Feeding mechanism for aero-engine part machining

Abstract

The utility model relates to the technical field of aero-engine part machining, and discloses a feeding mechanism for aero-engine part machining, which comprises a box body, the bottom of the box body is fixedly communicated with an outer feeding port, and the side wall of the outer feeding port is fixedly provided with an annular rubber sealing stop block. A cavity is formed by the inner side face of the annular rubber sealing check block and the side face of the feeding opening. According to the feeding mechanism for machining the aero-engine parts, the outer feeding opening is formed, an annular rubber sealing check block is fixedly mounted on the side face of the outer feeding opening, and a cavity is formed by the inner side face of the annular rubber sealing check block and the outer side face of the outer feeding opening, so that when feeding is conducted, the side face of the annular rubber sealing check block can be tightly attached to the side face of a feeding barrel; according to the coating absorption device, the cavity is formed in the absorption barrel, so that the volatilized coating can be retained in the cavity and flows into the absorption agent in the absorption barrel through the connecting pipe, the volatilized coating can be absorbed, and then atmospheric pollution can be reduced.

Description

TECHNICAL FIELD

[0001] The utility model relates to aviation engine parts processing technical field, concretely is a kind of aviation engine parts processing with feeding mechanism. BACKGROUND

[0002] Aviation engine parts processing need to smear or spray coating layer to protect, at this time, feeding mechanism is needed to cooperate processing, the feeding opening of existing aviation engine parts processing with feeding mechanism cannot completely seal the feed inlet of material barrel, so that in the process of feeding, part of component in coating can form mist, and discharge into atmosphere, not only cause certain adverse effect to surrounding production environment, also can have certain influence to the health of operator, therefore, an aviation engine parts processing with feeding mechanism is proposed to solve the problems mentioned in the above background. SUMMARY

[0003] (I) technical problem solved

[0004] In view of the deficiencies in the prior art, the utility model provides an aviation engine parts processing with feeding mechanism, has the advantages of reducing pollution, solves the problems raised in the above background technology.

[0005] (II) technical scheme

[0006] To achieve the above object, the utility model provides the following technical scheme: an aviation engine parts processing with feeding mechanism, including box, box bottom is fixedly connected with outer feeding opening, the outer feeding opening side wall is fixedly installed with annular rubber sealing block, the inner side surface of annular rubber sealing block and the side surface of outer feeding opening form cavity, the connecting pipe is fixedly connected with the other end of connecting pipe, the other end of connecting pipe is fixedly connected with absorption cylinder, the top of absorption cylinder is fixedly connected with the side surface of box bottom, the side surface of absorption cylinder is fixedly installed with inlet and outlet.

[0007] Preferably, the inner wall of the inner feeding opening is fixedly installed with the slot hole block, the threaded rod is movably installed in the slot hole block, the threaded rod is threadedly connected with the lock hole block, the spring is fixedly installed at the bottom of the outer feeding opening, the other end of the spring is fixedly installed with the spring plate, by providing the inner feeding opening, the inner feeding opening can be directly connected with the feeding cylinder, the lock hole block can be moved in the slot hole block by rotating the threaded rod, so that the opening and closing of the inner feeding opening can be controlled, the spring is fixedly installed at the bottom of the outer feeding opening, and the other end of the spring is fixedly installed with the spring plate, so that the feeding cylinder is loaded.

[0008] Preferably, the threaded rod is fixedly connected with a controller at one end outside the outer feeding port, a weighing rod is fixedly installed at the bottom of the controller, and a weighing plate is fixedly connected to the other end of the weighing rod.

[0009] Preferably, the box body is fixedly installed with support blocks at four corners, and the four support blocks are fixedly connected with the side surface of the weighing plate.

[0010] Preferably, the box body is internally provided with a vacuum layer, a water layer and a coating layer, the box body is fixedly installed with a cover plate at the top, the cover plate is fixedly installed with a driving device and a feeding port, the box body is fixedly installed with a refrigeration device at the side surface, the refrigeration device is fixedly installed with a connecting pipeline at the side surface, and the other end of the connecting pipeline is communicated with the water layer.

