CN213499018U - Spacecraft composite film processing pressure regulator - Google Patents
Spacecraft composite film processing pressure regulator Download PDFInfo
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- CN213499018U CN213499018U CN202022427000.3U CN202022427000U CN213499018U CN 213499018 U CN213499018 U CN 213499018U CN 202022427000 U CN202022427000 U CN 202022427000U CN 213499018 U CN213499018 U CN 213499018U
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Abstract
The utility model belongs to the technical field of the spacecraft complex film, concretely relates to spacecraft complex film processing voltage regulator, including the mounting bracket, adjusting chute has been seted up to one side of mounting bracket, and adjusting chute's inboard both ends sliding connection has adjusting seat and alignment jig respectively, and the inboard of alignment jig is rotated through the bearing and is connected with the compression roller, rotates through the bearing in the adjusting seat to be connected with accommodate the lead screw, and the one end of accommodate the lead screw is through bolt fixedly connected with hand wheel, and lead screw nut has been cup jointed in accommodate the lead screw's the outside, and one side of lead screw nut is rotated through the pivot and; the utility model discloses an accommodate the lead screw, screw-nut and the regulation ejector pin of design rotate accommodate the lead screw through the hand wheel and drive screw-nut and remove when using to push up the position control that the alignment jig slided the compression roller through adjusting the ejector pin, thereby adjust the pressure of compression roller to the complex film of process, more convenient and can carry out the regulation of arbitrary distance as required when adjusting.
Description
Technical Field
The utility model relates to a spacecraft complex film technical field specifically is a spacecraft complex film processing voltage regulator.
Background
The composite membrane is a separation membrane which is formed by taking a microporous membrane or an ultrafiltration membrane as a nominal layer and covering the surface of the composite membrane with a dense homogeneous membrane with the thickness of only 0.1-0.25 mu m as a barrier layer. So that the permeation amount of the substance is greatly increased. The composite membrane material includes any possible combination of materials, such as ceramic membrane on metal oxide or aromatic polyamide membrane on polysulfone microporous membrane, and the flat membrane or the roll membrane is reinforced with non-woven fabric to support the pressure resistance of the microporous membrane, while the hollow fiber membrane is not needed.
The voltage regulator of current spacecraft complex film processing usefulness when using, adjusts through the position for the compression roller to adjust the pressure to the complex film of process, fix then the adjusting position through the bolt usually when adjusting, comparatively troublesome and adjusting position is fixed when adjusting, consequently, technical personnel in the field provide a spacecraft complex film processing voltage regulator, in order to solve the problem that proposes in the above-mentioned background art.
Disclosure of Invention
An object of the utility model is to provide a spacecraft complex film processing voltage regulator has solved the voltage regulator of current spacecraft complex film processing usefulness and when using, adjusts through the position for the compression roller to adjust the pressure to the complex film of process, fix then adjusting position through the bolt usually when adjusting, comparatively troublesome and adjusting position fixed problem when adjusting.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a spacecraft complex film processing voltage regulator, includes the mounting bracket, the regulation spout has been seted up to one side of mounting bracket, the inboard both ends of adjusting the spout sliding connection respectively have adjusting seat and alignment jig, the inboard of alignment jig is rotated through the bearing and is connected with the compression roller, rotate through the bearing in the adjusting seat and be connected with accommodate the lead screw, bolt fixedly connected with hand wheel is passed through to accommodate the lead screw's one end, screw-nut has been cup jointed in accommodate the lead screw's the outside, one side of screw-nut rotates through the pivot and is connected with the regulation ejector pin, the one end of adjusting the ejector pin is rotated through rotating in the pivot and is connected with the regulation kicking block, the inboard upper end of mounting bracket and the upside of alignment jig all are provided with coupling mechanism.
Preferably, the two ends of the adjusting screw rod are provided with screw rod nuts, the two screw rod nuts are symmetrically sleeved on the adjusting screw rod, and the thread turning directions of the surfaces of the two ends of the adjusting screw rod are opposite.
Preferably, coupling mechanism includes connection slot, connection cardboard and connects the briquetting, connection slot sets up the inboard upper end surface at the mounting bracket and the upside surface of alignment jig, connect the cardboard setting in one side of adjusting the kicking block, and adjust the kicking block and connect cardboard formula structure as an organic whole, connection slot's one end sliding connection has the connection briquetting, one side of connecting the briquetting is provided with the knob screw, the knob screw closes with the alignment jig and the mounting bracket through the screw thread soon and is connected.
Preferably, the connecting clamping plate is in a dovetail shape, and one end of the connecting slot, which is connected with the pressing block, is respectively pressed and clamped on the connecting clamping plate.
