CN216579125U - Novel plastic straight machine head - Google Patents
Novel plastic straight machine head Download PDFInfo
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- CN216579125U CN216579125U CN202123391632.XU CN202123391632U CN216579125U CN 216579125 U CN216579125 U CN 216579125U CN 202123391632 U CN202123391632 U CN 202123391632U CN 216579125 U CN216579125 U CN 216579125U
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Abstract
The utility model relates to a novel straight aircraft nose of plastics, including the connecting main body, one side of connecting main body is provided with the fixed block, the outside of connecting main body and fixed block is provided with protection machanism, protection machanism includes first guard ring and second guard ring, first guard ring is located the outside of connecting main body, the second guard ring is located the outside of fixed block. This novel straight aircraft nose of plastics, through setting up the outside first protective ring of connecting main part and the outside second protective ring of fixed block, can stably protect connecting main part and fixed block, again through setting up the fixed screw, can adjust and control the fixed of connecting main part and fixed block and dismantle, the inside first water conservancy diversion piece that sets up of connecting main part and the inside second water conservancy diversion piece that sets up of fixed block are cooperated again, transmit the inside of second water conservancy diversion piece through first water conservancy diversion piece to the material, the transmission of convenient control material, it is convenient to guarantee that the integral erection dismantles, excellent in practical effect, user's use has been made things convenient for.
Description
Technical Field
The utility model relates to a straight aircraft nose technical field specifically is novel straight aircraft nose of plastics.
Background
The extruder belongs to one of the types of plastic machinery, originates from the eighteenth century, can divide the aircraft nose into right angle aircraft nose and bevel nose etc. according to aircraft nose material flow direction and the contained angle of screw rod central line, and the screw extruder relies on pressure and shearing force that the screw rod rotation produced, can make the material fully carry out plastify and evenly mix, and through the bush shaping, the plastic extruder can be classified into double screw extruder, single screw extruder and rare many screw rod extruder and no screw rod extruder basically.
Along with the development of scientific technology, plastics also account for more effects in people's life, the straight aircraft nose of plastics that use at present often the water conservancy diversion mechanism is not convenient for adjust, and often needs the aircraft nose design of overlength, leads to people wholly to install when using and use also comparatively inconvenient, so has proposed the straight aircraft nose of plastics and has solved this problem.
SUMMERY OF THE UTILITY MODEL
The not enough to prior art, the utility model provides a novel straight aircraft nose of plastics possesses installation and the dismantlement that straight aircraft nose can be convenient, can convenient maintenance straight aircraft nose advantage such as, has solved the problem that integral erection used also comparatively inconvenient.
In order to achieve the above object, the utility model provides a following technical scheme: the novel plastic straight machine head comprises a connecting main body, wherein a fixed block is arranged on one side of the connecting main body, and a protection mechanism is arranged outside the connecting main body and the fixed block;
the protection mechanism includes first protection ring and second protection ring, first protection ring is located the outside of connecting the main part, the second protection ring is located the outside of fixed block, the outside threaded connection of first protection ring has first fixed silk, the outside threaded connection of fixed block has the fixed silk of second, be provided with the shock pad between connecting main part and the fixed block.
Further, the connecting body comprises two cylinders, a feeding hole is formed in one side of the connecting body, and screw grooves which are uniformly distributed are formed in the outer portion of the connecting body.
Furthermore, the connecting body is cylindrical, and fixing screws which are uniformly distributed are arranged outside the connecting body.
Further, the inner wall sliding connection of feed port has first water conservancy diversion piece, the material through hole has been seted up to one side of first water conservancy diversion piece.
Further, the fixed block is cylindric, the discharge opening has been seted up to one side of fixed block, the discharge opening comprises the circular cone groove that quantity is two, and two circular cone grooves link to each other, the inside of discharge opening is provided with the second water conservancy diversion piece, fixed block and fixed screw threaded connection.
Further, the second water conservancy diversion piece is conical, the material through hole has been seted up to one side of second water conservancy diversion piece, the fixed slot that evenly distributes and quantity is no less than four is seted up to the outside of second water conservancy diversion piece.
Compared with the prior art, the technical scheme of the application has the following beneficial effects:
this novel straight aircraft nose of plastics, through setting up the outside first protective ring of connecting main part and the outside second protective ring of fixed block, can stably protect connecting main part and fixed block, again through setting up the fixed screw, can adjust and control the fixed of connecting main part and fixed block and dismantle, the inside first water conservancy diversion piece that sets up of connecting main part and the inside second water conservancy diversion piece that sets up of fixed block are cooperated again, transmit the inside of second water conservancy diversion piece through first water conservancy diversion piece to the material, the transmission of convenient control material, it is convenient to guarantee that the integral erection dismantles, excellent in practical effect, user's use has been made things convenient for.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a top view of the present invention.
