Abstract: A compression ignition internal combustion engine (1), which includes a cylinder (2), a piston (3) reciprocably received within the cylinder (2), a pair of contra-rotating crankshafts (4, 5) rotatably mounted relative to the cylinder (2), a pair of connecting rods (6, 7) each having a first end (61, 71) connected to a crank journal (41, 51) of a respective one of the crankshafts (4, 5) and a second end (62, 72) connected to the piston (3). The engine (1) is configured such that the stroke of the piston (3) in a first direction toward the crankshafts (4, 5) causes each crankshaft (4, 5) to rotate by a first angle and the piston stroke in a second direction opposite the first direction causes each crankshaft (4,5) to rotate by a second angle different (???) from the first angle.

Abstract: Disclosed are laminates comprising a carbon fiber reinforced polymer sheet and a layer of polysilazane and methods for producing such laminates.

Abstract: A supersonic jet aircraft and a method of operating the same. The supersonic jet aircraft having at least three turbofan engines and an engine management computer. A first engine of the at least three turbofan engines is configured to be de-activatable during flight to move from an operational state in which it provides thrust to an operational state in which it stops providing thrust. Other engines of the at least three turbofan engines are configured to provide sufficient thrust to the supersonic jet aircraft when the first engine is de-activated such that the aircraft can perform a supersonic climb operation and/or a supersonic cruise operation.

Abstract: A combustion system includes an annular tube disposed between an inner wall and an outer wall, the annular tube extending from an inlet end to an outlet end; at least one fluid inlet disposed in the annular tube proximate the inlet end, the fluid inlet providing a conduit through which fluid flows into the annular tube; at least one outlet disposed in the annular tube proximate the outlet end; at least one primary fuel injector, the primary fuel injector dispersing fuel into a fluid stream entering the annular tube via the fluid inlet; and at least one secondary fuel injector, the secondary fuel injector disposed in the annular tube.

Abstract: A gas injection valve for injecting a combustible gas into an internal combustion engine, comprising a valve element, which can be moved between closed position and an open position, the open position being defined by a maximum stroke of the valve element. The maximum stroke of the valve element can be adjusted during operation of the gas injection valve.

Abstract: Internal combustion engine having: a cylinder defining a combustion chamber; an exhaust duct that is flown through by the exhaust gases; and a system to supply a water-based operator liquid to the combustion chamber having: a tank designed to contain a certain amount of water-based operator liquid and a heating device designed to heat the water-based operator liquid contained in the tank. The heating device has: a first gas-liquid heat exchanger, which is designed to be flown through by at least part of the exhaust gases flowing along the exhaust duct; a second liquid-liquid heat exchanger, which is designed to heat the water-based operator liquid contained in the tank; and a hydraulic circuit, which is designed to send round an exchange fluid through the first heat exchanger to transfer the heat from the exhaust gases to the exchange fluid and through the second heat exchanger to transfer the heat from the exchange fluid to the water-based operator liquid contained in the tank.

Abstract: The evaporative fuel processing system includes a fuel tank, a canister, a pump, a pressure detection unit, a temperature detection unit, and a leak diagnosis unit a leak diagnosis unit configured to diagnose leak in the diagnostic object based on a first pressure change which is a change in pressure detected by the pressure detection unit when the temperature in the diagnostic object changes, a second pressure change which is a change in pressure detected by the pressure detection unit when the inside of the diagnostic object is pressurized or depressurized by the pump, a detected temperature by the temperature detection unit, a first preparation information and a second preparation information.

Abstract: In a fuel vapor treatment apparatus, when an internal combustion engine is in non-turbocharging operation, a controller is configured to open a first valve and a second valve, and when the internal combustion engine is in turbocharging operation, the controller is configured to close the first valve, and to open a third valve based on pressure in a fuel tank detected by a first pressure detector.

Abstract: An air box and methods are provided for communicating an airstream through an air filter to an air intake duct of an internal combustion engine of a vehicle. The air box is comprised of a housing that supports the air filter within an interior of the housing. A mount portion within the housing fixedly receives a base of the air filter. Multiple air inlets couple with corresponding air inlet ports of the vehicle to direct the airstream into the air box. A duct directs the airstream from the multiple air inlets to the interior of the housing and to the air filter. An opening into the housing exposes at least one surface of an electronic control unit (ECU) to the airstream for cooling of the ECU. A conduit communicates the airstream from an interior of the air filter to the air intake duct of the internal combustion engine.

