CN114011665A - Clamp for air rudder - Google Patents
Clamp for air rudder Download PDFInfo
- Publication number
- CN114011665A CN114011665A CN202111322009.0A CN202111322009A CN114011665A CN 114011665 A CN114011665 A CN 114011665A CN 202111322009 A CN202111322009 A CN 202111322009A CN 114011665 A CN114011665 A CN 114011665A
- Authority
- CN
- China
- Prior art keywords
- hole
- fixing
- unit
- clamp
- link
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C—APPARATUS FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C13/00—Means for manipulating or holding work, e.g. for separate articles
- B05C13/02—Means for manipulating or holding work, e.g. for separate articles for particular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B13/00—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
- B05B13/02—Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
- B05B13/0285—Stands for supporting individual articles to be sprayed, e.g. doors, vehicle body parts
Abstract
The invention discloses a clamp for an air rudder, which is used for fixing a shaft core of the air rudder, wherein shaft holes are formed in two sides of the shaft core, and the clamp comprises: the connecting rod unit, the fixing units and the sleeve are arranged, a first hole and a second hole are formed in two sides of the sleeve, at least two fixing units are arranged, one ends of the at least two fixing units are connected with the connecting rod unit, and the other ends of the at least two fixing units are inserted into the first hole and the second hole respectively; the shaft core to be processed is placed in the sleeve, the connecting rod unit moves upwards or downwards to drive the fixing unit to move in the first hole and the second hole towards the direction close to or far away from the shaft core, and the shaft core is clamped or loosened; in the related art, an iron wire penetrates through a shaft hole in a shaft core of the air rudder, and then the iron wire is hung on the hook, so that the fixing effect is poor, and when the air rudder needs to be taken down after processing is finished, the iron wire can be unscrewed manually only, and then the air rudder is taken down; after the processing is finished, the invention only needs to control the connecting rod unit to move downwards, and is convenient to use.
Description
Technical Field
The invention relates to the technical field of air rudders, in particular to a clamp for an air rudder.
Background
Air rudders are one of the important components on aerospace vehicles for altering the air flow and thereby adjusting the flight state of the vehicle. In the production of air vane, need hoist the air vane and get up to brush and glue or the spraying, traditional method is to pass the shaft hole on the axle core of air vane with the iron wire, then hang the iron wire on the couple, later send into brush and glue the room and spray booth through the mode that the chain was carried, wait to spout after the paint is dried then need the manual work to take off the air vane and put on goods shelves, this method not only fixed effect is not good, influence brush and glue and spraying quality, and the operation is complicated moreover, and the operating time has been increased, and the work efficiency is reduced.
Disclosure of Invention
In view of this, the present invention provides a clamp for an air vane, which solves the problem of poor fixing effect of the air vane in the prior art through the cooperation between a connecting rod unit, a fixing unit and a sleeve.
In order to solve the above problem, an embodiment of the present invention provides a clamp for an air rudder, which is used for fixing a shaft core of the air rudder, wherein shaft holes are formed on two sides of the shaft core, and the clamp includes: the connecting rod unit, the fixing units and the sleeve are arranged, a first hole and a second hole corresponding to the shaft holes are formed in the two sides of the sleeve, at least two fixing units are arranged, one ends of the at least two fixing units are connected with the connecting rod unit, and the other ends of the at least two fixing units are inserted into the first hole and the second hole respectively;
the shaft core of the air rudder to be processed is arranged in the sleeve, and the connecting rod unit drives the fixing unit to move in the first hole and the second hole towards the direction close to the shaft core, so that the shaft core is clamped.
In some embodiments, the link unit includes a guide rod, a slider, a first link and a second link, the slider is located on the guide rod, the guide rod drives the slider to move up and down, one end of each of the first link and the second link is connected to the slider, and the other end of each of the first link and the second link is connected to the corresponding fixing unit.
In some embodiments, the fixing unit includes a first fixing rod having one end connected to the first link and the other end inserted into the first hole, and a second fixing rod having one end connected to the second link and the other end inserted into the second hole.
