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Jesse S Blake, Age 46Baltimore, MD

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Known as:
Jesse Starnes Blake Jesse Starn Blake Jess E Blake Jesse Lake

Jesse Blake Phones & Addresses

Baltimore, MD

Ellicott City, MD

Alameda, CA

Warrenton, OR

Springville, UT

San Francisco, CA

Salt Lake City, UT

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Jesse Blake resumes & CV records

Resumes

Jesse Blake Photo 42

Lead Outsourcing Manager

Location:
Towson, MD
Industry:
Motion Pictures And Film
Work:
Zenimax Online Studios
Lead Outsourcing Manager Thq Kaos Studios Sep 2010 - Oct 2010
Contract Artist Mindwalk Studios - 曼德沃克工作室 May 2009 - Mar 2010
Character Lead and Project Manager Stormfront Studios Jul 2005 - Mar 2008
3D Modeler Page 44 Studios 2005 - 2005
3D Modeler
Education:
Academy of Art University 2000 - 2003
Bachelors, Bachelor of Arts University of Utah 1996 - 2000
Skills:
Game Development, 3D Modeling, Maya, Uv Mapping, Xbox 360, Video Games, Computer Games, Modeling, Ps3, 3D Studio Max, Mmo, Casual Games, Perforce, Gameplay, Digital Painting, Art, Concept Design
Jesse Blake Photo 43

Jesse Blake

Location:
Baltimore, Maryland Area
Industry:
Motion Pictures and Film

Publications & IP owners

Us Patents

Loading Structure With Tether Guide For Unmanned Aerial Vehicle

US Patent:
2021026, Sep 2, 2021
Filed:
Nov 22, 2020
Appl. No.:
17/100930
Inventors:
- Mountain View CA, US
Jesse Blake - Sunnyvale CA, US
André Prager - Sunnyvale CA, US
Evan Twyford - Mountain View CA, US
International Classification:
B64D 1/22
B64C 39/02
Abstract:
A payload loading system is disclosed. The payload loading system includes a UAV and a loading structure. A retractable tether is coupled to a payload coupling apparatus at a distal end and the UAV at a proximate end. A payload is loaded to the UAV by coupling the payload to the payload coupling apparatus. The loading structure of the payload loading system includes a landing platform and a tether guide. The tether guide is coupled to the landing platform and directs the tether as the UAV approaches and travels across at least a portion of the landing platform such that the payload coupling apparatus arrives at a target location. The payload is loaded to the payload coupling apparatus while the payload coupling apparatus is within the target location.

Loading Structure With Tether Guide For Unmanned Aerial Vehicle

US Patent:
2019037, Dec 12, 2019
Filed:
Jun 11, 2018
Appl. No.:
16/005288
Inventors:
- Mountain View CA, US
Jesse Blake - Sunnyvale CA, US
André Prager - Sunnyvale CA, US
Evan Twyford - Mountain View CA, US
International Classification:
B64D 1/22
B64C 39/02
Abstract:
A payload loading system is disclosed. The payload loading system includes a UAV and a loading structure. A retractable tether is coupled to a payload coupling apparatus at a distal end and the UAV at a proximate end. A payload is loaded to the UAV by coupling the payload to the payload coupling apparatus. The loading structure of the payload loading system includes a landing platform and a tether guide. The tether guide is coupled to the landing platform and directs the tether as the UAV approaches and travels across at least a portion of the landing platform such that the payload coupling apparatus arrives at a target location. The payload is loaded to the payload coupling apparatus while the payload coupling apparatus is within the target location.

Assembly Systems And Methods For Unmanned Aerial Vehicles

US Patent:
2019016, May 30, 2019
Filed:
Nov 27, 2017
Appl. No.:
15/823114
Inventors:
- Mountain View CA, US
Adem Rudin - Mountain View CA, US
Stephen Benson - San Carlos CA, US
James Schmalzried - San Jose CA, US
Kyle Liske - San Francisco CA, US
Jesse Blake - Sunnyvale CA, US
André Prager - Sunnyvale CA, US
Nicolas Renold - Mountain View CA, US
Thorsten Schilling - Cupertino CA, US
International Classification:
B64C 1/06
Abstract:
Systems and methods for assembling Unmanned Autonomous Vehicle (UAV) are disclosed herein. In one embodiment, a method for assembling a UAV includes connecting a wing spar with boom carriers to form an H-frame. The wing spar provides mounting locations for securing horizontal propulsion units, and the boom carriers provide mounting locations for securing vertical propulsion units. The method also includes attaching a fuselage body to the wing spar; attaching a pre-formed wing shell to the H-frame; and attaching pre-formed individual boom shells to their corresponding boom carriers. The H-frame provides structural frame for mounting the wing shell and the boom shells.

Uav Group Charging Based On Demand For Uav Service

US Patent:
2019012, May 2, 2019
Filed:
Oct 26, 2017
Appl. No.:
15/794925
Inventors:
- Mountain View CA, US
Jesse Blake - Sunnyvale CA, US
International Classification:
B60L 11/18
H02J 7/00
G05D 1/10
G08G 5/00
B64C 39/02
Abstract:
Example embodiments can help to more efficiently charge unmanned aerial vehicles (UAVs) in a plurality of UAVs that provide delivery services. An example method includes: determining demand data indicating demand for item-transport services by the plurality of UAVs during a period of time; determining battery state information for the plurality of UAVs, wherein the battery state information is based at least in part on individual battery state information for each of two or more of the UAVs; based at least in part on (a) the demand data for item-transport services by the plurality of UAVs, and (b) the battery state information for the fleet of UAVs, determining respective charge-rate profiles for one or more of the UAVs; and sending instructions to cause respective batteries of the one or more of the UAVs to be charged according to the respectively determined charge-rate profiles.

Systems For Charging Aerial Vehicles

US Patent:
2019002, Jan 24, 2019
Filed:
Jul 19, 2017
Appl. No.:
15/654644
Inventors:
- Mountain View CA, US
Matthew Nubbe - Mountain View CA, US
Jim Schmalzried - Mountain View CA, US
Jesse Blake - Mountain View CA, US
Scott Velez - Mountain View CA, US
Dustin Sanders - Mountain View CA, US
Stephen Benson - Mountain View CA, US
Evan Twyford - Mountain View CA, US
International Classification:
B60L 11/18
B64F 1/00
B64F 1/02
B64C 39/02
Abstract:
An example embodiment includes a landing pad having a housing and a power terminal configured to draw electric power from a power source. The landing pad further includes an electrically conductive landing terminal dorsal to the housing and configured such that, during a landing state of an aerial vehicle, the landing terminal makes contact with a plurality of electric contacts disposed ventrally to a fuselage of the aerial vehicle. The landing terminal is configured to transfer electric power drawn by the power terminal to the aerial vehicle via the electric contacts during the landing state of the aerial vehicle.

Possible Relatives

D Blake  Deanna L Blake  Damon Blake  Dana H Blake  Daniel R Blake  Delbert C Blake  Della M Blake  Jesse A Johnston  Jesse J Stanton  Jesse W Stark 

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