Abstract: An apparatus and a method are provided for an air box configured to cool an engine control unit (ECU) by way of an airstream being communicated to an air intake system of an internal combustion engine of a vehicle. The air box is comprised of a housing to support an air filter within an interior of the housing. An opening in the housing fixedly receives at least one surface of the ECU to transfer heat from the ECU to the airstream. A mount portion within the housing receives the air filter. A conduit to a clean side of the air filter is configured to be coupled with the air intake system. An inlet to the housing is configured to couple with an air inlet duct of the vehicle so as to direct the airstream into the interior of the housing.

Abstract: A snorkel system comprising: (a) a vehicle adapter configured to connect to a vehicle; (b) one or more air tubes configured to extend along an interior of an engine compartment of the vehicle; and (c) one or more angle adapters adapted to be located within the engine compartment of the vehicle, the one or more angle adapters fluidly connecting the vehicle adapter and the one or more air tubes together; wherein the one or more angle adapters include: an inlet opening located within a first plane, the inlet opening being located proximate to and in fluid communication with the vehicle adapter, and an outlet opening being in communication with a first end of the one or more air tubes, the outlet opening being located within a second plane that is spaced apart from and extends substantially parallel to the first angle adapter.

Abstract: The present disclosure relates to a valve drive for at least one poppet valve of an internal combustion engine. The present disclosure further relates to an internal combustion engine and a motor vehicle having such a valve drive. The valve drive includes a valve lever for actuating the at least one poppet valve; and a valve lever axle on which the valve lever is mounted in a pivotably movable manner. The valve drive is characterized in that a fuel distributor for receiving pressurized fuel, that is to say, a rail, is integrated in the valve lever axle.

Abstract: Provided is a high-pressure fuel pump that ensures oil tightness even at high fuel pressure and has a small and lightweight inexpensive discharge valve structure. Therefore, a high-pressure fuel pump according to the present invention includes: a discharge valve arranged on a discharge side of a pressurizing chamber; a discharge valve seat on which the discharge valve is seated; and a facing member configured independently as a separate member from the discharge valve seat and located on an opposite side of the discharge valve seat with the discharge valve interposed therebetween, in which a stroke direction regulating portion that regulates displacement of the discharge valve in a stroke direction is formed on a tapered surface of the facing member.

Abstract: A filter assembly for filtering hydraulic fluid in a hydraulically actuated fuel injector is disclosed. The filter assembly includes a plurality of first rollers and a plurality of second rollers. The first rollers are parallelly disposed one after the other, and define first axes disposed in a first plane. The second rollers are parallelly disposed one after the other, and define second axes disposed in a second plane. The first plane is parallel to the second plane. Further, each second roller is disposed between a consecutively arranged pair of first rollers to define one or more filtration zones for filtering the hydraulic fluid.

Abstract: An electronic carburetor injection system is provided for an internal combustion engine. The electronic carburetor injection system is a standalone, user programmable fuel injection system that delivers additional fuel to the engine whenever a lean fuel/air mixture is delivered by a carburetor. The electronic carburetor injection system includes a fuel injector that delivers liquid fuel in the form of a spray discharge. A plate supports the fuel injector between the carburetor and an intake manifold of the engine. The plate includes an injector port that allows the spray discharge to enter the intake manifold without interfering with operating the carburetor. An engine control unit operates the fuel injector according to signals received from an oxygen sensor that is disposed within an exhaust system of the engine. During operation, the electronic carburetor injection system maintains the fuel/air mixture within a proper range across multiple driving conditions and changing environmental conditions.

Abstract: To provide a combined cycle plant, a control device thereof, and a steam turbine startup method that are aimed at improving the operability of a combined cycle plant by allowing a quick change of the output. A combined cycle plant is provided with: a gas turbine having a compressor, a combustor, and a turbine; a supplementary firing burner that raises the temperature of exhaust gas of the gas turbine; a heat recovery steam generator that generates steam using exhaust heat of the exhaust gas; a steam turbine that is driven by steam generated by the heat recovery steam generator; and a control device that changes both an output of the combustor and an output of the supplementary firing burner when an output of the combined cycle plant is to be changed.

Abstract: A remote engine start system, comprising an engine start unit and a control unit is disclosed. The engine start unit is arranged in a vehicle and configured to receive signals from a remote control. The vehicle comprises a drive motor. The engine start unit is configured to initiate the start of the drive motor upon receipt of a signal from the remote control. The control unit is configured to monitor the function of the engine start unit, and to detect errors in the function of the engine start unit. The remote engine start system is configured to prevent the starting of the drive motor once an error in the function of the engine start unit was detected, and to initiate the turning off of the drive motor, if the drive motor is turned on and an error in the function of the engine start unit was detected.