Preferably, the cross section of the adjusting ejector block is U-shaped, and adjusting ejector rods are connected to two sides of the adjusting ejector block.
Preferably, the inner sides of the two ends of the mounting rack are both connected with press rollers.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses an accommodate the lead screw, screw-nut and the regulation ejector pin of design rotate accommodate the lead screw through the hand wheel and drive screw-nut and remove when using to push up the position control that the alignment jig slided the compression roller through adjusting the ejector pin, thereby adjust the pressure of compression roller to the complex film of process, more convenient and can carry out the regulation of arbitrary distance as required when adjusting.
2. The utility model discloses a connection cardboard of design with connect the briquetting, need change the compression roller when using the compression roller, can drive to connect the briquetting through rotating the knob screw and put aside or sticiss from connecting the cardboard and carry out the dismouting, convenient and fast more when changing on connecting the cardboard.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the connecting mechanism of the present invention;
fig. 3 is a schematic side view of the present invention.
In the figure: 1. an adjusting bracket; 2. a mounting frame; 3. adjusting the screw rod; 4. a feed screw nut; 5. adjusting the ejector rod; 6. adjusting the top block; 7. a connecting mechanism; 8. a hand wheel; 9. an adjusting seat; 10. a knob screw; 11. a compression roller; 12. connecting the slots; 13. connecting a clamping plate; 14. connecting the pressing blocks; 15. and adjusting the sliding chute.
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.
Examples
Referring to fig. 1-3, a spacecraft composite membrane processing pressure regulator comprises a mounting frame 2, an adjusting chute 15 is formed in one side of the mounting frame 2, an adjusting seat 9 and an adjusting frame 1 are respectively connected to the two ends of the inner side of the adjusting chute 15 in a sliding manner, a press roller 11 is rotatably connected to the inner side of the adjusting frame 1 through a bearing, an adjusting screw rod 3 is rotatably connected to the inner side of the adjusting seat 9 through a bearing, a hand wheel 8 is fixedly connected to one end of the adjusting screw rod 3 through a bolt, a screw nut 4 is sleeved on the outer side of the adjusting screw rod 3, an adjusting ejector rod 5 is rotatably connected to one side of the screw nut 4 through a rotating shaft, an adjusting ejector block 6 is rotatably connected to one end of the adjusting ejector rod 5 through the rotating shaft, connecting mechanisms 7 are respectively arranged at the upper end of the inner side of the mounting frame 2 and the upper side of the adjusting frame 1, lead screw nuts 4 sleeved at two ends of the adjusting lead screw 3 relatively run, so that an adjusting ejector rod 5 is driven to rotate, and the adjusting ejector block 6 is pushed to drive the adjusting frame 1 and the compression roller 11 to slide and adjust the position.
Referring to fig. 1, the two ends of the adjusting screw rod 3 are both provided with the screw rod nuts 4, the two screw rod nuts 4 are symmetrically sleeved on the adjusting screw rod 3, and the thread turning directions of the surfaces of the two ends of the adjusting screw rod 3 are opposite, so that the adjusting screw rod 3 drives the screw rod nuts 4 to move and push the adjusting frame 1 to slide and adjust.
Please refer to fig. 1-2, the connecting mechanism 7 includes a connecting slot 12, a connecting clamp plate 13 and a connecting press block 14, the connecting slot 12 is disposed on the inner upper end surface of the mounting frame 2 and the upper side surface of the adjusting frame 1, the connecting clamp plate 13 is disposed on one side of the adjusting top block 6, and the adjusting top block 6 and the connecting clamp plate 13 are of an integrated structure, one end of the connecting slot 12 is slidably connected with the connecting press block 14, one side of the connecting press block 14 is provided with a knob screw 10, the knob screw 10 is screwed with the adjusting frame 1 and the mounting frame 2 through threads, and the connecting press block 14 is driven by rotating the knob screw 10 to move away from the connecting clamp plate 13 or tightly press the connecting clamp plate 13 for dismounting.
Referring to fig. 2, the connecting card 13 is shaped like a dovetail, and one end of the connecting slot 12 is connected to one end of the pressing block 14 and is respectively pressed and fastened on the connecting card 13.
Referring to fig. 2, the cross-sectional shape of the adjusting ejector block 6 is U-shaped, and the adjusting ejector rods 5 are connected to both sides of the adjusting ejector block 6, so that the adjusting ejector rods 5 are more stable when the adjusting ejector block 6 is pushed to adjust the position.
Referring to fig. 3, the inner sides of the two ends of the mounting frame 2 are both connected with press rollers 11, so that the spacecraft composite membrane can be pressed gradually.
