referring to fig1 the pump - nozzle arrangement comprises a cylindrical housing 1 , which contains a tightly arranged cap 2 at its upper end having a fluid delivery socket 3 and fluid discharge socket 4 . at the inlet side , a screen or filter 5 is interposed in the fluid delivery path . the cylindrical housing 1 also contains an actuating system 6 , a magnetic arrangement , made up of a soft iron sleeve 8 carrying magnet windings 7 as well as a longitudinally - displaceable armature 9 with a plurality of poles 10 . the actuating system is operable upon delivery of an electric current to the windings 7 , the armature moving longitudinally , that is , downward as shown in fig1 until the sleeve 11 lodges at its upper end against the rear edge of an adjusting screw 12 partially screwed into the cap 2 . thus the elements 11 and 12 define the stroke of the armature 9 . a construction of the actuating device 6 comprising double thread screwed windings has been found to be especially suitable . also contained in the cylindrical housing are at least one duct 13 connected with the fluid delivery socket 3 and one duct 14 connected with the discharge outlet 4 . these ducts are located outside the actuating device 6 so as not mutually to interfere . the lower end of the armature 9 , which has a plane end face , is faced by the end face of a pump piston 15 , which is biased upwardly by a pressure spring 16 supported by a sleeve 17 . the sleeve 17 is screwed into a lower cap 19 forming the housing of the nozzle arrangement 18 . the lower cap 19 , in turn , is screwed together with another sleeve 20 , which also closes off the bottom of the cylindrical housing 1 . the ducts 13 and 14 extend through the component 20 , as indicated by 13 &# 39 ; and 14 &# 39 ;. the component 20 also supports a pressure spring 21 which constitutes a return spring for the armature 9 , biasing it upwardly . various points of the arrangement are provided with seals , partly in the form of ring seals , partly in the form of packings . between the sleeve 17 and the narrowed down part 22 at the bottom end of the cap 19 , a sleeve - like prolongation 23 of element 17 is secured . the prolongation 23 forms in its upper region a guide for the pump piston 15 , and in its expanded lower region defines a chamber 24 of the nozzle arrangement 18 . in order to avoid the formation of vapor lock , it is desirable to keep this chamber as small as possible . disposed within the chamber 24 is a nozzle needle 25 which has a flared lower portion 26 which bears on a valve seat 27 , and the needle is biased upwardly , closed , by a spring 28 . a guide reinforcement 29 is provided on the nozzle needle 25 which is supported by a prolongation 30 forming a part of component 27 . this component 27 has several fluid inlet openings 31 formed in the prolongation 30 through which the fuel can enter the ring space between parts 25 and 27 ; thus the fuel which is in the ring space can be injected in a downward direction into the cylinder when the nozzle arrangement is actuated . fuel entering through the fluid delivery socket 3 is fed through the inlet duct 13 &# 39 ; and continues into a cross duct 13 &# 34 ; which communicates with an axially - extending duct 32 in the pump piston 15 . at the outlet end of the duct 32 a valve disc 33 bears on the lower end of the pump piston , such valve disc forming a part of a one - way suction valve which also includes a weak closing spring 34 . the suction valve is designed so that it will open in response to pressure provided by the fluid in the longitudinal duct 32 outside of the discharge times of the nozzle arrangement 18 , wherein increased pressure in the chamber will close the valve . a pair of outlet openings 35 and 36 in component 23 are selectively opened and closed by pump piston 15 . the pump piston 15 has a control edge 37 formed such that the flow communicates from the nozzle arrangement , e . g . the chamber 24 , out through the openings 35 or 36 along the control edge 37 when the pump piston 15 is retracted , that is at its upper position between delivery times . the openings 35 and 36 , however , will be blocked by the pump piston 15 when the piston 15 is actuated downwardly for delivery of fuel through the nozzle 25 . the openings 35 and 36 in turn are connected to a ring duct 38 , which connects with the outlet duct 14 &# 39 ; e . g . through a clearance in the threading between the sleeve 17 and the cap 19 . accordingly , the device illustrated in fig1 is actuated by energizing the actuating device 6 , thereby longitudinally displacing the pump piston in a direction towards the nozzle arrangement , that is , downwardly . during this displacement , the suction valve 33 , 34 is closed and the pressure in the chamber which now increases from the decreased volume in the chamber , results in the movement of the nozzle needle 25 in a downward direction , and opening of the nozzle valve 26 , 27 proper . thus the fuel quantity present in the chamber 24 will be ejected into the engine . in the intervals between injections , the pump piston 15 will be in the position shown in fig1 . the control edge 37 produces a connection between openings 35 and 36 and the chamber 24 of the nozzle arrangement 18 . thus there is a constant flow of fluid between the delivery 3 and the discharge 4 and thereby an on - going cooling of the chamber 24 and other areas of the pump - nozzle device . the scavenging effect of the flow also constantly removes any trapped gas , air or vapor locks which may form in the chamber 24 or in other zones of the device through which the flow passes . the discharge 4 may be connected directly with a tank for