Solid-liquid raw material special proportion injection device for liquid medicine manufacturing
Technical Field
The invention relates to the technical field of liquid medicine manufacturing, in particular to a solid-liquid raw material special proportion injection device for liquid medicine manufacturing.
Background
At present, in the process of manufacturing liquid medicine, a plurality of raw materials of two raw material pistons need to be mixed in a fixed proportion, wherein the solid and the liquid are most difficult to mix, common instruments use high-precision instruments for mixing, the manufacturing cost is high, the maintenance cost is high, and the limitation is large.
Disclosure of Invention
The present invention is directed to a device for injecting a solid-liquid raw material for chemical solution production at a specific ratio, which solves the problems of the prior art.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a special proportion injection device of solid-liquid raw materials for liquid medicine manufacturing, includes the main casing body, the bottom of the main casing body is provided with hollow joint casing, the inside socket that is provided with in bottom of hollow joint casing, one side of the main casing body is provided with the overload protection mechanism of integral type, one side of overload protection mechanism is through a bolt fastening motor installation casing, the internally mounted motor of motor installation casing, the center of the main casing body is through the fixed rotation axis of bearing, and the inside of the main casing body is provided with turbine mechanism installation space and circular plate valve installation space, turbine mechanism and circular plate valve are installed respectively to the rotation axis on being located the axis body of turbine mechanism installation space and circular plate valve installation space inside, the periphery of circular plate valve is provided with a plurality of semi-circular groove structure that are the setting of annular array, the inside of the main casing body is provided with the inside first discharge hole of intercommunication turbo mechanism installation space and hollow joint casing, the inside of the main casing body is provided with the inside second discharge hole of intercommunication circular plate valve installation space and hollow joint casing, the top of the main casing body is provided with the liquid entering pipeline and the infundibulate groove structure of integral type respectively, just liquid entering pipeline and infundibulate groove structure communicate the top of turbo mechanism installation space and circular plate valve installation space respectively, the inside on liquid entering pipeline top is provided with connection port.
Preferably, the overload protection mechanism comprises a main hollow shell for the overload protection mechanism, a main hollow section for the overload protection mechanism, a rotating column for the overload protection mechanism, an auxiliary hollow shell for the overload protection mechanism, an auxiliary hollow section for the overload protection mechanism, a movable plate for the overload protection mechanism, a spiral spring for the overload protection mechanism, a push rod for the overload protection mechanism and a semicircular groove structure for the overload protection mechanism.
Preferably, the center of one end face of the main hollow shell for the overload protection mechanism is fixedly connected with the end part of a rotating shaft, the center of the inside of the main hollow shell for the overload protection mechanism is the main hollow interval for the overload protection mechanism, the main hollow shell for the overload protection mechanism is sleeved with a rotating column for the overload protection mechanism in the main hollow interval for the overload protection mechanism, a plurality of auxiliary hollow shells for the overload protection mechanism are arranged on the side face of the main hollow shell for the overload protection mechanism and integrated with the main hollow shell, the inside of the auxiliary hollow shell for the overload protection mechanism is the auxiliary hollow interval for the overload protection mechanism, a movable plate for the overload protection mechanism is arranged on one end face of the main hollow interval for the overload protection mechanism in the auxiliary hollow interval for the overload protection mechanism, and an overload protection machine is fixed between one ends of the movable plates for the overload protection mechanism in the auxiliary hollow interval for the overload protection mechanism Construct and use coil spring, overload protection constructs a terminal surface of fly leaf and is provided with the overload protection mechanism with its integral type structure and uses the push rod, just overload protection constructs and runs through with the push rod overload protection mechanism constructs with main cavity casing, and is located overload protection constructs with the interval inside of main cavity, overload protection constructs with the push rod and is lieing in overload protection constructs with the interval one end of main cavity is semi-circular structure, the side of overload protection mechanism with the column spinner is provided with and is used for placing overload protection constructs with the semi-circular groove structure for the overload protection mechanism of push rod tip, overload protection constructs one end and motor spindle tip fixed connection with the column spinner.
Preferably, the initial length of the coil spring for overload protection mechanism is longer than the length of the sub hollow section for overload protection mechanism.
Preferably, the structural shape of the end part of the push rod for the overload protection mechanism is consistent with the structural shape of the semicircular groove structure for the overload protection mechanism.
