CN216432899U

CN216432899U - A three-dimensional detects and presss from both sides apparatus for unmanned aerial vehicle crankcase

Info

Publication number: CN216432899U
Application number: CN202123063950.3U
Authority: CN
Inventors: 杨承章; 王力; 徐智方
Original assignee: Xiangyang Lianhang Power Technology Co ltd
Current assignee: Xiangyang Lianhang Power Technology Co ltd
Priority date: 2021-12-08
Filing date: 2021-12-08
Publication date: 2022-05-03
Anticipated expiration: 2031-12-08

Abstract

The utility model discloses a three-dimensional detects and presss from both sides apparatus for unmanned aerial vehicle crankcase, including examining test table, examine the both sides at anterior and rear portion in test table top and all be provided with the support column, four common fixedly connected with fixed plate between the support column, the anterior and the equal fixedly connected with diaphragm in rear portion at fixed plate top, the utility model relates to an unmanned air vehicle technique field. This a three-dimensional detects double-layered apparatus for unmanned aerial vehicle crankcase, surface through at the dwang sets up two second belt pulleys, make fixing device when fixing the unmanned aerial vehicle crankcase, can make two sets of threaded rods impel forward simultaneously through the rotation of dwang, and then reach the effect to the unmanned aerial vehicle crankcase quick fixation, arc wall and rectangle recess are seted up through the top at the bearing platform simultaneously, make the crankcase bottom can be rather than the looks adaptation completely, avoid when fixing the crankcase, need the people to hand to hold the crankcase in order to guarantee that it can not empty.

Description

A three-dimensional detects and presss from both sides apparatus for unmanned aerial vehicle crankcase

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a three-dimensional detects and presss from both sides apparatus for unmanned aerial vehicle crankcase.

Background

In-process at production unmanned aerial vehicle crankcase, often can carry out the three-coordinate detection of sampling to the unmanned aerial vehicle crankcase, in order to ensure the outward appearance of unmanned aerial vehicle crankcase, profile and size precision are up to standard, because unmanned aerial vehicle's outward appearance is irregular and in addition there is not the fixing device rather than the looks adaptation in the market, cause the unmanned aerial vehicle crankcase to need use support articles such as cushion to place the unmanned aerial vehicle crankcase steady before detecting on examining the test table, it is comparatively troublesome for the unmanned aerial vehicle crankcase interpolation support to use cushion etc., and the cushion does not possess the fixed ability, thereby cause the crankcase product to lead to detecting the inaccurate problem of data at the in-process of detecting easily squint.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art, the utility model provides a three-dimensional detects and presss from both sides apparatus for unmanned aerial vehicle crankcase has solved and has lacked fixing device and cause the not accurate problem of unmanned aerial vehicle crankcase detection data.

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a three-dimensional detects clamp apparatus for unmanned aerial vehicle crankcase, is including examining test table, it all is provided with the support column, four to examine the both sides at anterior and rear portion of test table top common fixedly connected with fixed plate between the support column, the anterior and the equal fixedly connected with diaphragm in rear portion at fixed plate top are located anteriorly opening fixedly connected with bearing is passed through to the anterior both sides of diaphragm, the inner ring fixedly connected with thread bush of bearing, the inside threaded connection of thread bush has the threaded rod, the one end of threaded rod runs through anterior diaphragm and extends to the rear portion of anterior diaphragm, the equal fixedly connected with spout plate in both sides of the front portion of fixed plate, the inside sliding connection of spout plate has the slider, the homonymy the bottom fixed connection of mounting and threaded rod is passed through at the top of slider, the first belt pulley of fixed surface connection of thread bush is located anteriorly the diaphragm just is located to rotate through rotating between two thread bushes and is connected with the rotation and rotates and rotate the rotation and to be connected with the clamp apparatus The pole, the equal fixedly connected with second belt pulley in the front portion and the rear portion on rotor lever surface is located the rear portion the transmission is connected with first belt between second belt pulley and the first belt pulley in left side, is located the front portion the transmission is connected with the second belt between second belt pulley and the first belt pulley in right side.

Preferably, the top of the fixing plate is fixedly connected with a bearing platform, the top of the bearing platform is provided with an arc-shaped groove, and the top of the bearing platform is provided with a rectangular groove.

Preferably, one end of the threaded rod is fixedly connected with a rubber pad.

