GENERATORS USE AS AUXILIARY

Brand Owner (click to sort) Address Description
ERX Hyliion Inc. Suite 100 1202 BMC Drive Cedar Park TX 78613 Generators for use as auxiliary power sources for electric land vehicles;Powertrains and drivetrains for land vehicles; Electric powertrains and drivetrains for land vehicles; motors for use as auxiliary power sources for electric land vehicles; hybrid systems for vehicles, namely, axles with regenerative brakes, batteries and electric motors for trucks and trailers; fuel efficiency technology for land vehicles, namely, axles with regenerative brakes, batteries, and electric motors;
HYLIION HYPERTRUCK Hyliion Inc. Suite 100 1202 BMC Drive Cedar Park TX 78613 Generators for use as auxiliary power sources for electric land vehicles;HYLIION HYPER TRUCK;Electric trucks; Range extended electric trucks; Electrically-powered motor vehicles; Powertrains and drivetrains for land vehicles; Electric powertrains and drivetrains for land vehicles; Motors for use as auxiliary power sources for electric land vehicles; Hybrid systems for vehicles, namely, axles with regenerative brakes, batteries and electric motors for trucks and trailers; Fuel efficiency technology for land vehicles, namely, axles with regenerative brakes, batteries, and electric motors;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. A vertical take-off and landing aircraft is provided with a plurality of thrust generators which generate thrust substantially vertically upward with respect to the aircraft; a first prime mover which drives the thrust generators, and an occupant seat. At least one of the thrust generators is disposed at either a front section of the aircraft or a rear section of the aircraft, and the remaining thrust generator or thrust generators are disposed at either the rear section or the front section, whichever the at least one of the thrust generators is not disposed at. The prime mover and a sitting surface of the occupant seat are disposed between the at least one of the thrust generators at the front section of the aircraft and the at least one of the thrust generators at the rear section of the aircraft, and in a position lower than all of the thrust generators. The center of gravity of the vertical take-off and landing aircraft is below the center of the aircraft and hangs down when the aircraft is in flight due to the thrust generated by the thrust generators.