Preferably, the turbine mechanism includes a turbine mechanism bushing and a turbine mechanism branch fin.
Preferably, a plurality of branch fins for a turbine mechanism are provided on a side surface of the sleeve for a turbine mechanism, the branch fins being integrated with the sleeve for a turbine mechanism, and a center of the sleeve for a turbine mechanism is fitted around a shaft body of the rotating shaft.
Preferably, the plurality of branch fins for a turbine mechanism are arranged in an annular array with respect to the axial line of the sleeve for a turbine mechanism as the center of a circle.
Compared with the prior art, the invention has the beneficial effects that: the invention utilizes the rotating motor to control the flow, and in addition, the device utilizes the circular plate valve and the turbine mechanism to perform proportional mixing action, thereby ensuring the mixing quality and ensuring the quality of the mixed materials. The device is a mechanical mechanism, and has the advantages of low manufacturing cost, low maintenance cost and strong practicability.
Drawings
FIG. 1 is a schematic structural view of a device for injecting solid-liquid raw materials for manufacturing a liquid medicine according to a specific ratio of the present invention;
FIG. 2 is a schematic structural diagram of a turbine mechanism in the device for injecting solid-liquid raw materials for manufacturing liquid medicine in a special proportion according to the present invention;
FIG. 3 is a schematic structural diagram of an overload protection mechanism in a solid-liquid raw material special proportion injection device for manufacturing liquid medicine according to the present invention;
in the figure: 1, a main housing, 2, a hollow snap housing, 3, a socket, 4, an overload protection mechanism, 41, a main hollow housing for the overload protection mechanism, 42, a main hollow section for the overload protection mechanism, 43, a rotary column for the overload protection mechanism, 44, an auxiliary hollow housing for the overload protection mechanism, 45, an auxiliary hollow section for the overload protection mechanism, 46, a movable plate for the overload protection mechanism, 47, a coil spring for the overload protection mechanism, 48, a push rod for the overload protection mechanism, 49, a semicircular groove structure for the overload protection mechanism, 5, a motor mounting housing, 6, a motor, 7, a rotary shaft, 8, a bearing, 9, a turbine mechanism mounting space, 10, a circular plate valve mounting space, 11, a turbine mechanism, 111, a shaft sleeve for the turbine mechanism, 112, a branch fin for the turbine mechanism, 12, a circular plate valve, 13, a semicircular groove structure, 14, a first discharge hole, 15, a second discharge orifice, 16, a liquid inlet conduit, 17, a funnel-shaped groove configuration, 18, connecting ports.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, an embodiment of the present invention: the novel flat plate valve comprises a main shell body 1, wherein a hollow clamping shell body 2 is arranged at the bottom of the main shell body 1, a socket 3 is arranged inside the bottom end of the hollow clamping shell body 2, an integrated overload protection mechanism 4 is arranged on one side of the main shell body 1, a motor installation shell body 5 is fixed on one side of the overload protection mechanism 4 through a bolt, a motor 6 is installed inside the motor installation shell body 5, a rotating shaft 7 is fixed at the center inside the main shell body 1 through a bearing 8, a turbine mechanism installation space 9 and a circular plate valve installation space 10 are arranged inside the main shell body 1, a turbine mechanism 11 and a circular plate valve 12 are respectively installed on a shaft body of the rotating shaft 7 inside the turbine mechanism installation space 9 and the circular plate valve installation space 10, and a plurality of semicircular groove structures 13 arranged in an annular array are arranged on the circumferential surface of the circular plate valve 12, the inside of main casing body 1 is provided with intercommunication turbo mechanism installation space 9 and the inside first discharge hole 14 of hollow joint casing 2, the inside of main casing body 1 is provided with intercommunication circular plate valve installation space 10 and the inside second discharge hole 15 of hollow joint casing 2, the top of main casing body 1 is provided with the liquid inlet pipe way 16 and the infundibulate groove structure 17 of integral type respectively, just liquid inlet pipe way 16 and infundibulate groove structure 17 communicate respectively the top of turbo mechanism installation space 9 and circular plate valve installation space 10, the inside on liquid inlet pipe way 16 top is provided with connection port 18.