Preferably, one end of the rotating rod is fixedly connected with a handle through a fixing part.

Preferably, the inside of the supporting column is in threaded connection with a fixing bolt through a threaded hole.

Preferably, the top of the detection table is provided with a plurality of thread fixing grooves matched with the fixing bolts.

Advantageous effects

The utility model provides a three-dimensional detects and presss from both sides apparatus for unmanned aerial vehicle crankcase. Compared with the prior art, the method has the following beneficial effects:

(1) this a three-dimensional detects double-layered apparatus for unmanned aerial vehicle crankcase, surface through at the dwang sets up two second belt pulleys, make fixing device when fixing the unmanned aerial vehicle crankcase, can make two sets of threaded rods impel forward simultaneously through the rotation of dwang, and then reach the effect to the unmanned aerial vehicle crankcase quick fixation, arc wall and rectangle recess are seted up through the top at the bearing platform simultaneously, make the crankcase bottom can be rather than the looks adaptation completely, avoid when fixing the crankcase, need the people to hand to hold the crankcase in order to guarantee that it can not empty.

(2) This a three-coordinate detects and presss from both sides apparatus for unmanned aerial vehicle crankcase sets up fixing bolt and offers the screw thread fixed slot at the top of examining test table through the inside at the support column for fixing device can fasten on examining test table through the cooperation of fixing bolt, support column and screw thread fixed slot, thereby avoids personnel's maloperation and leads to the whole unexpected hidden danger that shifts and empty of device.

Drawings

Fig. 1 is a schematic external structural view of the present invention;

FIG. 2 is an enlarged view of a portion A of FIG. 1;

fig. 3 is a top view of the fixing plate structure of the present invention;

fig. 4 is a side view of the structure of the supporting platform of the present invention.

In the figure: 1. a detection table; 2. a support pillar; 3. a fixing plate; 4. a transverse plate; 5. a bearing; 6. a threaded sleeve; 7. a threaded rod; 8. a chute plate; 9. a slider; 10. a first pulley; 11. rotating the rod; 12. a second pulley; 13. a first belt; 14. a second belt; 15. a support platform; 16. an arc-shaped slot; 17. a rectangular groove; 18. a rubber pad; 19. a handle; 20. fixing the bolt; 21. and (4) a thread fixing groove.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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. 1-4, the present invention provides a technical solution: a three-coordinate detection clamp tool for an unmanned aerial vehicle crankcase comprises a detection table 1, wherein support columns 2 are arranged on two sides of the front portion and the rear portion of the top of the detection table 1, a fixed plate 3 is fixedly connected among the four support columns 2 together, transverse plates 4 are fixedly connected on the front portion and the rear portion of the top of the fixed plate 3, bearings 5 are fixedly connected on two sides of the front portion of the transverse plate 4 through openings, a threaded sleeve 6 is fixedly connected to an inner ring of each bearing 5, a threaded rod 7 is connected to an inner thread of each threaded sleeve 6, one end of each threaded rod 7 penetrates through the front transverse plate 4 and extends to the rear portion of the corresponding front transverse plate 4, sliding groove plates 8 are fixedly connected on two sides of the front portion of the fixed plate 3, sliding blocks 9 are slidably connected to the inner portions of the sliding groove plates 8, the tops of the sliding blocks 9 on the same side are fixedly connected with the bottoms of the threaded rods 7 through fixing pieces, and first belt pulleys 10 are fixedly connected to the surfaces of the threaded sleeves 6, the front portion of being located anterior diaphragm 4 just is located and rotates through rotating between two thread bush 6 and is connected with dwang 11, and the equal fixedly connected with second belt pulley 12 in anterior and the rear portion on dwang 11 surface is located the transmission between second belt pulley 12 in rear portion and the first belt pulley 10 in left side and is connected with first belt 13, is located the transmission between anterior second belt pulley 12 and the first belt pulley 10 in right side and is connected with second belt 14.

Further, in order to stably place the bottom of the crankcase on the fixing plate 3, the top of the fixing plate 3 is fixedly connected with a supporting platform 15, the top of the supporting platform 15 is provided with an arc-shaped groove 16, and the top of the supporting platform 15 is provided with a rectangular groove 17.

Further, in order to increase the friction between the threaded rod 7 and the crankcase, a rubber pad 18 is fixedly connected to one end of the threaded rod 7.