In some embodiments, the first fixing rod and/or the second fixing rod are/is a pin, the pin is connected with the corresponding first connecting rod or the second connecting rod by a pin shaft, and a guide part is arranged at one end of the pin inserted into the first hole and the second hole.
In some embodiments, the link unit further comprises a guard structure surrounded by the baffle, and the guide rod is located in the guard structure and extends out of the guard structure at an end thereof remote from the sleeve.
In some embodiments, the link unit further includes a limiting structure located on an upper surface of the protective structure, the guide rod passes through the limiting structure, and the limiting structure is used for limiting a limiting position of the guide rod when the guide rod moves downwards.
In some embodiments, the link unit further comprises a positioning structure connecting the guide bar with the guard structure for preventing the guide bar from sliding down.
In some embodiments, the sleeve includes the body, and the cover is equipped with the thickening layer on the periphery at first hole and second hole place on the body, offers the hole that corresponds with first hole and second hole on the thickening layer, and the thickening layer is used for preventing to produce when fixed unit removes to the axle center direction and rocks.
In some embodiments, the inner wall of the body and the surface of the fixing unit are both provided with a plastic layer or a rubber layer.
In some embodiments, the clamp further comprises a drive unit connected with the link unit for powering the same.
Compared with the prior art, the clamp for the air rudder has at least the following beneficial effects:
the shaft core of the air rudder to be processed is placed in the sleeve, the connecting rod unit moves upwards to drive the fixing unit to move in the first hole and the second hole towards the direction close to the shaft core, and the shaft core is clamped, and the clamp is in a first state; the connecting rod unit moves downwards to drive the fixing unit to move in the first hole and the second hole towards the direction far away from the shaft core, so that the shaft core is loosened, the shaft core can be easily pulled out at the moment, and the clamp is in a second state; the invention realizes the easy switching of two states by changing the moving direction of the connecting rod unit.
In the related art, an iron wire penetrates through a shaft hole in a shaft core of the air rudder, and then the iron wire is hung on the hook, under the condition, when the air rudder needs to be taken down after processing, the iron wire can be unscrewed only manually, and then the air rudder is taken down; after the processing is finished, the invention only needs to control the connecting rod unit to move downwards, and is convenient to use.
The air rudder clamping device is simple in structure, ingenious in conception, capable of clamping and fixing the air rudder by using fewer parts, and easy to popularize on an automatic production line of the air rudder.
The foregoing description is only an overview of the technical solutions of the present invention, and in order to make the technical solutions of the present invention more clearly understood and to implement them in accordance with the contents of the description, the following detailed description is given with reference to the preferred embodiments of the present invention and the accompanying drawings.
Drawings
Fig. 1 is a schematic structural view of a clamp for an air rudder according to an embodiment of the present invention;
fig. 2 is a sectional view of a clamp for an air rudder according to an embodiment of the present invention in an open state;
fig. 3 is a cross-sectional view of a clamp for an air vane according to an embodiment of the present invention in a clamped state;
fig. 4 is a schematic structural view of a bolt in a clamp for an air rudder according to an embodiment of the present invention;
FIG. 5a is a front view of a slider and guide rod mating in a clamp for an air rudder according to an embodiment of the present invention;
FIG. 5b is a side view of the slider and guide rod mating in a clamp for an air rudder according to an embodiment of the present invention;
fig. 6a is a cross-sectional view of a sleeve in a clamp for an air rudder according to an embodiment of the present invention;
FIG. 6b is a cross-sectional view of a sleeve and a portion of a pin of a clamp for an air vane in accordance with an embodiment of the present invention;
fig. 7 is a sectional view of a first link or a second link in a clamp for an air rudder according to an embodiment of the present invention;
FIG. 8a is a front view of a baffle in a clamp for an air rudder provided by an embodiment of the present invention;
FIG. 8b is a top view of a baffle in a clamp for an air rudder provided by an embodiment of the present invention;
FIG. 9a is a view of the positioning structure and the guide rod of a clamp for an air rudder according to an embodiment of the present invention;
FIG. 9b is a cross-sectional view taken along line A-A of FIG. 9 a;
fig. 10 is a schematic structural view of a limiting structure in a clamp for an air rudder according to an embodiment of the present invention.