Referring to fig. 2, the overload protection mechanism 4 includes a main hollow housing 41 for the overload protection mechanism, a main hollow section 42 for the overload protection mechanism, a rotary column 43 for the overload protection mechanism, an auxiliary hollow housing 44 for the overload protection mechanism, an auxiliary hollow section 45 for the overload protection mechanism, a movable plate 46 for the overload protection mechanism, a coil spring 47 for the overload protection mechanism, a push rod 48 for the overload protection mechanism, and a semicircular groove structure 49 for the overload protection mechanism; the center of an end face of the main hollow shell 41 for the overload protection mechanism is fixedly connected with an end portion of the rotating shaft 7, the center of the inside of the main hollow shell 41 for the overload protection mechanism is the main hollow interval 42 for the overload protection mechanism, the main hollow shell 41 for the overload protection mechanism is positioned in the main hollow interval 42 for the overload protection mechanism, a rotating column 43 for the overload protection mechanism is sleeved in the main hollow interval 42 for the overload protection mechanism, a plurality of auxiliary hollow shells 44 for the overload protection mechanism in an integrated structure with the main hollow shell 41 for the overload protection mechanism are arranged on the side face of the main hollow shell 41 for the overload protection mechanism, the inside of the auxiliary hollow shell 44 for the overload protection mechanism is an auxiliary hollow interval 45 for the overload protection mechanism, a movable plate 46 for the overload protection mechanism is positioned on an end face of the main hollow interval 42 for the overload protection mechanism in the auxiliary hollow interval 45 for the overload protection mechanism, and the auxiliary hollow interval 45 for the overload protection mechanism is positioned in one movable plate 46 for the overload protection mechanism A spiral spring 47 for an overload protection mechanism is fixed between the ends, a push rod 48 for the overload protection mechanism is arranged on one end face of a movable plate 46 for the overload protection mechanism, the push rod 48 for the overload protection mechanism penetrates through a main hollow shell 41 for the overload protection mechanism and is positioned in the main hollow interval 42 for the overload protection mechanism, the push rod 48 for the overload protection mechanism is of a semicircular structure at one end positioned in the main hollow interval 42 for the overload protection mechanism, a semicircular groove structure 49 for the overload protection mechanism, which is used for placing the end part of the push rod 48 for the overload protection mechanism, is arranged on the side face of a rotating column 43 for the overload protection mechanism, and one end of the rotating column 43 for the overload protection mechanism is fixedly connected with the end part of a main shaft of a motor; the initial length of the coil spring 47 for the overload protection mechanism is longer than the length of the sub hollow section 45 for the overload protection mechanism; the structural shape of the end part of the push rod 48 for the overload protection mechanism is consistent with the structural shape of the semicircular groove structure 49 for the overload protection mechanism, and the structure has the main functions of: the main working principle is as follows: when the maximum rotation force of the coil spring 47 for the overload protection mechanism is used, and the rotation force caused by the external force is larger than the elastic force of the coil spring 47 for the overload protection mechanism, the push rod 48 for the overload protection mechanism is separated from the semicircular groove structure 49 for the overload protection mechanism, so that the main hollow housing 41 for the overload protection mechanism and the rotary column 43 for the overload protection mechanism rotate relatively.
Referring to fig. 3, the turbine mechanism 11 includes a turbine mechanism bushing 111 and a turbine mechanism branch fin 112; a plurality of turbine mechanism branch fins 112 integrated with the turbine mechanism branch shaft sleeve 111 are arranged on the side surface of the turbine mechanism shaft sleeve 111, and the center of the turbine mechanism shaft sleeve 111 is sleeved on the shaft body of the rotating shaft 7; the plurality of branch fins 112 for the turbo mechanism are arranged in an annular array around the axial line of the shaft sleeve 111 for the turbo mechanism as the center of a circle, and mainly function as: the liquid distributor has the function of shunting and realizes the function of controlling and shunting liquid.
It should be noted that the ratio of the liquid discharge amount caused by one rotation of the turbine mechanism 11 to the solid discharge flow amount caused by one rotation of the circular plate valve 12 is the same as the mixing ratio
The specific use mode is as follows: in the working process of the invention, the sleeve joint 3 in the device is clamped at the feed inlet of the mixing and stirring shell, then the solid is originally put into the leak-shaped groove structure 17, then the liquid enters the pipeline 16 and is connected with the discharge outlet of the liquid raw material, at the moment, the motor 6 is opened, the discharge speed is controlled, and the solid and the liquid are simultaneously discharged under the action of rotation, thereby realizing the equal proportion mixing function.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.