[0011] Compared with the prior art, the utility model provides a kind of feeding mechanism for aero-engine parts machining, with the following beneficial effects:

[0012] 1、the feeding mechanism for aero-engine parts machining, by being provided with outer feeding port, outer feeding port side fixed installation has annular rubber sealing block, annular rubber sealing block inner side and outer feeding port outer side form cavity, when feeding, annular rubber sealing block side can be tightly attached with the side of feeding cylinder, so that the volatile coating can be kept in cavity, by connecting pipe flow into the absorbent in absorption cylinder, so that volatile coating can be absorbed, to reduce air pollution in turn.

[0013] 2、the feeding mechanism for aero-engine parts machining, by the cooperation of weighing rod and weighing plate, when weight value reaches corresponding set value, the rotation of threaded rod can be controlled by controller, so as to automatically open and close inner feeding port. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 for the three-dimensional overall installation drawing of the utility model structure;

[0015] Figure 2 for the internal structure diagram of the utility model structure box body;

[0016] Figure 3The utility model discloses a structure outer feeding opening structure connection diagram.

[0017] Figure 4 The utility model discloses a structure annular rubber seal stop block structure diagram.

[0018] 1, box, 11, vacuum layer, 12, water layer, 13, coating layer, 14, cover plate, 15, drive arrangement, 16, feed inlet, 17, refrigerator, 2, outer feeding opening, 21, annular rubber seal stop block, 22, connecting pipe, 23, absorption cylinder, 231, inlet, 232, outlet, 24, inner feeding opening, 25, slot block, 26, threaded rod, 27, lock hole block, 28, spring, 29, spring plate, 3, controller, 31, weighing lever, 32, weighing plate, 4, support block. DETAILED DESCRIPTION

[0019] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative work belong to the scope of protection of the utility model.

[0020] Please refer to Figures 1-4 A kind of feeding mechanism for aero-engine parts machining, including box 1, box 1 bottom is fixedly connected with outer feeding opening 2, outer feeding opening 2 side wall is fixedly installed with annular rubber seal stop block 21, annular rubber seal stop block 21 inner side and outer feeding opening 2 side form cavity, annular rubber seal stop block 21 top is fixedly connected with connecting pipe 22, connecting pipe 22 other end is fixedly connected with absorption cylinder 23, absorption cylinder 23 top and box 1 bottom side are fixedly connected, absorption cylinder 23 side is fixedly installed with inlet 231 and outlet 232.

[0021] Through the above technical scheme, by being provided with outer feeding opening 2, outer feeding opening 2 side is fixedly installed with annular rubber seal stop block 21, annular rubber seal stop block 21 inner side and outer feeding opening 2 outer side form cavity, when feeding, annular rubber seal stop block 21 side can be tightly combined with the side of feeding cylinder, so that volatile coating can be kept in cavity, by connecting pipe 22 flow into the absorbent in absorption cylinder 23, so that volatile coating can be absorbed, and then atmospheric pollution can be reduced.

[0022] Specifically, the inner feeding port 24 is internally provided with a slot block 25 fixedly installed on the inner wall, the slot block 25 is movably installed with a threaded rod 26, the threaded rod 26 is threadedly connected with a lock hole block 27, the bottom of the outer feeding port 2 is fixedly installed with a spring 28, and the other end of the spring 28 is fixedly installed with a spring plate 29.

[0023] Through the above technical scheme, by setting the inner feeding port 24, the inner feeding port 24 can be directly connected with the feeding cylinder, the rotation of the threaded rod 26 can control the movement of the lock hole block 27 in the slot block 25, so as to control the opening and closing of the inner feeding port 24, and by setting the spring 28 fixedly installed at the bottom of the outer feeding port 2 and the spring plate 29 fixedly installed at the other end of the spring 28, the feeding cylinder can be loaded.

[0024] Specifically, the threaded rod 26 is fixedly connected with a controller 3 at one end outside the outer feeding port 2, the controller 3 is fixedly installed with a weighing rod 31 at the bottom, and the other end of the weighing rod 31 is fixedly connected with a weighing plate 32.

[0025] Through the above technical scheme, by setting the controller 3, when the corresponding value is set in the controller 3, the rotation of the threaded rod 26 can be controlled by the controller 3 through the cooperation of the weighing rod 31 and the weighing plate 32 when the weight value reaches the corresponding set value, so as to automatically open and close the inner feeding port 24.