Wherein:
100. a link unit; 200. a fixing unit; 300. a sleeve; 400. a shaft core; 101. a guide bar; 102. a slider; 103. a first link; 104. a second link; 105. a protective structure; 106. a limiting structure; 107. a positioning structure; 201. a first fixing lever; 202. a second fixing bar; 301. a body; 302. thickening the layer; 1051. a baffle plate; 1052. a groove; 1061. a limiting ring; 1062. and (4) screws.
Detailed Description
To further explain the technical means and effects of the present invention adopted to achieve the predetermined object, the following detailed description of the embodiments, structures, features and effects according to the present invention will be made with reference to the accompanying drawings and preferred embodiments. In the following description, different "one embodiment" or "an embodiment" refers to not necessarily the same embodiment. Furthermore, the particular features, structures, or characteristics may be combined in any suitable manner in one or more embodiments.
In the description of the present invention, it is to be understood that the terms "vertical", "lateral", "longitudinal", "front", "rear", "left", "right", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description of the present invention, and do not mean that the device or member to which the present invention is directed must have a specific orientation or position, and thus, cannot be construed as limiting the present invention.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The embodiment provides a anchor clamps for air vane, as shown in fig. 1, is used for fixing the axle core of air vane, and the axle hole has been seted up to the both sides of axle core, and anchor clamps include: link unit 100, fixed unit 200 and sleeve 300, the first hole and the second hole that correspond with the shaft hole are seted up to the both sides of sleeve 300, and fixed unit 200 is provided with at least two, and the one end of two at least fixed units 200 all is connected with link unit 100, and the other end of two at least fixed units 200 inserts respectively in first hole and the second hole. The shaft core of the air vane to be processed is arranged in the sleeve 300, and the connecting rod unit 100 drives the fixing unit 200 to move in the first hole and the second hole towards the direction close to the shaft core, so that the shaft core is clamped.
When the air rudder is fixed in the related art, an iron wire is manually passed through a shaft hole on a shaft core of the air rudder, then the iron wire is hung on the hook, and when the air rudder needs to be taken down after processing is finished, the iron wire can only be manually unscrewed, and then the air rudder is taken down; the fixing effect is poor, and the air rudder is troublesome to take down, time-consuming and labor-consuming; in this embodiment, the shaft core of the air vane to be processed is placed in the sleeve 300, and the connecting rod unit 100 moves upward to drive the two fixing units 200 to move in the first hole and the second hole respectively in the direction close to the shaft core, so as to clamp the shaft core; after the processing is finished, the connecting rod unit 100 moves downwards to drive the two fixing units 200 to move in the first hole and the second hole respectively towards the direction far away from the shaft core, so that the shaft core is loosened, and the shaft core can be easily pulled out of the sleeve 300; therefore, the clamp for the air rudder provided by the embodiment is convenient to use, and the working efficiency is improved.
Specifically, the sleeve 300 is a cylindrical hollow structure, one end of which is open and the other end of which is closed; more specifically, the lower end of the sleeve 300 is open, so that clamping can be easily achieved without moving the air rudder by aligning the open bottom of the sleeve 300 with the air rudder shaft core.
Specifically, the first hole and the second hole are provided in the side wall of the sleeve 300, and the first hole and the second hole are coaxial and are symmetrical about the axis of the sleeve 300, so that the stability of the air rudder when being clamped can be ensured.
In a specific embodiment:
as shown in fig. 1, the link unit 100 includes a guide rod 101, a slider 102, a first link 103 and a second link 104, the slider 102 is located on the guide rod 101, the guide rod 101 drives the slider 102 to move up and down, one end of each of the first link 103 and the second link 104 is connected to the slider 102, and the other end is connected to the corresponding fixing unit 200.
Thus, the guide rod 101 moves up and down, which drives the slider 102 to move up and down, and further drives the first link 103 and the second link 104 to move inward or outward.