Abstract: A vehicle includes an electric power reception unit that is configured to receive electric power that is required to activate a system of the vehicle, from a portable device that is portable, the portable device including an electrical storage device provided therein, and the portable device being configured to carry out at least one of authentication of a user of the vehicle and issuance of a command to activate the system.

Abstract: In at least some implementations, an ignition system for a combustion engine includes a controller, an ignition circuit, and a wire providing two-way communication between the ignition circuit and the controller. The ignition circuit may include a charge capacitor that is discharged to cause an ignition event. The ignition circuit may be an inductive discharge ignition circuit including a coil and may then also include a second wire that provides electrical power to the coil.

Abstract: At the start of the engine, when the temperature of the catalyst is less than the activation temperature, control for activating the catalyst (i.e., activation control) is performed. In the activation control, the first and second discharge actions of the ignition apparatuses are controlled. The first discharge action is performed to ignite the mixed gas in the cylinder. The second discharge action is performed to generate ozone. The first discharge action is performed immediately after the start of the cranking. The first discharge action is performed in the crank angle section at the retard side rather than the compression TDC. The first discharge action is performed in every cylinder. The second discharge action is performed before the start of the cranking. The second discharge action is performed in the other cylinder except for the initial combustion cylinder.

Abstract: A system and method for generating microwaves for microwave enhanced combustion (MEC) input to an MEC antenna of an internal combustion engine. The system uses a microwave generator and a directional coupler, which delivers the MEC input signal to the MEC antenna and receives a reflected signal from the MEC antenna. A feedback path determines a desired frequency for the MEC input signal, based on the reflected signal, and also determines a power feedback correction value. An open loop path determines desired power and timing for the MEC input signal, based on various engine conditions. The desired power is corrected with the power feedback correction value.

Abstract: The present invention relates to a flow controller configured to selectively act as a pump or as a flow regulator. The flow controller comprises: an inlet for a fluid; an outlet for the fluid; a pump assembly arranged between the inlet and the outlet and configured to pump the fluid through the flow controller from the inlet to the outlet; a hydro electrical generator assembly arranged between the inlet and the outlet, the hydro electrical generator assembly configured to allow the fluid flow through the flow controller from the inlet to the outlet and to generate electricity by transforming flow energy of the fluid flowing through the flow controller into electricity; and a mode controller configured to selectively set the flow controller in a pumping mode or in an electricity generating mode.

Abstract: An assembly for generating energy from waves, comprising a concentric ring flywheel operatively arranged to generate electrical current, the concentric ring flywheel comprising a first shaft including an input end and an output end, a plurality of rings, the plurality of rings including at least a first ring, including a first radially inward facing surface arranged to connect with the output end of the first shaft, and a first radially outward facing surface, a second ring arranged concentrically around the first ring, the second ring including a second radially inward facing surface and a second radially outward facing surface, one or more first clutch connectors arranged in a first space radially arranged between the first and second rings to non-rotatably connect the second ring and the first ring, and a wave energy capture device operatively arranged to rotate the first shaft.

Abstract: A wave energy capture device, including a wave chamber arranged to engage a body of water including a plurality of waves, including a floor having a front end and a rear end, a first opening arranged proximate the front end, a second opening arranged proximate the rear end, and a hose arranged on said floor and extending from the first opening to the second opening, the hose operatively arranged to fill with water from the body of water, and a cylinder arranged on the floor proximate the front end, the cylinder connected to the wave chamber via one or more springs, wherein, when one of the plurality of waves enters the first opening, the cylinder is displaced along the floor from the front end toward the rear end, and expresses the water in the hose in a first direction from the front end toward the rear end.

Abstract: The present invention discloses a ducted bidirectional tidal current power station system, mainly consisting of a bidirectional tidal current power generation device, a dam, an open sea, an inland sea, a duct, and an opening/closing gate. The bidirectional tidal current power generation device is installed in the duct on the bottom of the dam. Openings, respectively communicated with the open sea and the inland sea, are formed at two ends of the duct, and an opening/closing gate is arranged at each of the two openings. By the ducted bidirectional tidal current power station system of the present invention, the cost of marine construction, operation and maintenance of the tidal current power generation device in an open sea area is saved, and the complex structure of the power generation device in the tidal power station and the cost of strict construction of auxiliary devices and runners are avoided.