the fluid . during delivery times of the nozzle arrangement , however , the pump piston 15 blocks the openings 35 and 36 so that when a comparatively high pressure must be generated in the chamber 24 for actuating of the nozzle arrangement , that is , forcing the nozzle needle downward to open the chamber , such pressure build up is not impaired by fuel flowing out the outlet . another embodiment of the present invention is shown in fig2 . in this arrangement , there is provided , rather than intermittent scavenging and cooling , a constant flow of fuel through the nozzle arrangement to provide such scavenging . the device is similar to that shown in fig1 comprising a cylindrical housing 40 , an electromagnetic actuating device 41 , which may be identical to that shown in fig1 and at least one delivery duct 42 and discharge duct 43 which are in communication with the inlet 44 and outlet 45 . the inlet and outlet are provided with extensions 42 &# 39 ; and 43 &# 39 ; respectively in the component 60 closing off the bottom of the housing 40 . the delivery duct 42 &# 39 ; connects with an axially - extending duct 46 in the pump piston 47 , and the axially - extending duct 46 is again provided with a one - way suction valve consisting of a valve disc 48 bearing on the end face of the pump piston 47 , and a closing spring 49 . the nozzle arrangement 50 , as does the arrangement in fig1 contains a lower cap 51 , and a nozzle needle 52 which is designed in a manner similar to that of the corresponding element of the embodiment in fig1 . the chamber 53 of the nozzle arrangement 50 is subdivided into two parts by a pressure valve formed by an inset 54 , a valve disc 55 and a closing spring 55a . this pressure valve is disposed in the chamber between the suction valve 48 , 49 and the nozzle needle 52 , and prevents vapor lock created in the chamber 53 , e . g ., through heat transfer from a cylinder into the cap 51 , from reaching the zone of the suction valve 48 , 49 . this arrangement will assure that any increase in pressure in the lower chamber due to formation of vapor does not reach the suction valve , and that such valve at all times operates at opposition to a fluid pressure , but not to an increased vapor pressure . the device according to fig2 also contains an arrangement which ensures uniflow scavenging of the chamber 53 of the nozzle arrangement and other ducts of the device . in this case , the outlet of fuel flowing through the nozzle arrangement passes through a critical flow - through throttle 56 in the sleeve - like part 57 enclosing the chamber 53 . the critical flow - through throttle 56 opens into a ring duct 58 which in turn opens into a discharge duct 43 &# 39 ; e . g ., through a clearance in the threading 59 . thus , the chamber 53 is always in communication with the outlet 45 through the critical flow - through throttle 56 . when both valve discs 48 and 55 are open , uniflow scavenging will occur . if , upon a pressure increase in the lower part of the chamber 53 , e . g . due to vaporization of gases in the chamber 53 , the pressure valve 55 closes , uniflow scavenging will be temporarily interrupted , since fuel will not be flowing from the inlet duct 46 into the lower chamber 53 . however , the presence of the throttle 56 will cause a pressure relief resultant from any vapor lock . thereafter , the pressure valve will re - open and uniflow scavenging will resume . in this arrangement , the throttle 56 will not be blocked during times when it is necessary to increase pressure in the chamber 53 in order to actuate the nozzle , however is not necessary due to the design of the throttle 56 . during the discharge time for the nozzle arrangement , the presence of the throttle 56 will not impair the buildup of pressure in the chamber 53 necessary for longitudinal displacement of the nozzle needle insofar as the flow of fluids through a critical flow - through throttle is for the most part independent of the pressure on its inlet side . thus , in either of the aforementioned arrangements , the invention at most requires the formation of additional ducts in presently used components , and does not entail any additional construction effort . it is thus possible to retain a very small nozzle chamber . the invention can also be utilized if there is no combined pump - nozzle unit , but only the nozzle itself is in a heat transfer connection with the cylinder of the internal combustion engine . it is notably important that the invention ensures uniflow scavenging , i . e ., that no change in the flow direction occurs either during the actuation of the device or during the intervals in which the device is not actuated . the buildup of pressure required to actuate the nozzle arrangements remains unaffected in that means are provided in the path of the uniflow scavenging which limits the flow at least temporarily . in the embodiment described in connection with fig1 the control edge arrangement suspends the uniflow scavenging during delivery times of the nozzle arrangement completely or at least largely to permit the build - up of pressure , and in the embodiment described in connection with fig2 the critical flow - through throttle inherently allows a pressure build - up in the chamber as is required . the embodiments of the invention described herein are merely illustrative , and the invention may be embodied in other forms while still employing the inventive principles contained herein . other such modifications and variations will be apparent to those skilled in the art . all such modifications and variations are intended to be within the scope of the invention as defined in the following claims .