Specifically, in the initial state, as shown in fig. 2, a portion of one end of the fixing unit 200 away from the link unit 100 is inserted into the first hole and the second hole, and when the guide rod 101 drives the slider 102 to move downward, the first link 103 and the second link 104 drive the fixing unit 200 to move in the direction approaching the shaft core in the first hole and the second hole, so as to clamp the shaft core 400, as shown in fig. 3.
After the air vane is machined, the guide rod 101 drives the sliding block 102 to move upwards, the first connecting rod 103 and the second connecting rod 104 drive the fixing unit 200 to move in the first hole and the second hole towards the direction far away from the shaft core, so that the shaft core 400 is loosened, and at the moment, the clamp returns to the initial state.
In a specific embodiment:
the fixing unit 200 includes a first fixing rod 201 and a second fixing rod 202, one end of the first fixing rod 201 is connected with the first link 103, the other end of the first fixing rod 201 is inserted into the first hole, one end of the second fixing rod 202 is connected with the second link 104, and the other end of the second fixing rod 202 is inserted into the second hole.
Specifically, the first fixing rod 201 and/or the second fixing rod 202 are/is a pin, and the pin is connected with the corresponding first connecting rod 103 or the second connecting rod 104 by a pin.
In order to facilitate the insertion of the inserted pin into the shaft hole of the air rudder shaft core 400, as shown in fig. 4, a guide portion is provided at one end of the inserted pin inserted into the first hole and the second hole, and the guide portion has an inclined angle or a rounded angle.
In addition, in order to prevent the metal on the surface of the bolt from colliding with the air rudder shaft handle, the surface of the bolt is sleeved with a plastic layer or a rubber layer.
In some of these embodiments:
as shown in fig. 1, the link unit 100 further includes a guard structure 105 surrounded by the baffle 1051, the guide rod 101 is located in the guard structure 105, and an end of the guide rod 101 away from the sleeve 300 extends out of the guard structure 105.
Specifically, the protective structure 105 includes a first baffle and a second baffle which are arranged oppositely, and further includes a top plate arranged on the first baffle and the second baffle, the first baffle, the second baffle and the top plate enclose a protective structure 105 with openings on two sides, wherein the openings on two sides are used for connecting a sliding block in the protective structure 105 with the first connecting rod 103 and the second connecting rod 104.
The slider 102 and the guide rod 101 are connected by a pin, and the inner surface of the baffle 1051 is provided with a groove 1052 for limiting the pin.
Specifically, as shown in fig. 8a and 8b, grooves 1052 are formed in the inner surfaces of the first baffle and the second baffle, the pin is located in the grooves 1052, and when the slider 102 moves up and down along the guide rod 101, the pin moves up and down along the grooves 1052, so that the pin is prevented from sliding out of the protective structure 105.
In some of these embodiments:
as shown in fig. 1, the link unit 100 further includes a limiting structure 106, the limiting structure 106 is located on the upper surface of the protective structure 105, the guide rod 101 passes through the limiting structure 106, and the limiting structure 106 is used for limiting the limiting position of the guide rod 101 when moving downwards.
The main function of the position-limiting structure 106 is to fix an initial position of the clamp, and in the initial position, the fixing unit 200, i.e., two pins, must be partially inserted into the first and second holes in an end thereof away from the link unit 100; if the two pins are not inserted into the corresponding first and second holes in the initial state, when the guide rod 101 drives the slider 102 to move downward, the first and second links 103 and 104 may drive the pins to move downward, and the pins cannot be inserted into the corresponding first and second holes.
Specifically, as shown in fig. 10, the limiting structure 106 includes a limiting ring 1061 and a screw 1062, the limiting ring 1061 is provided with a threaded hole, the guide rod 101 passes through the limiting ring 1061, and after the other end of the fixing unit 200 is inserted into the first hole and the second hole, the screw 1062 limits the guide rod 101 through the threaded hole.
Thus, the limiting ring 1061 is sleeved on the guide rod 101, and when a part of one end of each of the two pins far away from the link unit 100 is inserted into the first hole and the second hole, the guide rod 101 is locked by the screw 1062, which is the initial state of the clamp; of course, when the jig is operated, the screw 1062 needs to be operated so as not to interfere with the up-and-down movement of the guide bar 101.