Abstract: A guide bearing system including a pad adjuster to traverse at least one bearing in a direction to adjust a radial clearance. The system can further include a sensor for measuring deviations in the radial clearance. In some embodiments, the guide bearing system includes a controller that receives a distance signal from the sensor measuring the radial clearance and signals the pad adjuster to traverse the at least one bearing to compensate for the deviations in the radial clearance.

Abstract: A multi-rotor, multi-axis wind turbine where the rotors are in relative motion to one another to maximize the energy captured and thus generated, where there is a primary rotor axis and direction and one or more secondary rotor axes, where each rotor rotates about a different axis, and the rotors can operate in either a horizontal or vertical axis orientation or some orientation in between, and there are at least two rotor axes operating in different directions such that the relative motion of the primary rotor drives at least one secondary rotor into the surrounding air increasing the relative net vector velocity of the secondary rotor with respect to the wind velocity and surrounding air which increases the amount of energy captured at a given location for a given wind velocity over the prior art.

Abstract: A variable-pitch vertical axis wind turbine comprises a hub supported for rotation about a central axis and a blade pivotally mounted to the hub so as to permit relative rotation between the blade and the hub. The blade and the hub define a pitch angle therebetween. The wind turbine comprises a mechanism configured to produce reciprocating motion during rotation of the hub about the central axis. The wind turbine comprises a linkage configured to transfer the reciprocating motion produced by the mechanism to the blade so as to vary the pitch angle.

Abstract: A wind turbine and associated control method includes a controller configured with a high speed shaft brake in the generator gear train. The controller receives an input signal corresponding to rotational speed of the high speed shaft, wherein upon the high speed shaft reaching a predefined rotational speed and under a braking condition that calls for the rotor to come to a complete standstill, the controller generates an activate signal to activate the brake. An interlock system is in communication with the low speed shaft sensor and the controller and is configured to override the activate signal when the rotational speed of the low speed shaft is above a threshold value.

Abstract: The invention relates to a power plant controller for controlling wind turbine generators. More particularly, the invention relates to a method for compensating data obtained from measurements at a connection point to the grid in case of a communication failure where communication of such data is lost or becomes unreliable. The measured data are used in the power plant controller for determining setpoints for controlling the wind turbine generators' production of active and reactive power. In response to detection of a communication fault a new setpoint is determined independently of new measured grid data by reconfiguring parts of the power plant controller.

Abstract: A vertical axis wind turbine generator having a support stand (11), a shaft (41) defining the longitudinal direction and axis (19) of the generator. Two rotating members (12, 13) are coupled to the support stand (11) and the upper end of the shaft (41), thus being enabled to rotate about the axis (19). Two or more blades (14, 24, 34) having two free ends (15, 16) are connected by connecting members (17 and 18) to the two rotating members (12, 13), wherein movement of the first and/or second rotating members (12, 13) towards or away from one another causes the blades (14, 24, 34) to move further from, or closer to, the shaft (41).

Abstract: A wind energy park comprising a number of wind turbines (1) is disclosed. Each wind turbine (1) comprises a tower (2) placed on a foundation, at least one nacelle (3) mounted on the tower (2) and a rotor (4) coupled to the nacelle (3) generating electrical energy for a power grid of the wind energy park. The wind energy park further comprises at least one airborne wind energy system (12, 13) coupled to one of the wind turbines (1) via a cable (6).

Abstract: Provided are embodiments of a wind energy system. The system includes a plurality of wind turbines connected to at least one cable network. The cable network is configured to transmit the electrical power fed-in by the connected wind turbines. The system also includes at least one control apparatus configured to control the power fed into the cable network by at least one of the wind turbine by providing at least one power set point. At least one temperature detecting device is configured to detect the temperature of the cable network. At least one condition detecting device is configured to detect the condition of the wind energy system, and the control apparatus includes at least one control device configured to determine the power set point based on the detected temperature and the detected condition.

Abstract: Provided is a method of manufacturing a panel of a wind turbine nacelle, which method includes the steps of providing a mold for the panel; arranging at least one divider in the mold to spatially divide the mold into at least a first mold region and a second mold region; arranging composite material in the mold; curing the composite material; and separating the cured panel into at least a first panel portion and a second panel portion along a line defined by a divider. Also provided is a method of constructing a wind turbine nacelle, and a wind turbine including such a nacelle.