In the figure: the device comprises a connecting main body 1, a first flow guide block 2, a first protective ring 3, a fixing screw 4, a shock absorption pad 5, a second protective ring 6, a fixing block 7, a second flow guide block 8, a feeding hole 11, a first fixing wire 31, a second fixing wire 71 and a discharging hole 72.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, the novel plastic straight machine head of the present embodiment includes a connecting body 1, a fixing block 7 is disposed on one side of the connecting body 1, and a protection mechanism is disposed outside the connecting body 1 and the fixing block 7.
In this embodiment, connecting body 1 comprises the cylinder that quantity is two, and feed port 11 has been seted up to one side of connecting body 1, and the inner wall sliding connection of feed port 11 has first water conservancy diversion piece 2, and logical material hole has been seted up to one side of first water conservancy diversion piece 2, and connecting body 1 is cylindricly, and connecting body 1's outside is provided with the even fixed screw 4 that distributes, and the even screw groove that distributes has been seted up to connecting body 1's outside.
In this embodiment, the protection mechanism includes first protection ring 3 and second protection ring 6, first protection ring 3 is located the outside of connecting main body 1, second protection ring 6 is located the outside of fixed block 7, be provided with shock pad 5 between connecting main body 1 and the fixed block 7, the outside threaded connection of first protection ring 3 has first fixed silk 31, the outside threaded connection of fixed block 7 has second fixed silk 71, fixed block 7 is cylindricly, discharge opening 72 has been seted up to one side of fixed block 7, discharge opening 72 comprises the circular cone groove that quantity is two, two circular cone grooves link to each other, the inside of discharge opening 72 is provided with second water conservancy diversion piece 8, second water conservancy diversion piece 8 is the cone shape, the material through hole has been seted up to one side of second water conservancy diversion piece 8, the outside of second water conservancy diversion piece 8 has been seted up and has been distributed evenly and quantity and be no less than four fixed slots, fixed block 7 and fixed screw 4 threaded connection.
The working principle of the above embodiment is as follows:
this novel straight aircraft nose of plastics, through setting up the outside first protective ring 3 of connecting main part 1 outside and the outside second protective ring 6 of fixed block 7, can stably protect connecting main part 1 and fixed block 7, again through setting up fixed screw 4, can adjust and control the fixed of connecting main part 1 and fixed block 7 and dismantle, the inside first water conservancy diversion piece 2 that sets up of connecting main part 1 and the inside second water conservancy diversion piece 8 that sets up of fixed block 7 of cooperation again, transmit the inside to second water conservancy diversion piece 8 through first water conservancy diversion piece 2 through the material, the transmission of convenient control material, guarantee that the integral erection dismantles conveniently, excellent in practical effect, user's use has been made things convenient for.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. Novel straight aircraft nose of plastics, including connecting main part (1), its characterized in that: a fixed block (7) is arranged on one side of the connecting main body (1), and a protection mechanism is arranged outside the connecting main body (1) and the fixed block (7);
protection machanism includes first protection ring (3) and second protection ring (6), first protection ring (3) are located the outside of connecting main part (1), second protection ring (6) are located the outside of fixed block (7), the outside threaded connection of first protection ring (3) has first fixed silk (31), the outside threaded connection of fixed block (7) has the fixed silk of second (71), be provided with shock pad (5) between connecting main part (1) and fixed block (7).
2. The new plastic straight handpiece of claim 1, characterized in that: connecting body (1) comprises the cylinder that quantity is two, feed port (11) have been seted up to one side of connecting body (1), the even screw groove that distributes has been seted up to the outside of connecting body (1).
3. The new plastic straight handpiece of claim 2, characterized in that: connecting body (1) is cylindricly, connecting body (1)'s outside is provided with evenly distributed set screw (4).
4. The new plastic straight handpiece of claim 2, characterized in that: the inner wall of the feed port (11) is connected with a first flow guide block (2) in a sliding mode, and a feed through hole is formed in one side of the first flow guide block (2).
5. The new plastic straight handpiece of claim 1, characterized in that: the fixed block (7) is cylindric, discharge opening (72) have been seted up to one side of fixed block (7), discharge opening (72) comprise the circular cone groove that quantity is two, and two circular cone grooves link to each other, the inside of discharge opening (72) is provided with second water conservancy diversion piece (8), fixed block (7) and fixed screw (4) threaded connection.
6. The new plastic straight handpiece of claim 5, characterized in that: the second flow guide block (8) is conical, a material passing hole is formed in one side of the second flow guide block (8), and fixing grooves which are uniformly distributed and are not less than four in number are formed in the outer portion of the second flow guide block (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123391632.XU CN216579125U (en) | 2021-12-30 | 2021-12-30 | Novel plastic straight machine head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123391632.XU CN216579125U (en) | 2021-12-30 | 2021-12-30 | Novel plastic straight machine head |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216579125U true CN216579125U (en) | 2022-05-24 |
Family
ID=81631693
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123391632.XU Active CN216579125U (en) | 2021-12-30 | 2021-12-30 | Novel plastic straight machine head |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216579125U (en) |
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2021
- 2021-12-30 CN CN202123391632.XU patent/CN216579125U/en active Active
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