In some of these embodiments:
as shown in fig. 9a and 9b, the link unit 100 further comprises a positioning structure 107, the positioning structure 107 connecting the guide bar 101 with the shielding structure 105 for preventing the guide bar 101 from sliding down.
Specifically, a first hole has been seted up on protective structure 105, and a second hole has been seted up to the position that guide arm 101 corresponds, and the one end of bolt passes through spring and first hole butt, and the other end passes the second hole, realizes the location to guide arm 101.
In some of these embodiments:
as shown in fig. 6a and 6b, the sleeve 300 includes a body 301, a thickening layer 302 is sleeved on a circumferential surface of the body 301 where the first hole and the second hole are located, holes corresponding to the first hole and the second hole are formed in the thickening layer 302, and the thickening layer 302 is used for preventing the fixing unit 200 from shaking when moving towards the axial direction.
Specifically, body 301 and thickening layer 302 integrated into one piece play spacing effect to the bolt, prevent that the bolt from rocking at the removal in-process.
In addition, in order to prevent the metal on the inner wall of the body 301 from colliding with the air rudder shaft handle, the inner wall of the body 301 is provided with a plastic layer or a rubber layer.
Specifically, the body 301 is a cylindrical hollow structure, one end of which is open, and the other end of which is closed; the guard structure 105 is fixed at its closed end.
In some of these embodiments:
the jig further includes a driving unit connected to the link unit 100 for providing power thereto, the driving unit being a motor or a cylinder.
In a specific embodiment:
the driving unit is connected with the mechanical arm.
In the related technology, an iron wire penetrates through a shaft hole on a shaft core of the air rudder, and then the iron wire is hung on the hook, and at the moment, if the air rudder needs to be moved, the hook needs to be moved, so that the stability is obviously poor; in the embodiment, the driving unit is controlled by the mechanical arm, so that the reliability is higher.
The using process of the invention is as follows:
initial state: parts of one ends of the two bolts far away from the connecting rod unit 100 are inserted into the corresponding first hole and the second hole, and the guide rod 101 is locked through the screw 1062 at the moment, so that the guide rod 101 is prevented from moving up and down;
when the air rudder needs to be clamped, the screw 1062 is operated to enable the screw to not affect the up-and-down movement of the guide rod 101, the driving unit (a motor or an air cylinder) drives the guide rod 101 to move upwards, the slider 102 moves upwards under the action of the guide rod 101, and the first connecting rod 103 and the second connecting rod 104 connected with the slider 102 drive the two bolts to move towards the direction close to the shaft core 400 in the first hole and the second hole respectively, so that the clamping of the shaft core 400 is realized; in this way, the air rudder needs to be moved, and the air rudder can be operated through the mechanical arm and moved to a proper position for processing;
after the machining is finished, the air rudder is moved to a proper position through the mechanical arm, then the driving unit (a motor or an air cylinder) drives the guide rod 101 to move downwards, the sliding block 102 moves downwards under the action of the guide rod 101, the first connecting rod 103 and the second connecting rod 104 which are connected with the sliding block 102 drive the two bolts to move towards the direction far away from the shaft core 400 in the first hole and the second hole respectively, the shaft core 400 is loosened, and at the moment, the clamp is lifted through the mechanical arm to take out the air rudder;
when the air vane is removed and the two pins are partially inserted into the corresponding first and second holes at the end of the link unit 100, the guide rod 101 is locked by the screw 1062, and the clamp is returned to the original state.
In summary, it is easily understood by those skilled in the art that the advantageous technical features described above can be freely combined and superimposed without conflict.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, and any simple modification, equivalent change and modification made to the above embodiment according to the technical spirit of the present invention are still within the scope of the technical solution of the present invention.