Abstract: A method for detecting when a rotor blade of a wind turbine is stuck is described. The method can include monitoring, via a controller, a speed of rotation of the wind turbine, and, determining, via the controller, a running average of the speed of rotation. The method further includes applying, via the controller, at least one filtering operation to the running average to obtain a filtered value, and, determining, via the controller, a stuck condition of one or more rotor blades of the wind turbine based on the filtered value. The method can also include performing a control operation to reduce loading on the wind turbine based on the stuck condition.

Abstract: The invention relates to an assembly for monitoring and/or controlling a wind turbine. The assembly for monitoring and/or controlling a wind turbine comprises: an arrangement of two strain sensors, in particular three strain sensors, which detects blade bending moments of a rotor blade of a wind turbine in at least two different spatial directions; a first fibre optic vibration sensor for detecting vibrations of the rotor blade in a first spatial direction; and at least one second fibre optic vibration sensor for detecting vibrations of the rotor in a second spatial direction, which differs from the first spatial direction.

Abstract: A method for retrofitting a wind turbine blade with a replacement blade tip segment includes producing a replacement blade tip segment with an internal beam receiver section, and producing a beam structure. The existing blade tip segment is cut away from the wind turbine blade, wherein the cut defines a chord-wise joint line at the remaining blade root segment of the wind turbine blade. The beam structure is fixed into spar structure of the blade root segment. The replacement blade tip segment is aligned and connected with the blade root segment in a span-wise direction so that the beam structure moves into the beam receiver section. A finish surface can be provided to the blade shell components of the blade root segment and the replacement tip segment at the joint line.

Abstract: A method for manufacturing a wind turbine blade that is pre-staged for subsequent retrofitting with a replacement blade tip segment includes providing the wind turbine blade with a continuous spar structure from a root end to a tip end of the wind turbine blade. At a pre-defined span-wise location, one of a span-wise extending beam structure or span-wise extending receiver section is configured with the spar structure.

Abstract: Provided is a filter device configured for providing air for a generator of a wind turbine. The filter device includes a housing including a filter, at least one attaching element configured for attaching the housing to a drive end side of the generator, such that the air is guidable through the filter into the generator. Further, a wind turbine is provided which includes a filter device for providing air for a generator of the wind turbine. Furthermore, a method for arranging a filter device configured for providing air for a generator of a wind turbine is also provided.

Abstract: The present invention relates to an actuator (10) comprising a first connection unit, a second connection unit, a spring arranged between the first and second connection unit, a guide tube (12) arranged inside the spring, and a dip rod configured to be displaceable relative to the guide tube (12) so that it dips into the guide tube (12), wherein the dip rod is mounted in a guide bush (14), characterised in that the guide bush (14) comprises a recess (18) in the circumferential direction of the guide bush (14) adapted to accommodate a tapered end of the guide tube (12).

Abstract: A thermal actuator unit of the present invention includes a first member, a second member, an elastic part which is disposed between the first member and the second member, and a thermal deformation part which is disposed on a side of the first member opposite to a side with the second member and has a shape-memory alloy to be deformed to the side with the second member due to heat.

Abstract: The invention relates to pressure transfer device, system comprising the pressure transfer device, a fleet comprising the system and use of a pressure transfer device for pumping fluid at pressures above 500 bars, the pressure transfer device (1?, 1?) comprising a pressure chamber housing (1?, 1?) and at least one connection port (3?, 3?), the at least one connection port (3?, 3?) being connectable to a dual acting pressure boosting liquid partition device (2) via fluid communication means (26?, 27; 26?, 27?), the pressure chamber housing comprises: —a pressure cavity (4?, 4?) inside the pressure chamber housing, and at least a first port (5?, 5?) for inlet and/or outlet of fluid to the pressure cavity (4?, 4?), —a bellows (6?, 6?) defining an inner volume (7?, 7?) inside the pressure cavity (4?, 4?), and wherein the inner volume (7?, 7?) is in fluid communication with the connection port (3?, 3?), wherein the pressure cavity (4?, 4?) has a center axis (C?, C?) with an axial length (L) defined by the distance

Abstract: A control device of a hybrid vehicle including an engine, a first rotating machine, a power transmission device, a differential mechanism, a lock mechanism, a mechanical oil pump, and an electric oil pump, the control device comprises: a hybrid control portion; a state determining portion; and a flow rate control portion prohibiting the double drive motor running to cause the hybrid vehicle to run in the single drive motor running and controlling the first rotating machine to rotate the mechanical oil pump to cause the mechanical oil pump to discharge the hydraulic oil at the flow rate required for the power transmission device when it is determined that the electric oil pump is in the state of insufficient capacity at the time of running in the motor running mode.

