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Greg B Vulikh

from Redwood City, CA
Age ~35
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Also known as:
Gregory Vulikh, Gregory Vulika
Phone and address:
988 Haven Ave, Redwood City, CA 94063
Related to:
Boris VulikhYefim HRebecca Vulikh, 29Boris HPolina Vulikh, 30
Connected to:
Sudhakar Vulimiri, 69Bruno Vulin, 63Lisa Vulin, 54Tanja V Vulin, 44Leeanna R Vuljanic, 44Stacey Vulku, 33Jacob M Vullo, 48Jennifer B Vullo, 72Judiann C Vullo, 72Lisa Y Vullo, 43

Greg Vulikh Phones & Addresses

  • 988 Haven Ave, Redwood City, CA 94063
  • Lynn, MA
  • 15 Oakledge Rd, Swampscott, MA 01907 (781) 775-7022
  • Beverly, MA
  • 15 Oakledge Rd, Swampscott, MA 01907

Professional Records

License Records

Greg Vulikh

Address:
Swampscott, MA 01907
License #:
23355
Issued Date:
Mar 12, 2012
Type:
Engineer in Training

Publications

Us Patents

Modular Miniature Unmanned Aircraft With Vectored-Thrust Control

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US Patent:
20130175390, Jul 11, 2013
Filed:
Aug 4, 2012
Appl. No.:
13/567015
Inventors:
Adam Woodworth - Melrose MA, US
James Peverill - Canton MA, US
Greg Vulikh - Manassas VA, US
Jeremy Hollman - Manassas VA, US
Assignee:
AURORA FLIGHT SCIENCES CORPORATION - Manassas VA
International Classification:
B64D 27/26
B64C 19/00
B64D 9/00
US Classification:
244 54, 2441371, 244 751
Abstract:
An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.

Modular Miniature Unmanned Aircraft With Vectored-Thrust Control

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US Patent:
20140054423, Feb 27, 2014
Filed:
Jul 30, 2013
Appl. No.:
13/954218
Inventors:
James Peverill - Canton MA, US
Greg Vulikh - Manassas VA, US
Jeremy Scott Hollman - Manassas VA, US
International Classification:
B64D 27/26
B64C 39/02
US Classification:
244 23 D
Abstract:
An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.

Modular Miniature Unmanned Aircraft With Vectored-Thrust Control

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US Patent:
20140061384, Mar 6, 2014
Filed:
Jul 30, 2013
Appl. No.:
13/954278
Inventors:
James Peverill - Canton MA, US
Greg Vulikh - Manassas VA, US
Jeremy Scott Hollman - Manassas VA, US
International Classification:
B64C 1/30
US Classification:
244120
Abstract:
An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.

Modular Miniature Unmanned Aircraft With Vectored-Thrust Control

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US Patent:
20140061390, Mar 6, 2014
Filed:
Jul 30, 2013
Appl. No.:
13/954362
Inventors:
James Peverill - Canton MA, US
Greg Vulikh - Manassas VA, US
Jeremy Scott Hollman - Manassas VA, US
International Classification:
B64C 15/00
US Classification:
244 23 D
Abstract:
An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.

Electrical System For Unmanned Aerial Vehicles

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US Patent:
20180186464, Jul 5, 2018
Filed:
Dec 30, 2016
Appl. No.:
15/395996
Inventors:
- Mountain View CA, US
Greg Vulikh - Redwood City CA, US
John FitzSimons - San Jose CA, US
International Classification:
B64D 31/06
B64C 39/02
B64D 27/24
H02P 5/00
Abstract:
An example unmanned aerial vehicle includes a power source, a processor module having one or more processors, and a plurality of boom arms, each boom arm being couplable to a printed circuit board (PCB) and a plurality of propellers. In the example UAV, a PCB of each boom arm includes a power hub electrically couplable to the power source and to corresponding propellers of the boom arm, and a signal hub electrically couplable to at least one processor of the processor module and to the corresponding propellers. Further, in the example UAV, the power hub of each PCB is configured to transfer power from the power source to the corresponding propellers, and wherein the signal hub of each PCB is configured to transfer signals from the processor module to the corresponding propellers such that the processor module controls the plurality of propellers.
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Greg B Vulikh from Redwood City, CA, age ~35 Get Report