglas Dr, Long Beach, CA 90808
Allen J. Gerbino
Director, President, Secretary, Treasurer
Helicopter Haven, Inc
4235 E Donald Douglas Dr, Long Beach, CA 90808
2549 N Palm Dr, Long Beach, CA 90755
Allen J. Gerbino
President, Director, President, Secretary, Treasurer
TANK ONE, INC
Whol Photo Equipment/Supplies
2549 N Palm Dr, Signal Hill, CA 90755

Publications

Us Patents

Retractable Lifting Blades For Aircraft

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US Patent:
7475847, Jan 13, 2009
Filed:
Dec 22, 2005
Appl. No.:
11/317855
Inventors:
Allen J. Gerbino - Long Beach CA, US
International Classification:
B64C 27/52
US Classification:
244 1725
Abstract:
A rotor blade assembly for providing vertical lift to an aircraft, having a rotor head and a plurality of blades, with each blade attached to a mechanism such as a cam surface, whereby movement of the mechanism causes the radial distance between the distal tip of the attached blade and the center of the rotor head to alter, decreasing or increasing the length of the lifting surface. The blades are moved from a fully extended position providing maximum lift, to a retracted position in which the blades are removed from the airstream. The pitch of the blades may be controlled by a pitch controller to achieve full helicopter responsiveness. A plurality of bladeletts may be positioned near the outer periphery of the rotor head. When they are moved into the airstream, passing air impacts the bladeletts exerting a pressure, causing rotational movement of the rotor blade assembly.

Retractable Lifting Blades For Aircraft

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US Patent:
8523103, Sep 3, 2013
Filed:
Dec 17, 2008
Appl. No.:
12/337189
Inventors:
Allen J. Gerbino - Signal Hill CA, US
International Classification:
B64C 27/52
US Classification:
244 1725
Abstract:
A rotor blade assembly for providing vertical lift to an aircraft, having a rotor head and a plurality of blades, with each blade attached to a mechanism such as a cam surface, whereby movement of the mechanism causes the radial distance between the distal tip of the attached blade and the center of the rotor head to alter, decreasing or increasing the length of the lifting surface. The blades are moved from a fully extended position providing maximum lift, to a retracted position in which the blades are removed from the airstream. The pitch of the blades may be controlled by a pitch controller to achieve full helicopter responsiveness. A plurality of bladeletts may be positioned near the outer periphery of the rotor head. When they are moved into the airstream, passing air impacts the bladeletts exerting a pressure, causing rotational movement of the rotor blade assembly.

Retractable Lifting Blades For Aircraft

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US Patent:
20040144892, Jul 29, 2004
Filed:
Sep 9, 2003
Appl. No.:
10/657838
Inventors:
Allen Gerbino - Long Beach CA, US
International Classification:
B64C027/00
US Classification:
244/017110
Abstract:
A rotor blade assembly for providing vertical lift to an aircraft, having a rotor head and a plurality of blades, with each blade attached to a mechanism such as a cam surface, whereby movement of the mechanism causes the radial distance between the distal tip of the attached blade and the center of the rotor head to alter, decreasing or increasing the length of the lifting surface. The blades are moved from a fully extended position providing maximum lift, to a retracted position in which the blades are removed from the airstream. The pitch of the blades may be controlled to achieve full helicopter responsiveness. A plurality of bladeletts may be positioned near the outer periphery of the rotor head. When they are moved into the airstream, passing air impacts the bladeletts exerting a pressure, causing rotational movement of the rotor blade assembly.
Allen J Gerbino from Lakewood, CA, age ~86 Get Report