Abstract: In an exemplary embodiment, a capacity control valve includes: a valve main body 2 having a first valve chamber 7 through which a fluid at control pressure passes and which has a first valve seat surface 31A, and an interior space 4 through which a fluid at suction pressure passes; and a valve body 21 having an intermediate communication passage 26 for communicating the first valve chamber 7 and the interior space 4, and a first valve part 21C for opening and closing the intermediate communication passage 26 adjacent to the first valve seat surface 31A, wherein an opening area of the first valve part 21C is smaller than that of the intermediate communication passage 26. The capacity control valve is capable of simultaneously achieving reduction of a start-up time of the variable capacity compressor and improvement of responsiveness of capacity control at the time of control.

Abstract: A spool operation failure due to foreign matter contamination is prevented. A variable displacement compressor 100 includes a first control valve 300 controlling the opening degree of a supply passage 145, a check valve 350, a second control valve 400 controlling the opening degree of a discharge passage 146, and a back-pressure relief passage 147. The second control valve 400 includes a back pressure chamber 410 communicating with an intermediate supply passage 145b1, a valve chamber 420 to which a valve hole 103d and a discharge hole 431a are open and that constitutes a part of the discharge passage 146, a partition member 430 partitioning into the back pressure chamber 410 and the valve chamber 420, and a spool 440 extending through a through hole 432a formed in the partition member 430. The spool 440 has a pressure receiving portion 441 disposed in the back pressure chamber 410, a valve portion 442 disposed in the valve chamber 420, and a shaft portion 443.

Abstract: The present invention discloses a zipper tab assembly with exhausting and/or inflating functions. The zipper tab assembly includes a housing, an electric air pump disposed inside the housing and configured to exhaust or inflate, and a power terminal having an input port and an output port. The input port protrudes out of the housing, and the output port is disposed inside the housing and electrically connected to the electric air pump. The zipper tab assembly further includes a hook disposed outside the housing and connected to the housing. The zipper tab assembly of the present invention has exhausting and/or inflating functions and has the advantages of practicability, convenient utilization, small size, light weight, convenient wearing and convenient carrying.

Abstract: A pump unit (10) can be carried by an operating person for the pressurized filling of inflatable filling chambers with a fluid, in particular lifting pads (2), blocking pads, tents or the like. The pump unite includes a fluid pump (12), an electric motor (11) for driving the fluid pump (12), a battery (13), a control unit (17) for controlling the operation of the fluid pump, and a connector (18) for the connection of a fluid hose (3) which leads to the filling chamber. A manually actuatable control valve (16) is positioned on the pump unit (10).

Abstract: A cryopump includes: a first-stage cryopanel; a second-stage cryopanel; a cryocooler thermally coupled to the first-stage cryopanel and the second-stage cryopanel to cool the first-stage cryopanel to a first-stage cooling temperature and cool the second-stage cryopanel to a second-stage cooling temperature that is lower than the first-stage cooling temperature; and a cryocooler controller configured to execute first-stage temperature control for controlling the first-stage cooling temperature to a first-stage target temperature and increase the cooling capacity of the cryocooler when an increase in the second-stage cooling temperature is detected during the execution of the first-stage temperature control.

Abstract: A pump device (10) for pumping a fluid, having a hydraulic enclosure (12) that comprises an annular section, a pump ring (14) that is deformable and which defines an annular pump chamber at least in certain regions, a pump ring carrier (16) that is solidly connected to the pump ring (14), a first connector and a second connector, which first connector and which second connector are in fluid communication with the pump chamber, wherein the pump device (10) is set up in such a way that at least one measure influences a parking position of an eccentric (18) such that said parking position is preferred in the region of a clamping member (114), the measure being selected from: a) at least one recess in the hydraulic housing, which recess locally widens the chamber for the pump ring (14) in the axial direction, b) a geometry of the pump ring carrier (16), in which the pump ring carrier (16) has an enlarged diameter on its inner side facing the eccentric (18) in the angular region of the clamping member (114), and c

Abstract: Disclosed herein is a fluid supply system that can provide fluid to a jetting assembly at a constant pressure or at pressures within a desired range of pressures. In an example, the fluid can be ink, and the jetting assembly can be a print head configured for dispensing the ink.