F02N7/08

Air turbine starter
10815897 · 2020-10-27 · ·

An air turbine starter for starting an engine, comprising a housing defining an inlet, an outlet, and a flow path extending between the inlet and the outlet for communicating a flow of gas there through. A turbine member is journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas. A gear box includes a gear train coupled with the turbine member. A gear box housing at least partially defines an interior having an open face and a body at least partially closes the open face.

Method for starting an internal combustion engine
10794352 · 2020-10-06 · ·

A method for starting an internal combustion engine by a compressed air starting system, in which in a first starting sequence the engagement of the starter is brought about by compressed air, a decompression valve for relieving the cylinder working space is acted on in the opening direction, and starting of the internal combustion engine is initiated by pulsed compressed air being applied to the starter. In a second starting sequence the decompression valve is acted on in the closing direction, and constant compressed air is applied to the starter.

Motor vehicle combustion engine starter with air vent opening

The invention relates mainly to a starter (11) for a motor vehicle combustion engine, comprising: an electric motor (15), a drive pinion (60), a pinion body (61) on which said drive pinion (60) is mounted, a drive shaft (12) able to transmit a torque derived from the electric motor (15) to the drive pinion (60) via the pinion body, the pinion body (61) being mounted with the ability to slide axially with respect to the drive shaft (12), and in which, with there being a chamber (86) delimited notably by one end of the drive shaft (12) and one end of the pinion body (61) opposite the end of the drive shaft (12), the chamber (86) is vented via a through-opening (85) made in an annular wall of the drive shaft (12) or of the pinion body (61).

System and method for cranking an engine

A system and method includes a secondary energy storage system (SESS) and a control system. The SESS is configured to be disposed onboard a vehicle and conductively connected via switch devices to a primary battery and a cranking device of the vehicle. The control system is configured to control the switch devices to close a conductive path to discharge electric current from the SESS for powering the cranking device to rotate an engine shaft during a cranking operation. The control system is configured to control the switch devices to open the conductive path and prevent discharge of electric current from the SESS after the cranking operation is complete.

Air turbine starter

An air turbine starter for starting an engine, comprising a housing defining an inlet, an outlet, and a flow path extending between the inlet and the outlet for communicating a flow of gas there through. A turbine member is journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas. A secondary supply port is fluidly coupled to the flow of the pressurized gas in the housing.

Air starter and methods for determining hydrostatic lock

Air starter and methods for determining hydrostatic lock in a combustion engine during a start sequence with an air starter, including during the start sequence of the combustion engine, monitoring a speed parameter indicative of a rotational speed of the turbine air starter and a pressure parameter indicative of an inlet air pressure of the turbine air starter, and determining that a hydrostatic lock condition exists in the combustion engine based on both the speed threshold and the pressure threshold.

Air starter and methods for determining hydrostatic lock

Air starter and methods for determining hydrostatic lock in a combustion engine during a start sequence with an air starter, including during the start sequence of the combustion engine, monitoring a speed parameter indicative of a rotational speed of the turbine air starter and a pressure parameter indicative of an inlet air pressure of the turbine air starter, and determining that a hydrostatic lock condition exists in the combustion engine based on both the speed threshold and the pressure threshold.

METHOD FOR STARTING AN INTERNAL COMBUSTION ENGINE
20190277238 · 2019-09-12 ·

A method for starting an internal combustion engine by a compressed air starting system, in which in a first starting sequence the engagement of the starter is brought about by compressed air, a decompression valve for relieving the cylinder working space is acted on in the opening direction, and starting of the internal combustion engine is initiated by pulsed compressed air being applied to the starter. In a second starting sequence the decompression valve is acted on in the closing direction, and constant compressed air is applied to the starter.

Hydraulic device configured as a starter motor

A hydraulic device is disclosed. The hydraulic device can include a rotor, a plurality of vanes and a ring. The ring can include a suction cavity and a pressure cavity. The suction cavity and pressure cavity can be configured for ingress and egress of a hydraulic fluid through the ring. The ring can include a suction port defined entirely by the ring and in fluid communication with the suction cavity. The suction port can be configured to receive hydraulic fluid from a first region between the ring and the rotor. The ring can include a pressure port defined entirely by the ring and in fluid communication with the pressure cavity. The pressure port can be configured to allow for passage of the hydraulic fluid from the pressure cavity to a second region between the ring and the rotor.

Hydraulic device configured as a starter motor

A hydraulic device is disclosed. The hydraulic device can include a rotor, a plurality of vanes and a ring. The ring can include a suction cavity and a pressure cavity. The suction cavity and pressure cavity can be configured for ingress and egress of a hydraulic fluid through the ring. The ring can include a suction port defined entirely by the ring and in fluid communication with the suction cavity. The suction port can be configured to receive hydraulic fluid from a first region between the ring and the rotor. The ring can include a pressure port defined entirely by the ring and in fluid communication with the pressure cavity. The pressure port can be configured to allow for passage of the hydraulic fluid from the pressure cavity to a second region between the ring and the rotor.