TL;DR: In this article, an electromagnetic clutch is engaged when the rotation rate of the compression unit and the engine rotation rate match, to switch from motor drive to engine drive during engine startup or engine acceleration.
Abstract: In order to achieve a smooth shift between two drive sources, an electromagnetic clutch is engaged, when the rotation rate of the compression unit and the engine rotation rate match, to switch from motor drive to engine drive during engine startup or engine acceleration. The motor is driven before the electromagnetic clutch is cut off to switch from engine rive to motor drive during engine stop or engine deceleration.
TL;DR: In this paper, a vehicle-starting engine torque restricting device is proposed to restrict engine torque upon starting of a vehicle with an engine used as a vehicle drive power source, so that a required output of a first electric motor which generates a reaction force corresponding to the engine torque can be made smaller than when engine torque is not restricted.
Abstract: A vehicle-starting-engine-torque restricting device is provided to restrict engine torque upon starting of a vehicle with an engine used as a vehicle drive power source, so that a required output of a first electric motor which generates a reaction force corresponding to the engine torque can be made smaller than when the engine torque is not restricted. Namely, the vehicle-starting-engine-torque restricting device eliminates a need of increasing the maximum output of the first electric motor to generate the reaction force corresponding to the engine torque, making it possible to reduce the required size of the first electric motor.
TL;DR: In this paper, reaction engine control systems employing relatively moveable plug-cowl configurations with associated control systems are described for providing control of thrust direction and magnitude, engine operating conditions, missile kinematics, and other parameters of liquid and solid propellant rockets.
Abstract: Missile configurations with engine and propellant control systems are the subject of this application together with weapons and navigational techniques employing same. Reaction engine control systems employing relatively moveable plug-cowl configurations with associated control systems are described herein for providing control of thrust direction and magnitude, engine operating conditions, missile kinematics, and other parameters of liquid and solid propellant rockets.
TL;DR: A reaction engine driven electrical generating system comprising an electrical generator having an armature and a reaction engine that is driven to rotate the armature for generating electricity is described in this paper, where the reaction engine drive includes a generally cylindrical housing with an internal truncated cone which internally divides the housing into two sections.
Abstract: A reaction engine driven electrical generating system comprising an electrical generator having an armature and a reaction engine driven to rotate the armature for generating electricity. The reaction engine drive includes a generally cylindrical housing with an internal truncated cone which internally divides the housing into two sections. A drive shaft extends generally horizontally into the housing and a reaction force rotation unit carrying a plurality of reaction engines is mounted upon the drive shaft. An enlarged air port is fashioned within one end of the housing and cooperates with an air inlet disc fixedly connected to the drive shaft. A plurality of air inlet aperatures extend through the air inlet disc and air conduits connect the inlet aperatures directly to corresponding intakes of said plurality of reaction engines. A monitor is operably connected to the armature or drive shaft and serves to provide a readout of speed of rotation of the drive shaft and generator armature. A fuel control is then modulated by the speed monitor to control the fuel flow to the reaction engines and maintain a generally constant armature speed over varying conditions of electrical load.