Claims (10)
1. The utility model provides a anchor clamps for air vane which characterized in that for the axle core of fixed air vane, the shaft hole has been seted up to the both sides of axle core, anchor clamps include: the connecting rod unit (100), the fixing units (200) and the sleeve (300), wherein a first hole and a second hole corresponding to the shaft holes are formed in two sides of the sleeve (300), at least two fixing units (200) are arranged, one ends of the at least two fixing units (200) are connected with the connecting rod unit (100), and the other ends of the at least two fixing units (200) are respectively inserted into the first hole and the second hole;
the shaft core of the air rudder to be processed is arranged in the sleeve (300), and the connecting rod unit (100) drives the fixing unit (200) to move towards the direction close to the shaft core in the first hole and the second hole, so that the shaft core is clamped.
2. The clamp for the air rudder according to claim 1, wherein the link unit (100) includes a guide rod (101), a slider (102), a first link (103), and a second link (104), the slider (102) is located on the guide rod (101), the guide rod (101) drives the slider (102) to move up and down, one end of each of the first link (103) and the second link (104) is connected to the slider (102), and the other end is connected to the corresponding fixing unit (200).
3. The clamp for the air rudder according to claim 2, wherein the fixing unit (200) includes a first fixing rod (201) and a second fixing rod (202), one end of the first fixing rod (201) is connected to the first link (103), the other end of the first fixing rod (201) is inserted into the first hole, one end of the second fixing rod (202) is connected to the second link (104), and the other end of the second fixing rod (202) is inserted into the second hole.
4. The clamp for the air rudder according to claim 3, wherein the first fixing rod (201) and/or the second fixing rod (202) is a pin connected with the corresponding first link (103) or the second link (104) by a pin; and one end of the bolt inserted into the first hole and the second hole is provided with a guide part.
5. A clamp for an air rudder according to any one of claims 2-4, characterised in that the linkage unit (100) further includes a shielding structure (105) enclosed by a baffle (1051), the guide rod (101) being located inside the shielding structure (105) and its end remote from the sleeve (300) protruding out of the shielding structure (105).
6. A clamp for an air rudder according to claim 5, wherein the link unit (100) further includes a limit structure (106), the limit structure (106) being located on the guard structure (105), the guide rod (101) passing through the limit structure (106), the limit structure (106) being for limiting an extreme position when the guide rod (101) moves downward.
7. Clamp for an air rudder according to claim 5, characterised in that the link unit (100) further comprises a positioning structure (107), the positioning structure (107) connecting the guide rod (101) with a guard structure (105) for avoiding the guide rod (101) from sliding down.
8. The clamp for the air rudder according to any one of claims 1 to 4, wherein the sleeve (300) includes a body (301), a thickening layer (302) is sleeved on a circumferential surface where the first hole and the second hole are located on the body (301), holes corresponding to the first hole and the second hole are formed in the thickening layer (302), and the thickening layer (302) is used for preventing the fixing unit (200) from shaking when moving towards the axial core direction.
9. A clamp for an air rudder according to claim 8, wherein the inner wall of the body (301), the surface of the fixing unit (200) are provided with a plastic or rubber layer.