Further, in order to rotate the rotating lever 11, a handle 19 is fixedly connected to one end of the rotating lever 11 through a fixing member.

Further, in order to avoid the fixing device from displacing on the detection table 1, the inside of the supporting column 2 is connected with a fixing bolt 20 through a threaded hole, and the top of the detection table 1 is provided with a plurality of thread fixing grooves 21 matched with the fixing bolt 20.

And those not described in detail in this specification are well within the skill of those in the art.

When the device is used, firstly, the fixing device is fastened at the top of the detection table 1 by utilizing the matching of the fixing bolt 20, the support column 2 and the thread fixing groove 21, then the crankcase of the unmanned aerial vehicle is taken and placed at the top of the fixing plate 3, the bottom of the crankcase is attached to the arc-shaped groove 16 and the rectangular groove 17, the crankcase can be stably placed on the fixing plate 3 by attaching the arc-shaped groove 16 and the rectangular groove 17 to the bottom of the crankcase, so that the problem that the crankcase needs to be manually supported to avoid toppling when being fixed is avoided, then the handle 19 is utilized to rotate the rotating rod 11, the two second belt wheels 12 on the surface of the rotating rod 11 can rotate after the rotating rod 11 rotates, the two second belt wheels 12 can link the two first belt wheels 10 to rotate, the first belt wheel 10 drives the thread sleeve 6 to rotate, the threaded rod 7 in the thread sleeve 6 can move backwards after the thread sleeve rotates, the crankcase can be held stationary by the movement of the threaded rod 7.

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

1. The utility model provides a three-coordinate detects and presss from both sides apparatus for unmanned aerial vehicle crankcase, is including detecting platform (1), its characterized in that: the detection table is characterized in that supporting columns (2) are arranged on the two sides of the front portion and the rear portion of the top of the detection table (1), four fixing plates (3) are fixedly connected among the supporting columns (2) together, transverse plates (4) are fixedly connected to the front portion and the rear portion of the top of the fixing plates (3), bearings (5) are fixedly connected to the two sides of the front portion of the transverse plates (4) through openings, inner rings of the bearings (5) are fixedly connected with threaded sleeves (6), threaded rods (7) are connected to the inner threads of the threaded sleeves (6), one ends of the threaded rods (7) penetrate through the front transverse plates (4) and extend to the rear portions of the front transverse plates (4), sliding groove plates (8) are fixedly connected to the two sides of the front portion of the fixing plates (3), sliding blocks (9) are connected to the inner sliding grooves (8) in a sliding mode, the tops of the sliding blocks (9) on the same side are fixedly connected with the bottoms of the threaded rods (7) through fixing pieces, the surperficial fixedly connected with first belt pulley (10) of thread bush (6) is located the front portion of diaphragm (4) just is located and rotates through rotating between two thread bushes (6) and is connected with dwang (11), the anterior and the equal fixedly connected with second belt pulley (12) in rear portion on dwang (11) surface are located the rear portion the transmission is connected with first belt (13) between second belt pulley (12) and left side first belt pulley (10), are located the front portion the transmission is connected with second belt (14) between second belt pulley (12) and right side first belt pulley (10).

2. The three-coordinate detection clamp for the crankcase of the unmanned aerial vehicle as claimed in claim 1, wherein: the top of the fixed plate (3) is fixedly connected with a bearing platform (15), the top of the bearing platform (15) is provided with an arc-shaped groove (16), and the top of the bearing platform (15) is provided with a rectangular groove (17).

3. The three-coordinate detection clamp for the crankcase of the unmanned aerial vehicle as claimed in claim 1, wherein: one end of the threaded rod (7) is fixedly connected with a rubber pad (18).

4. The three-coordinate detection clamp for the crankcase of the unmanned aerial vehicle as claimed in claim 1, wherein: one end of the rotating rod (11) is fixedly connected with a handle (19) through a fixing part.

5. The three-coordinate detection clamp for the crankcase of the unmanned aerial vehicle as claimed in claim 1, wherein: the inside of the support column (2) is connected with a fixing bolt (20) through a threaded hole in a threaded manner.

6. The three-coordinate detection clamp for the crankcase of the unmanned aerial vehicle as claimed in claim 5, wherein: the top of the detection table (1) is provided with a plurality of thread fixing grooves (21) matched with the fixing bolts (20).