The invention relates to a device for controlling armature solenoid provided with a DC voltage source (14), at least one buffer capacitor (18), which is connected in parallel to the DC voltage source (14) and has a known capacitance (C), and a first switch (28), which is arranged between the DC voltage source (14) and the buffer capacitor (18). The exciter coil (16) and a second switch (30) arranged in series therewith are connected in parallel to the buffer capacitor (18). A control and evaluation unit (22), when the buffer capacitor (18) is charged, opens the first switch (28) and closes the second switch (30) in order to determine, on the basis of the measurement voltage (20), the frequency of the resonant circuit having the capacitance (C) of the buffer capacitor (18) and the inductance (L) of the armature solenoid (12). The inductance (L) of the armature solenoid (12) is determined on the basis of the frequency, and the air gap width (h) of the armature solenoid (12) is determined on the basis of the inductance. The PWM control signal with which the armature solenoid (12) is operable in order to generate a predefined force to be applied by the armature solenoid (12) is applied to the second switch (30) on the basis of a look-up table or a mathematical modelling of the electromagnetic behavior of the armature solenoid (12).

A military vehicle includes an engine, an energy storage system, an accessory drive coupled to the engine and including an air compressor and a first motor, a second motor coupled to an axle, and a clutch positioned between the engine and the second motor. The clutch is spring-biased into engagement with the engine and pneumatically disengaged by an air supply selectively provided thereto based on operation of the air compressor. In an engine mode, (i) the clutch does not receive the air supply such that the engine is coupled to the second motor and (ii) the engine drives (a) the accessory drive and (b) the axle through the second motor. In the electric mode, (i) the first motor drives the air compressor to compress air to facilitate supplying the air supply to the clutch to disengage the clutch and decouple the engine from the second motor and (ii) the second motor drives the axle.

Disclosed is an electrically motorised wheel, transmission and control module, kit, vehicle and system. The electrically motorised wheel 100 is configured to releasably couple to a non-motorised wheeled vehicle. The electrically motorised wheel 100 includes: a ground engaging assembly 110; a coupling assembly 125 for releasably coupling the electrically motorised wheel to an axle 2000 of the vehicle 2700; and a housing 1902 configured to house: an electric motor 560 operatively coupled to the ground engaging assembly 110; a control system 505 including or coupled to an inertial measurement unit 540, which is stationary within the housing 1902 during motorised rotation of the electrically motorised wheel 100, and a controller 510 configured to control operation of the electric motor 560 based one or more sensor signals received from the inertial measurement unit 540; and a power source 520 electrically connected to the control system 505 and the electric motor 560.

A first movable member for pivotally shifting to a predetermined position in conjunction with a pivotal operation of a shift lever, and a permanent magnet section disposed so as to face the first movable member are included whereby the shift lever is provided with a click feeling given by an attraction force acting between the first movable member and the permanent magnet section. The permanent magnet section is magnetized such that in a thickness direction, an N pole and an S pole are created by magnetization in a series arrangement, and such that in a width direction, an S pole is created by magnetization alongside the N pole and an N pole is created by magnetization alongside the S pole created by magnetization in the thickness direction.

A driveline includes a driver configured to be positioned between an engine and a transmission. The driver includes a housing, a motor/generator, and a clutch. The housing includes an engine mount configured to couple to the engine and a backing plate configured to couple to the transmission. The motor/generator is disposed within the housing and configured to couple to an input of the transmission. The clutch is disposed within the housing and coupled to the motor/generator. The clutch is configured to selectively couple an output of the engine to the motor/generator. The clutch is configured to be spring-biased into engagement with the engine and pneumatically disengaged by an air supply selectively provided thereto.

A military vehicle includes a chassis, a front end accessory drive (FEAD), and circuitry. The chassis includes an engine and an integrated motor generator (IMG). The FEAD includes multiple accessories and an electric motor-generator. The circuitry is configured to operate the military vehicle according to different modes. The circuitry is configured to receive a user input indicating a selected mode of the modes, and operate the chassis and the FEAD of the military vehicle according to the selected mode. The modes include an engine mode and an electric mode. In the engine mode, the engine drives the FEAD and the tractive elements of the military vehicle through the IMG for transportation. In the electric mode, the engine is shut off to reduce a sound output of the military vehicle and the IMG drives the tractive elements of the military vehicle for transportation and the electric motor-generator drives the FEAD.

An auxiliary power take-off assembly (32) for a transmission (6) of a motor vehicle (2) having a torque converter (8). A driveshaft (30) is permanently connected to a drive motor (4), via the pump shaft (24) of the torque converter (8). In addition, the auxiliary power take-off assembly (32) has a transmission drive chain which includes at least a drive input element (34) and a drive output element (42) connected to an additional assembly (66) to be driven, and a shifting element (64, 68). The shifting element (64, 68) is functionally arranged between the driveshaft (30) and the drive input element (34) of the transmission chain for the optionally connecting the driveshaft (30) to the drive input element (34).

Methods and systems are provided for a disconnect assembly in an electric drive unit. In one example, the system includes a dog clutch positioned in a differential, configured to selectively mechanically decouple an electric motor from one or more drive wheels, and including a first interface designed to selectively engage a second interface. In such an example, each of the first interface and the second interface include a plurality of teeth, each tooth in the plurality of teeth includes a drive flank and a coast flank, and the coast flank has a first tooth angle greater than a second tooth angle of the drive flank.

A front end accessory drive (FEAD) for a military vehicle. The FEAD includes a first belt, a second belt, multiple accessories, an electric motor-generator, at least one other accessory, and a sprag clutch. The accessories and the electric motor-generator are coupled with the first belt. The at least one other accessory, the first belt, and the second belt are coupled with the sprag clutch. The second belt is configured to couple with an output shaft of an engine of the military vehicle and be driven by the output shaft of the engine to drive the sprag clutch. The sprag clutch is thereby configured to drive the at least one other accessory and the first belt, and the first belt is thereby configured to drive the plurality of accessories, and the electric motor-generator.

A signal system for a vehicle has a vehicle mount that is configured to be attached to the vehicle. A power source is arranged through the vehicle mount and electrically coupled to a vehicle power source. A solenoid is electrically coupled to the power source and mechanically coupled to a spring. An arrow main pole is mechanically coupled to the spring, a first head blade and a second head blade. A solenoid controller is electrically coupled to the solenoid. Activating the solenoid controller engages the spring to rotate the arrow main pole approximately 180 degrees in a first direction into an expanded arrangement. Collapsing of this expanded arrangement by hand reloads the rotational energy back into the springs that can produce a future expanded arrangement.