The utility model discloses the concrete implementation process as follows: when the spacecraft composite membrane pressing device is used, the hand wheel 8 is rotated as required to drive the adjusting screw rod 3 to rotate, so that the screw rod nuts 4 sleeved at two ends of the adjusting screw rod 3 relatively run, the adjusting ejector rod 5 is driven to rotate, the adjusting ejector block 6 is pushed to drive the adjusting frame 1 to slide to adjust the position, the adjusting seat 9 slides along with the adjusting frame 1 when the adjusting frame 1 slides, the adjusting is more convenient and can adjust any distance as required, the pressing rollers 11 at two ends of the mounting frame 2 can gradually press the spacecraft composite membrane as required, when the situation that the pressing rollers 11 are damaged and need to be replaced after long-term use is realized, the connecting pressing block 14 is driven to slide in the connecting slot 12 by manually rotating the knob screw 10, the connecting pressing block 14 can be pulled out from the connecting slot 12 after being moved away from the connecting pressing plate 13, and then the adjusting frame 1 and the pressing rollers 11 are detached to be, during installation, only the connecting clamping plate 13 on the adjusting jacking block 6 needs to be inserted into the connecting slot 12, the knob screw 10 is screwed to push the connecting pressing block 14 to be tightly pressed on the connecting clamping plate 13, and the assembling and disassembling are more convenient and rapid.
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. The utility model provides a spacecraft complex film processing voltage regulator, includes mounting bracket (2), its characterized in that: adjusting chute (15) have been seted up to one side of mounting bracket (2), there are regulation seat (9) and alignment jig (1) inboard both ends of adjusting chute (15) sliding connection respectively, the inboard of alignment jig (1) is rotated through the bearing and is connected with compression roller (11), rotate through the bearing in regulation seat (9) and be connected with accommodate the lead screw (3), bolt fixedly connected with hand wheel (8) are passed through to the one end of accommodate the lead screw (3), screw-nut (4) have been cup jointed in the outside of accommodate the lead screw (3), one side of screw-nut (4) is rotated through the pivot and is connected with regulation ejector pin (5), the one end of adjusting ejector pin (5) is through rotating in the pivot and being connected with regulation kicking block (6), the inboard upper end of mounting bracket (2) and the upside of alignment jig (1) all are provided with coupling mechanism (7), alignment jig (1) and mounting bracket (2) are through coupling mechanism (7) and regulation kicking block (6 .
2. A spacecraft composite membrane processing pressure regulator according to claim 1, characterized in that: the two ends of the adjusting screw rod (3) are provided with screw rod nuts (4), the two screw rod nuts (4) are symmetrically sleeved on the adjusting screw rod (3), and the thread turning directions of the surfaces of the two ends of the adjusting screw rod (3) are opposite.
3. A spacecraft composite membrane processing pressure regulator according to claim 1, characterized in that: coupling mechanism (7) are including connection slot (12), connection cardboard (13) and connection briquetting (14), connection slot (12) are seted up at the inboard upper end surface of mounting bracket (2) and the upside surface of alignment jig (1), connect cardboard (13) and set up in the one side of adjusting kicking block (6), and adjust kicking block (6) and connect cardboard (13) formula structure as an organic whole, the one end sliding connection of connection slot (12) has connection briquetting (14), one side of connecting briquetting (14) is provided with knob screw (10), knob screw (10) close soon with alignment jig (1) and mounting bracket (2) through the screw thread and are connected.
4. A spacecraft composite membrane processing pressure regulator according to claim 3, wherein: the connecting clamping plate (13) is in a dovetail shape, and one end of the connecting slot (12) connected with one end of the pressing block (14) is respectively pressed and clamped on the connecting clamping plate (13).
5. A spacecraft composite membrane processing pressure regulator according to claim 1, characterized in that: the cross-sectional shape of adjusting kicking block (6) sets up to the U type, and adjusts the both sides of kicking block (6) and all is connected with and adjusts ejector pin (5).
6. A spacecraft composite membrane processing pressure regulator according to claim 1, characterized in that: the inner sides of the two ends of the mounting rack (2) are both connected with press rollers (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022427000.3U CN213499018U (en) | 2020-10-28 | 2020-10-28 | Spacecraft composite film processing pressure regulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022427000.3U CN213499018U (en) | 2020-10-28 | 2020-10-28 | Spacecraft composite film processing pressure regulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213499018U true CN213499018U (en) | 2021-06-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022427000.3U Active CN213499018U (en) | 2020-10-28 | 2020-10-28 | Spacecraft composite film processing pressure regulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213499018U (en) |
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2020
- 2020-10-28 CN CN202022427000.3U patent/CN213499018U/en active Active
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