[0026] Specifically, the bottom of the box body 1 is fixedly installed with a support block 4 at each corner, and the side surface of the four support blocks 4 is fixedly connected with the side surface of the weighing plate 32.

[0027] Through the above technical scheme, by setting the support block 4, the device can be supported, and the weighing plate 32 can be fixed.

[0028] Specifically, the box body 1 is internally provided with a vacuum layer 11, a water layer 12 and a coating layer 13, the top of the box body 1 is fixedly installed with a cover plate 14, the cover plate 14 is fixedly installed with a driving device 15 and a feeding port 16, the side surface of the box body 1 is fixedly installed with a refrigeration device 17, the side surface of the refrigeration device 17 is fixedly installed with a connecting pipeline, and the other end of the connecting pipeline is communicated with the water layer 12.

[0029] Through the above technical scheme, by setting the vacuum layer 11, the water layer 12 and the coating layer 13, the water layer 12 inside can be refrigerated by the refrigeration device 17, the setting of the vacuum layer 11 can slow down the emission of cold air, so that the coating layer 13 can maintain a low temperature state, thereby inhibiting volatilization.

[0030] In use, by setting the weighing value of the controller 3, the corresponding canister is placed in the designated position, the corresponding button of the controller 3 is pressed to control the opening of the inner feeding opening 24, the outer feeding opening 2 is provided, the annular rubber sealing block 21 is fixedly installed on the side of the outer feeding opening 2, the inner side of the annular rubber sealing block 21 and the outer side of the outer feeding opening 2 form a cavity, when feeding, the side of the annular rubber sealing block 21 can be tightly attached to the side of the feeding cylinder, so that the volatile paint can be left in the cavity, and the volatile paint can be absorbed into the absorbent in the absorption cylinder 23 through the connecting pipe 22, so that the volatile paint can be absorbed, and air pollution can be reduced, when the weight value reaches the corresponding set value, the rotation of the threaded rod 26 can be controlled by the controller 3, so that the inner feeding opening 24 can be automatically opened and closed.

[0031] Although the embodiments of the present application have been shown and described, it should be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present application, and the scope of the present application is defined by the appended claims and their equivalents.

Claims

1. A feeding mechanism for processing aero-engine parts, comprising a housing (1), characterized in that: The bottom of the box (1) is fixedly connected to an external feeding port (2). An annular rubber sealing block (21) is fixedly installed on the side wall of the external feeding port (2). The inner side of the annular rubber sealing block (21) forms a cavity with the side of the external feeding port (2). The top of the annular rubber sealing block (21) is fixedly connected to a connecting pipe (22). The other end of the connecting pipe (22) is fixedly connected to an absorption cylinder (23). The top of the absorption cylinder (23) is fixedly connected to the bottom side of the box (1). (23) An inlet (231) and an outlet (232) are fixedly installed on the side. An inner feed port (24) is provided inside the outer feed port (2). A slotted block (25) is fixedly installed on the inner wall of the inner feed port (24). A threaded rod (26) is movably installed inside the slotted block (25). A locking block (27) is threadedly connected to the threaded rod (26). A spring (28) is fixedly installed at the bottom of the outer feed port (2). A spring plate (29) is fixedly installed at the other end of the spring (28).

2. The feeding mechanism for processing aero-engine parts according to claim 1, characterized in that: The threaded rod (26) passes through the outside of the outer feed port (2) and is fixedly connected to a controller (3). A weighing rod (31) is fixedly installed at the bottom of the controller (3), and a weighing plate (32) is fixedly connected to the other end of the weighing rod (31).

3. The feeding mechanism for processing aero-engine parts according to claim 2, characterized in that: Support blocks (4) are fixedly installed at the four corners of the bottom of the box (1), and the sides of the four support blocks (4) are fixedly connected to the sides of the weighing plate (32).

4. The feeding mechanism for processing aero-engine parts according to claim 1, characterized in that: The box (1) is provided with a vacuum layer (11), a water layer (12) and a coating layer (13). A cover plate (14) is fixedly installed on the top of the box (1). A drive device (15) and a feed inlet (16) are fixedly installed on the cover plate (14). A cooler (17) is fixedly installed on the side of the box (1). A connecting pipe is fixedly installed on the side of the cooler (17). The other end of the connecting pipe is connected to the water layer (12).

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