10. A clamp for an air rudder according to any one of claims 1 to 4, wherein the clamp further includes a driving unit connected with the link unit (100) for powering the same.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111322009.0A CN114011665B (en) | 2021-11-09 | 2021-11-09 | Clamp for air rudder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111322009.0A CN114011665B (en) | 2021-11-09 | 2021-11-09 | Clamp for air rudder |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114011665A true CN114011665A (en) | 2022-02-08 |
| CN114011665B CN114011665B (en) | 2022-10-21 |
Family
ID=80062735
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111322009.0A Active CN114011665B (en) | 2021-11-09 | 2021-11-09 | Clamp for air rudder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114011665B (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2907585A1 (en) * | 2014-02-17 | 2015-08-19 | Drei Bond GmbH | Method and device for applying a fluid to a surface of a component |
| CN206142657U (en) * | 2016-10-31 | 2017-05-03 | 江西腾勒动力有限公司 | Connecting rod fixture |
| CN107186623A (en) * | 2017-07-06 | 2017-09-22 | 南华大学 | Airvane grinding hand-operated clamping fixture |
| CN207326725U (en) * | 2017-07-06 | 2018-05-08 | 南华大学 | Airvane grinding automatic clamping fixture |
| CN108982041A (en) * | 2018-09-20 | 2018-12-11 | 王瑞芳 | A kind of airvane rudder core exciting test device |
| CN209665155U (en) * | 2019-04-10 | 2019-11-22 | 河南中烟工业有限责任公司 | A kind of new-type reversed Tube vice |
| CN213004052U (en) * | 2020-06-01 | 2021-04-20 | 大连职业技术学院 | Automatic feeding and discharging clamping device of numerical control machine tool |
| CN214066480U (en) * | 2020-12-18 | 2021-08-27 | 昆山建蜀精密电子有限公司 | Automobile connecting rod fatigue test fixture |
-
2021
- 2021-11-09 CN CN202111322009.0A patent/CN114011665B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2907585A1 (en) * | 2014-02-17 | 2015-08-19 | Drei Bond GmbH | Method and device for applying a fluid to a surface of a component |
| CN206142657U (en) * | 2016-10-31 | 2017-05-03 | 江西腾勒动力有限公司 | Connecting rod fixture |
| CN107186623A (en) * | 2017-07-06 | 2017-09-22 | 南华大学 | Airvane grinding hand-operated clamping fixture |
| CN207326725U (en) * | 2017-07-06 | 2018-05-08 | 南华大学 | Airvane grinding automatic clamping fixture |
| CN108982041A (en) * | 2018-09-20 | 2018-12-11 | 王瑞芳 | A kind of airvane rudder core exciting test device |
| CN209665155U (en) * | 2019-04-10 | 2019-11-22 | 河南中烟工业有限责任公司 | A kind of new-type reversed Tube vice |
| CN213004052U (en) * | 2020-06-01 | 2021-04-20 | 大连职业技术学院 | Automatic feeding and discharging clamping device of numerical control machine tool |
| CN214066480U (en) * | 2020-12-18 | 2021-08-27 | 昆山建蜀精密电子有限公司 | Automobile connecting rod fatigue test fixture |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114011665B (en) | 2022-10-21 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208962008U (en) | A kind of Sidle manipulator | |
| CN112475390A (en) | Machining drilling machine equipment that stability is high | |
| CN114011665B (en) | Clamp for air rudder | |
| KR200317671Y1 (en) | Lug cutting machine | |
| CN210781557U (en) | Automatic pin mechanism of beating of PCB digit control machine tool | |
| WO2023216570A1 (en) | Tool changing device for machine tool, machine tool, and tool changing method for machine tool | |
| CN210306728U (en) | Multi-degree-of-freedom parallel drilling and riveting mechanism and integral movable machining equipment with same | |
| CN214769876U (en) | Welding device for machining | |
| CN213894228U (en) | Workpiece clamping and overturning mechanism | |
| CN214488947U (en) | Machining drilling machine equipment that stability is high | |
| CN110002171B (en) | Wire harness production line | |
| CN217750290U (en) | Sanitation car processing is with equipment of going up and down of being convenient for | |
| CN215547991U (en) | Automobile opening and closing part grabbing and lifting device | |
| CN210677902U (en) | Special fixture for milling groove machining | |
| CN216462921U (en) | Automatic screw locking mechanism | |
| CN213618405U (en) | Equipment for sewing cloth by ultrasonic wave | |
| CN114227234B (en) | Automatic interchangeable electricity is criticized first locking and is attached machine | |
| CN217830467U (en) | Reciprocating spraying machine | |
| CN217727619U (en) | Novel PCB board welding machine angle adjustment mechanism | |
| CN210587806U (en) | Frock clamp is used in metalwork welding | |
| CN113388975B (en) | Automatic wire wheel replacing device and embroidery machine thereof | |
| CN215317239U (en) | Machining center positioning device | |
| CN217224536U (en) | Cambered surface holder for numerical control machine tool | |
| CN210413333U (en) | Servo multi-torque control lock screw machine | |
| CN217660288U (en) | Movable rack and automatic poultry injection system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |