CN206953028U

CN206953028U - Fixture

Info

Publication number: CN206953028U
Application number: CN201720772448.4U
Authority: CN
Inventors: 张旭
Original assignee: Guangdong Midea Refrigeration Equipment Co Ltd
Current assignee: GD Midea Air Conditioning Equipment Co Ltd
Priority date: 2017-06-29
Filing date: 2017-06-29
Publication date: 2018-02-02
Anticipated expiration: 2027-06-29

Abstract

The utility model proposes a kind of fixture, for clamping the fuselage of air conditioner, including：Support frame, two slide rails being parallel to each other are arranged at intervals on support frame；Two groups of clamp assemblies, it is connected and perpendicular to slide rail with two slide rails；Drive component, it is connected with two groups of clamp assemblies, drive component drives two groups of clamp assemblies to be moved along slide rail, to clamp the fuselage with plane between two groups of clamp assemblies；With two groups of clip claw assemblies, the bottom of two groups of clamp assemblies is separately positioned on, two groups of clip claw assemblies are oppositely arranged, and the opposite face for two clamping jaws being oppositely arranged in two groups of clip claw assemblies has cambered surface, to clamp the fuselage with cambered surface between two groups of clip claw assemblies.Fixture in the utility model can not only clamp the fuselage of conventional cuboid formula, can also clamp the fuselage of the column type of single through-flow, improve the versatility of fixture, the equipment for being easy to production line to produce various types, improve the production capacity of production line.

Description

Fixture

Technical field

The utility model belongs to technical field of processing equipment, in particular to a kind of fixture.

Background technology

Floor standing air-conditioner device is to improve human lives' comfortableness, maintains the one kind of indoor air temperature within the specified range Electrical equipment.Family expenses floor standing air-conditioner device is generally positioned at parlor corner than more prominent place, the appearance design of high-grade air conditioner and outer Go sightseeing to spend and highly pursued by customer, exquisite air-conditioning outward appearance is also made something perfect even more perfect to whole family's interior decoration, therefore air-conditioning The fuselage appearance structure pattern of device is various, corresponding production frock technological requirement more and more higher.

The fuselage of conventional air conditioner installed inside cabinet is divided into according to structure：Conventional machine (profile shows as cuboid) and single through-flow Machine (profile shows as cylinder)；Machine general assembly line assembly technology, which is taken, in cabinet first carries out lying down formula assembled part parts, laggard Row, which is stood, to be assembled remaining parts and is simultaneously tested, and finally carries out lying down formula packaging offline；In posture conversion process is assembled, profit Carrying upset is carried out with robot control fixture, because every production line will possess the production capacity of various types, therefore, is needed badly A kind of general fixture for carrying upset air conditioner fuselage.

Utility model content

The utility model aims to solve the problem that one of technical problem present in prior art.

Therefore, a purpose of the present utility model is to propose a kind of fixture.

In view of this, a kind of fixture is proposed according to a purpose of the present utility model, for clamping the fuselage of air conditioner, Including：Support frame, two slide rails being parallel to each other are arranged at intervals on support frame；Two groups of clamp assemblies, it is connected with two slide rails Connect and perpendicular to slide rail；Drive component, it is connected with two groups of clamp assemblies, drive component drives two groups of clamp assemblies to be moved along slide rail It is dynamic, to clamp the fuselage with plane between two groups of clamp assemblies；With two groups of clip claw assemblies, two groups of clamping groups are separately positioned on The bottom of part, two groups of clip claw assemblies are oppositely arranged, and the relative mask for two clamping jaws being oppositely arranged in two groups of clip claw assemblies There is cambered surface, to clamp the fuselage with cambered surface between two groups of clip claw assemblies.

The utility model clamps the fuselage with plane, such as rectangular fuselage by two groups of clamp assemblies, passes through two Group clip claw assembly clamps the fuselage with radian, such as cylindrical body, section are fuselage of ellipse etc. so that the fixture energy The fuselage of various structures is enough clamped, improves the versatility of fixture, is advantageous to carry out a variety of fuselages with robot control fixture Upset is carried, improves the production capacity that the air conditioner of various types is assembled in production line production, it is cost-effective, improve job shop Space availability ratio.In utility model, during the fuselage with plane is gripped, drive component drives two groups of clamp assemblies Demand position (can carry out adjusting the driving duration for setting drive component or driving distance according to the width of the fuselage of air conditioner) is moved to, To clamp fuselage, it is easy to carry upset；During the fuselage with radian is gripped, drive component drives two groups of clamp assemblies Motion, and then two groups of clip claw assemblies of drive move to demand position and (can carry out tune according to the width of the fuselage of air conditioner and set driving The driving duration or driving distance of component), fitted by the cambered surface of the clamping jaw of two groups of clip claw assemblies and the cambered surface of fuselage, to embrace Firmly fuselage and clamp fuselage.Preferably, drive component has mnemonic, and adjustable adapts to different product, and servo provides surely Fixed demand dynamics, it is preferable that drive component includes stepper motor and leading screw, and leading screw one end is disposed therein one group of clamp assembly Mounting bracket on, the other end of leading screw is arranged on another group of clamp assembly and is connected with stepper motor, driving stepper motor Leading screw is rotated to further or separate two groups of clamp assemblies.

In addition, the fixture in above-mentioned technical proposal provided by the utility model, can also have following additional technical feature：

In the above-mentioned technical solutions, it is preferable that the distance between two groups of clamp assemblies be less than or equal to two groups of clip claw assemblies it Between distance.

In the technical scheme, when the distance between two groups of clamp assemblies are less than the distance between two groups of clip claw assemblies, When clamping the fuselage with plane, two groups of clamp assemblies are clamped to the both sides of fuselage.When between two groups of clamp assemblies When distance is equal to the distance between two groups of clip claw assemblies, when clamping the fuselage with plane, two groups of clamp assemblies and two groups of folders Claw assembly simultaneously clamps on the both sides of fuselage, further increases the stability for clamping the fuselage with plane.And when clamping has During the fuselage of radian, two groups of clip claw assemblies are embraced fuselage and are clamped, furthermore it is preferred that when between two groups of clamp assemblies When distance is equal to the distance between two groups of clip claw assemblies, and when a part for fuselage be U-shape structure, pass through two groups of clamp assemblies folders At the plane of the upper end of tight U-shaped fuselage, at the radian for the lower end that U-shaped fuselage is clamped by two groups of clip claw assemblies.

In any of the above-described technical scheme, it is preferable that the cambered surface of clamping jaw is from top to bottom to the clamping position place of fuselage The cambered surface that gradually extends of direction, the vertical plane extended downwardly is provided with the lower end of cambered surface.

In the technical scheme, the cambered surface of clamping jaw is gradually to the cambered surface of fuselage clamping position direction extension, and then relatively Fuselage can sufficiently be embraced and clamp fuselage by two clamping jaws set, it is preferable that the radian of the cambered surface of clamping jaw and fuselage The radian of cambered surface matches, in addition, the vertical plane of the lower end connection of the cambered surface of clamping jaw vertically downward, not only increases cambered surface and bear machine The ability of body gravity, the structural strength of clamping jaw is improved, also caused when the distance between two groups of clamp assemblies are equal to two groups of clamping jaws During the distance between component, the vertical plane of clip claw assembly can clamp the both sides of the fuselage with plane together with clamp assembly, carry High clip stability, it is easy to carry upset.

In any of the above-described technical scheme, it is preferable that the number of clamping jaw is at least one in every group of clip claw assembly, each folder Pawl is anchored on clamp assembly by the first fastener, wherein, each clamping jaw moves up and down and tight by first along clamp assembly Firmware is fixed.

In the technical scheme, when the number of clamping jaw is multiple in every group of clip claw assembly, multipair clamping jaw embraces fuselage simultaneously And fuselage is clamped, the steadiness for clamping fuselage is improved, is easy to upset to carry, each clamping jaw can move up and down again along clamp assembly Clamping jaw is anchored on clamp assembly by the first fastener, clamping jaw can be needed to adjust to suitable according to the size of fuselage Position, it is easy to clamp fuselage, also allows for changing the clamping jaw with different cambered surfaces, further matches a variety of fuselages and more firm Clamp fuselage.Preferably, the first fastener is bolt, and two sides and the clamp assembly of the opposing clamping surfaces of each clamping jaw fit And there is screwed hole, clamp assembly is provided with the first slideway, and bolt stretches into the first chute through screwed hole, clamping jaw is fastened On clamp assembly.

In any of the above-described technical scheme, it is preferable that every group of clamp assembly include mounting bracket, at least one connecting bracket and At least one clamping section, mounting bracket are slidably connected with two slide rails, and at least one connecting bracket is arranged on the lower surface of mounting bracket And perpendicular to mounting bracket, at least one clamping section is arranged at least one connecting bracket close to the side of fuselage clamping position, uses In fuselage of the clamping with plane.

In the technical scheme, every group of clamp assembly has the mounting bracket being slidably connected with two slide rails, in mounting bracket Lower surface sets at least one connecting bracket, and at least one clamping is set close to the side of fuselage clamping position in connecting bracket Portion, the fuselage of air conditioner is clamped by clamping section.The utility model is moved by drive component drive installation frame, and then drives two The connecting bracket of group clamp assembly is mutually drawn close so that two groups of clamping sections for stepping up component are mutually drawn close to clamp fuselage, or band Move two groups of clip claw assemblies and mutually draw close the clamping effect for clamp fuselage, improving fuselage, especially when the number of connecting bracket is When multiple, when the number of clamping section is multiple, the clamping dynamics of fuselage is further increased, is easy to carry upset fuselage.It is preferred that There are at least two sliding blocks ground, the upper surface of mounting bracket, and at least two sliding blocks are slidably connected with two slide rails respectively, so that every group of folder Tight component is moved by sliding block along slide rail.

In any of the above-described technical scheme, it is preferable that when the number of connecting bracket is multiple, multiple connecting bracket intervals It is arranged on mounting bracket；When the number of clamping section is one, a clamping section is arranged in multiple connecting brackets simultaneously, or is worked as When the number of clamping section is multiple, multiple clamping sections are corresponding at the same time or separately to be arranged in multiple connecting brackets.

In the technical scheme, multiple connecting bracket intervals are arranged on mounting bracket, enable to two groups of clamp assemblies Connecting bracket be more evenly distributed, and then facilitate gripping by the fuselage with certain length, improve the stability for clamping fuselage.One Individual clamping section is arranged in multiple connecting brackets simultaneously, is capable of the pressure of balanced each fuselage that connecting bracket is subject to, Jin Erti Height clamps the stability of fuselage, by setting multiple clamping sections, it is possible to increase the contact area of clamp assembly and fuselage, further Improve the stability for clamping fuselage.

In any of the above-described technical scheme, it is preferable that the number of clamping jaw and every group of clamp assembly in every group of clip claw assembly The number of connecting bracket is identical, and at least one clamping jaw is corresponding is arranged at least one connecting bracket, and positioned at clamping The lower section in portion.

In the technical scheme, the number of clamping jaw matches with clamping the number of support, and clamping jaw is located under clamping section Side so that when clamping the fuselage with plane, fuselage, now, the folder positioned at clamping section bottom can be clamped by clamping section Pawl can be bonded with fuselage sections, can be also bonded completely, i.e. the clamping without interference with clamping section；And clamping the machine with cambered surface During body, the upper edge of fuselage is clamped by clamping jaw, now clamping section can't typically fit with fuselage, not affect clamping jaw Clamping to fuselage, improve the versatility of fixture.

In any of the above-described technical scheme, it is preferable that each connecting bracket is set provided with least one along its short transverse The first slideway put, each clamping jaw are anchored at least one first slideway by the first fastener, wherein, each clamping jaw is along extremely Few first slideway is shifted and fixed by the first fastener up and down.

In the technical scheme, connecting bracket is provided with least one first slideway, and clamping jaw can pass through the first fastener It is fastened on the first slideway, and can be moved up and down along the first slideway, and then can suitably adjust the position of clamping jaw as needed, also just In changing the clamping jaw with different cambered surfaces, further to match a variety of fuselages and more firm clamping fuselage.Preferably, first is tight Firmware is bolt, and two sides and the clamp assembly of the opposing clamping surfaces of each clamping jaw fit and have screwed hole, and bolt passes through Screwed hole is stretched into the first chute, and clamping jaw is fastened on clamp assembly.

In any of the above-described technical scheme, it is preferable that the side of the close fuselage clamping position of clamp assembly and clamping jaw Clamping face is provided with flexure strip.

In the technical scheme, the face of stepping up of clamp assembly and clamping jaw is provided with elastic component, effectively fixture can be avoided to exist Clamp fuselage during to fuselage cause abrasion etc. destroy, effectively prevent fuselage from scratching, in addition, also improve step up component, Frictional force between clamping jaw and fuselage, and then improve the stability for clamping fuselage.Preferably, flexure strip is silica gel piece.

In any of the above-described technical scheme, it is preferable that fixture also includes：Two groups of Suction cup assemblies, it is separately positioned on two groups of folders The bottom of tight component, two groups of Suction cup assemblies are oppositely arranged, for adsorbing the both sides of fuselage.

In the technical scheme, fixture also has Suction cup assembly, and the both sides of fuselage are adsorbed by Suction cup assembly, can enter one Step improves the fastness of fixture clamping fuselage.In the utility model, during the fuselage with plane is gripped, driving group Part drives two groups of clamp assemblies to move to demand position, and behind, sucker module adsorbs in the both sides of fuselage clamping machine, further true Protect the fastness of fixture clamping air-conditioning；During the fuselage with radian is gripped, drive component drives two groups of clamp assemblies Motion, and then drive two groups of clip claw assemblies to move to demand position, embracing fuselage, simultaneously behind, sucker module adsorbs fuselage to clamping machine Both sides, further ensure that fixture clamping air-conditioning fastness.

In any of the above-described technical scheme, it is preferable that every group of Suction cup assembly includes at least one sucker, at least one pole And connecting rod, the corresponding back for being arranged at least one sucker of at least one pole, at least one pole are arranged on connection On bar, connecting rod is arranged on clamp assembly.

In the technical scheme, when Suction cup assembly has multiple suckers, it is possible to increase the dynamics of sucker suction fuselage, and then The firmness of fixture clamping fuselage is improved, at least one sucker is arranged in connecting rod by pole, and connecting rod is arranged on clamping On component, enable in every group of Suction cup assembly, the high unity of each sucker, the convenient sustained height to fuselage is inhaled It is attached, the clip stability of fuselage is improved, in addition, being installed by the way that connecting rod is unified at least one sucker so that fixture knot Structure is simple, improves the assembling speed of fixture.

In any of the above-described technical scheme, it is preferable that fixture also includes：Getter device, it is connected with least one pole, Pole is hollow stem, and pole is connected with sucker, and getter device is used to draw the gas in sucker.

In the technical scheme, getter device can draw the gas in sucker, after sucker fully contacts with fuselage, lead to The gas crossed in getter device absorption sucker, can make suction cup interior be in vacuum state or near vacuum state, and then can The side plate of fuselage is preferably adsorbed, effectively ensures that fuselage is not fallen out in handling process is overturn.Preferably, getter device is true Empty generator.

In any of the above-described technical scheme, it is preferable that fixture also includes：At least one magnetic valve, magnetic valve and at least one Individual pole is connected, for discharging the gas in pole.

In the technical scheme, fixture also includes magnetic valve, when getter device draws the gas in sucker, opens electromagnetism Valve, to exclude gas, and when exhaust finishes, magnetic valve is closed, to be in vacuum negative pressure condition all the time in sucker, it is ensured that Fuselage is not fallen out in handling process is overturn.Preferably, magnetic valve is four-way valve, while controls four poles to lead to extraneous It is disconnected.

In any of the above-described technical scheme, it is preferable that every group of clamp assembly is set provided with least one along its short transverse The second slideway put, connecting rod move up and down along at least one second slideway.

In the technical scheme, connecting rod can move up and down along the second slideway on clamp assembly, and then adjustable setting The height of sucker in connecting rod, be advantageous to capture fuselage of different shapes, it is ensured that clamp fuselage it is firm Property, it is easy to carry upset.

In any of the above-described technical scheme, it is preferable that the second fastener is set on pole, and pole is arranged on the limit of connecting rod In the hole of position, centerline direction of the pole along spacing hole moves through the second fastener and fixed.

In the technical scheme, pole is arranged in the spacing hole of connecting rod, and the second fastener is set on pole, when When two fasteners do not fasten pole, pole can move back and forth along spacing hole, can be moved to the installation site direction of fuselage, also can be to Moved away from the installation site direction of fuselage so that Suction cup assembly can preferably adsorb the appearance in fuselage of different shapes Face, especially cylindrical body, improve the adsorption effect of Suction cup assembly, it is preferable that spacing hole is screwed hole, and pole is provided with Relative external screw thread, the second fastener are nut.

In any of the above-described technical scheme, it is preferable that the top of support frame sets mounting plate, mounting plate and machine Tool arm is connected, and sensor is positioned proximate on mounting plate, to prevent fuselage from being collided with support frame.

In the technical scheme, the top of support frame sets mounting plate, and mounting plate is connected with mechanical arm, is made Obtaining robot etc. can control fixture carry out carrying upset to the fuselage of air conditioner by mechanical arm, be advantageous to air conditioner group Dress, improves the throughput rate of air conditioner, in addition, being positioned proximate to sensor on mounting plate, fixture can be avoided to press from both sides During taking fuselage, support frame collides with fuselage and damages fuselage, improves the security of air conditioner assembling.

Additional aspect and advantage of the present utility model will become obvious in following description section, or new by this practicality The practice of type is recognized.

Brief description of the drawings

Of the present utility model above-mentioned and/or additional aspect and advantage will in the description from combination accompanying drawings below to embodiment Become obvious and be readily appreciated that, wherein：

Fig. 1 shows the clamp structure schematic diagram of one embodiment of the present utility model；

Fig. 2 shows the clamp structure schematic diagram of second embodiment of the present utility model；

Fig. 3 shows the clamp structure schematic diagram of the 3rd embodiment of the present utility model；

Fig. 4 shows the clamp structure schematic diagram of the 4th embodiment of the present utility model；

Fig. 5 shows the structural representation of the fixture gripping rectangle fuselage of one embodiment of the present utility model；

Fig. 6 shows the structural representation of the fixture gripping cylindrical body of one embodiment of the present utility model.

Wherein, corresponding relations of the Fig. 1 into Fig. 6 between reference and component names is：

10 support frames, 102 mounting plates, 104 slide rails, 12 clamp assemblies, 122 mounting brackets, 124 connecting brackets, 1242 First slideway, 1,244 second slideways, 126 clamping sections, 14 drive components, 16 clip claw assemblies, 162 clamping jaws, 1622 cambered surfaces, 1624 hang down Face, 18 Suction cup assemblies, 182 suckers, 184 poles, 186 connecting rods, 20 fuselages, 22 flexure strips.

Embodiment

In order to be more clearly understood that above-mentioned purpose of the present utility model, feature and advantage, below in conjunction with the accompanying drawings and tool The utility model is further described in detail body embodiment.It should be noted that in the case where not conflicting, this Shen The feature in embodiment and embodiment please can be mutually combined.

Many details are elaborated in the following description in order to fully understand the utility model, still, this practicality New to be different from other modes described here using other to implement, therefore, the scope of protection of the utility model is simultaneously Do not limited by following public specific embodiment.

Fig. 1 to Fig. 6 shows the structural representation of the fixture of the embodiment according to the utility model first aspect.

As shown in Figures 1 to 6, a kind of fixture is provided according to one embodiment of the present utility model, for clamping sky The fuselage 20 of tune machine, including：Support frame 10, two slide rails 104 being parallel to each other are arranged at intervals on support frame 10；Two groups of clamping groups Part 12, it is connected and perpendicular to slide rail 104 with two slide rails 104；Drive component 14, it is connected with two groups of clamp assemblies 12, Drive component 14 drives two groups of clamp assemblies 12 to be moved along slide rail 104, has plane to be clamped between two groups of clamp assemblies 12 Fuselage 20；With two groups of components 16 of clamping jaw 162, the bottoms of two groups of clamp assemblies 12, two groups of components of clamping jaw 162 are separately positioned on 16 are oppositely arranged, and the opposite face for two clamping jaws 162 being oppositely arranged in two groups of components 16 of clamping jaw 162 has cambered surface 1622, with The fuselage 20 with cambered surface is clamped between two groups of components 16 of clamping jaw 162.

The utility model clamps the fuselage 20 with plane, such as rectangular fuselage 20 by two groups of clamp assemblies 12, The fuselage 20 with radian is clamped by two groups of components 16 of clamping jaw 162, such as cylindrical body 20, section are oval fuselage 20 etc. so that the fixture can clamp the fuselage 20 of various structures, improve the versatility of fixture, be advantageous to be controlled with robot Fixture carries out carrying upset to a variety of fuselages 20, improves the production capacity that the air conditioner of various types is assembled in production line production, section About cost, improve the space availability ratio of job shop.In utility model, during the fuselage 20 with plane is gripped, Drive component 14 drives two groups of clamp assemblies 12 to move to demand position and (can carry out tune according to the width of the fuselage 20 of air conditioner to set The driving duration or driving distance of drive component 14), to clamp fuselage 20, it is easy to carry upset；In machine of the gripping with radian During body 20, drive component 14 drives two groups of clamp assemblies 12 to move, and then drives two groups of components 16 of clamping jaw 162 to move to Demand position (can carry out adjusting the driving duration for setting drive component 14 or driving distance) according to the width of the fuselage 20 of air conditioner, lead to The cambered surface 1622 and the cambered surface of fuselage 20 for crossing the clamping jaw 162 of two groups of components 16 of clamping jaw 162 fit, to embrace fuselage 20 and clamp Fuselage 20.Preferably, drive component 14 has mnemonic, and adjustable adapts to different product, and servo provides stable demand Dynamics, it is preferable that drive component 14 includes stepper motor and leading screw, and leading screw one end is disposed therein the peace of one group of clamp assembly 12 Shelve on 122, the other end of leading screw is arranged on another group of clamp assembly 12 and is connected with stepper motor, driving stepper motor Leading screw is rotated to further or separate two groups of clamp assemblies 12.

In one embodiment of the present utility model, it is preferable that the distance between two groups of clamp assemblies 12 are less than or equal to two The distance between group component 16 of clamping jaw 162.

In this embodiment, between the distance between two groups of clamp assemblies 12 are less than two groups of components 16 of clamping jaw 162 away from From when, when clamp with plane fuselage 20 when, two groups of clamp assemblies 12 are clamped to the both sides of fuselage 20.When two groups of clampings When the distance between component 12 is equal to the distance between two groups of components 16 of clamping jaw 162, when clamping the fuselage 20 with plane, two Group clamp assembly 12 and two groups of components 16 of clamping jaw 162 simultaneously clamp on the both sides of fuselage 20, and further increasing clamping has plane Fuselage 20 stability.And when clamping the fuselage 20 with radian, two groups of components 16 of clamping jaw 162 are embraced fuselage 20 and carried out Clamp, furthermore it is preferred that when the distance between two groups of clamp assemblies 12 are equal to the distance between two groups of components 16 of clamping jaw 162, And a part for fuselage 20 at the plane for the upper end that U-shaped fuselage 20 is clamped by two groups of clamp assemblies 12, is led to when being U-shape structure Cross at the radian for the lower end that two groups of components 16 of clamping jaw 162 clamp U-shaped fuselage 20.

In one embodiment of the present utility model, it is preferable that the cambered surface 1622 of clamping jaw 162 is from top to bottom to fuselage 20 Clamping position where the cambered surface 1622 that gradually extends of direction, the vertical plane extended downwardly is provided with the lower end of cambered surface 1622 1624。

In this embodiment, the cambered surface 1622 of clamping jaw 162 is gradually to the cambered surface of the clamping position direction of fuselage 20 extension 1622, and then fuselage 20 can sufficiently be embraced and clamp fuselage 20 by two clamping jaws 162 being oppositely arranged, it is preferable that clamping jaw The radian and the radian of the cambered surface of fuselage 20 of 162 cambered surface 1622 match, in addition, the lower end of the cambered surface 1622 of clamping jaw 162 connects Vertical plane 1624 vertically downward is connect, not only increases the ability that cambered surface 1622 bears the gravity of fuselage 20, improves the knot of clamping jaw 162 Structure intensity, also cause when the distance between two groups of clamp assemblies 12 are equal to the distance between two groups of components 16 of clamping jaw 162, clamping jaw The vertical plane 1624 of 162 components 16 can clamp the both sides of the fuselage 20 with plane together with clamp assembly 12, improve and clamp surely It is qualitative, it is easy to carry upset.

In one embodiment of the present utility model, it is preferable that as shown in figure 4, clamping jaw in every group of component 16 of clamping jaw 162 162 number is at least one, and each clamping jaw 162 is anchored on clamp assembly 12 by the first fastener, wherein, each clamping jaw 162 move up and down along clamp assembly 12 and are fixed by the first fastener.

In this embodiment, when the number of clamping jaw 162 is multiple in every group of component 16 of clamping jaw 162, multipair clamping jaw 162 is simultaneously Embrace fuselage 20 and clamp fuselage 20, improve the steadiness for clamping fuselage 20, be easy to upset to carry, each clamping jaw 162 can edge Clamp assembly 12, which moves up and down, is again anchored on clamping jaw 162 on clamp assembly 12 by the first fastener, can be 162 by clamping jaw Need to adjust to suitable position according to the size of fuselage 20, be easy to clamp fuselage 20, also allowing for changing has different cambered surfaces 1622 Clamping jaw 162, further to match a variety of fuselages 20 and more firm clamping fuselage 20.Preferably, the first fastener is bolt, The two sides of the opposing clamping surfaces of each clamping jaw 162 fit with clamp assembly 12 and have screwed hole, are set on clamp assembly 12 There is the first slideway 1242, bolt stretches into the first chute through screwed hole, clamping jaw 162 is fastened on clamp assembly 12.

In one embodiment of the present utility model, it is preferable that as shown in Figure 3 and Figure 4, every group of clamp assembly 12 includes peace 122, at least one connecting bracket 124 and at least one clamping section 126 are shelved, mounting bracket 122 and two slide rails 104 are slided and connected Connect, at least one connecting bracket 124 is arranged on the lower surface of mounting bracket 122 and perpendicular to mounting bracket 122, at least one clamping section 126 are arranged at least one connecting bracket 124 close to the side of the clamping position of fuselage 20, for clamping the fuselage with plane 20。

In this embodiment, every group of clamp assembly 12 has the mounting bracket 122 being slidably connected with two slide rails 104, is pacifying The lower surface for shelving 122 sets at least one connecting bracket 124, in connecting bracket 124 close to the side of the clamping position of fuselage 20 At least one clamping section 126 is set, the fuselage 20 of air conditioner is clamped by clamping section 126.The utility model passes through drive component 14 drive installation framves 122 are moved, and then drive the connecting bracket 124 of two groups of clamp assemblies 12 mutually to draw close so that two groups are stepped up The clamping section 126 of component is mutually drawn close to clamp fuselage 20, or drives two groups of components 16 of clamping jaw 162 mutually to draw close to clamp fuselage 20, the clamping effect of fuselage 20 is improved, especially when the number of connecting bracket 124 is multiple, the number of clamping section 126 is more When individual, the clamping dynamics of fuselage 20 is further increased, is easy to carry upset fuselage 20.Preferably, the upper surface of mounting bracket 122 There are at least two sliding blocks, at least two sliding blocks are slidably connected with two slide rails 104 respectively, so that every group of clamp assembly 12 passes through cunning Block moves along slide rail 104.

In one embodiment of the present utility model, it is preferable that as shown in Figure 3 and Figure 4, when the number of connecting bracket 124 To be multiple, what multiple connecting brackets 124 were spaced is arranged on mounting bracket 122；When the number of clamping section 126 is one, one Clamping section 126 is arranged in multiple connecting brackets 124 simultaneously, or when the number of clamping section 126 is multiple, multiple clamping sections 126 corresponding are at the same time or separately arranged in multiple connecting brackets 124.

In this embodiment, what multiple connecting brackets 124 were spaced is arranged on mounting bracket 122, enables to two groups of clampings The connecting bracket 124 of component 12 is more evenly distributed, and then facilitates gripping by the fuselage 20 with certain length, improves and clamps fuselage 20 stability.One clamping section 126 is arranged in multiple connecting brackets 124 simultaneously, can balanced each connecting bracket 124 by The pressure of the fuselage 20 arrived, and then the stability for clamping fuselage 20 is improved, by setting multiple clamping sections 126, it is possible to increase folder The contact area of tight component 12 and fuselage 20, further improves the stability for clamping fuselage 20.

In one embodiment of the present utility model, it is preferable that as shown in Figure 3 and Figure 4, in every group of component 16 of clamping jaw 162 The number of clamping jaw 162 is identical with the number of the connecting bracket 124 of every group of clamp assembly 12, and at least one clamping jaw 162 is corresponding Be arranged at least one connecting bracket 124, and positioned at clamping section 126 lower section.

In this embodiment, the number of clamping jaw 162 matches with clamping the number of support, and clamping jaw 162 is located at clamping section 126 lower section so that when clamping the fuselage 20 with plane, fuselage 20 can be clamped by clamping section 126, now, be located at The clamping jaw 162 of the bottom of clamping section 126 can be bonded with the part of fuselage 20, can be also bonded completely, i.e., without interference with clamping section 126 Clamp；And when clamping the fuselage 20 with cambered surface, the upper edge of fuselage 20 is clamped by clamping jaw 162, now clamping section 126 1 As can't be fitted with fuselage 20, do not affect clamping of the clamping jaw 162 to fuselage 20, improve the versatility of fixture.

In one embodiment of the present utility model, it is preferable that as shown in Figure 3 and Figure 4, set in each connecting bracket 124 There is at least one the first slideway 1242 set along its short transverse, each clamping jaw 162 is anchored at least by the first fastener On one the first slideway 1242, wherein, each clamping jaw 162 shifts and tight by first along at least one first slideway about 1242 Firmware is fixed.

In this embodiment, connecting bracket 124 is provided with least one first slideway 1242, and clamping jaw 162 can pass through One fastener is fastened on the first slideway 1242, and can be moved up and down along the first slideway 1242, and then can suitably be adjusted as needed The position of whole clamping jaw 162, also allow for changing the clamping jaw 162 with different cambered surfaces 1622, further to match a variety of fuselages 20 simultaneously More firm clamping fuselage 20.Preferably, the first fastener is bolt, the two sides of the opposing clamping surfaces of each clamping jaw 162 with Clamp assembly 12 is fitted and has screwed hole, and bolt is stretched into the first chute through screwed hole, and clamping jaw 162 is fastened on into folder On tight component 12.

In one embodiment of the present utility model, it is preferable that the clamping of close fuselage 20 of clamp assembly 12 and clamping jaw 162 The clamping face of the side of position is provided with flexure strip 22.

In this embodiment, the face of stepping up of clamp assembly 12 and clamping jaw 162 is provided with elastic component, can effectively avoid fixture Cause abrasion etc. to destroy on fuselage 20 during fuselage 20 is clamped, effectively prevent fuselage 20 from scratching, add in addition, also improving The tightly frictional force between component, clamping jaw 162 and fuselage 20, and then improve the stability for clamping fuselage 20.Preferably, flexure strip 22 be silica gel piece.

In one embodiment of the present utility model, it is preferable that as shown in Figures 1 to 6, fixture also includes：Two groups of suckers 182 components 18, the bottom of two groups of clamp assemblies 12 is separately positioned on, two groups of components 18 of sucker 182 are oppositely arranged, for adsorbing The both sides of fuselage 20.

In this embodiment, fixture also has the component 18 of sucker 182, and the two of fuselage 20 are adsorbed by the component 18 of sucker 182 Side, it can further improve the fastness of fixture clamping fuselage 20.In the utility model, in fuselage 20 of the gripping with plane During, drive component 14 drives two groups of clamp assemblies 12 to move to demand position, after clamping fuselage 20, the module of sucker 182 Adsorb the fastness in the both sides of fuselage 20, further ensuring that fixture clamping air-conditioning；In the mistake of fuselage 20 of the gripping with radian Cheng Zhong, drive component 14 drive two groups of clamp assemblies 12 to move, and then drive two groups of components 16 of clamping jaw 162 to move to demand position Put, after embracing fuselage 20 and clamping fuselage 20, the module of sucker 182 adsorbs the both sides of fuselage 20, further ensures that fixture clamping is empty The fastness of tune.

In one embodiment of the present utility model, it is preferable that as shown in Figure 3 and Figure 4, every group of component 18 of sucker 182 wraps Include at least one sucker 182, at least one pole 184 and connecting rod 186, at least one pole 184 it is corresponding be arranged on to The back of a few sucker 182, at least one pole 184 are arranged in connecting rod 186, and connecting rod 186 is arranged on clamp assembly On 12.

In this embodiment, when the component 18 of sucker 182 has multiple suckers 182, it is possible to increase sucker 182 adsorbs fuselage 20 Dynamics, and then improve the firmness of fixture clamping fuselage 20, at least one sucker 182 is arranged on connecting rod by pole 184 On 186, connecting rod 186 is arranged on clamp assembly 12, is enabled in every group of component 18 of sucker 182, the height of each sucker 182 Degree is unified, and the convenient sustained height to fuselage 20 adsorbs, and the clip stability of fuselage 20 is improved, in addition, passing through connecting rod 186 unifications are installed at least one sucker 182 so that clamp structure is simple, improves the assembling speed of fixture.

In one embodiment of the present utility model, it is preferable that fixture also includes：Getter device, with least one pole 184 are connected, and pole 184 is hollow stem, and pole 184 is connected with sucker 182, and getter device is used to draw in sucker 182 Gas.

In this embodiment, getter device can draw the gas in sucker 182, fully be connect in sucker 182 and fuselage 20 After touch, the gas in sucker 182 is drawn by getter device, the inside of sucker 182 can be made to be in vacuum state or near vacuum State, and then the side plate of fuselage 20 can be preferably adsorbed, effectively ensure that fuselage 20 is not fallen out in handling process is overturn.It is excellent Selection of land, getter device are vacuum generator.

In one embodiment of the present utility model, it is preferable that fixture also includes：At least one magnetic valve, magnetic valve with At least one pole 184 is connected, for discharging the gas in pole 184.

In this embodiment, fixture also includes magnetic valve, when getter device draws the gas in sucker 182, opens electricity Magnet valve, to exclude gas, and when exhaust finishes, magnetic valve is closed, to be in negative pressure of vacuum shape in sucker 182 all the time State, it is ensured that fuselage 20 is not fallen out in handling process is overturn.Preferably, magnetic valve is four-way valve, while controls four poles 184 with extraneous break-make.

In one embodiment of the present utility model, it is preferable that as shown in figure 4, every group of clamp assembly 12 is provided with least One the second slideway 1244 set along its short transverse, connecting rod 186 move up and down along at least one second slideway 1244.

In this embodiment, connecting rod 186 can move up and down along the second slideway 1244 on clamp assembly 12, and then adjustable Section is arranged on the height of the sucker 182 in connecting rod 186, is advantageous to capture fuselage 20 of different shapes, it is ensured that fixture The fastness of fuselage 20 is clamped, is easy to carry upset.

In one embodiment of the present utility model, it is preferable that the second fastener is set on pole 184, and pole 184 is set In the spacing hole of connecting rod 186, centerline direction of the pole 184 along spacing hole moves through the second fastener and fixed.

In this embodiment, pole 184 is arranged in the spacing hole of connecting rod 186, and the second fastener is set in pole 184 On, when the second fastener does not fasten pole 184, pole 184 can move back and forth along spacing hole, can be to the installation site of fuselage 20 Direction move, can also support or oppose disembark body 20 installation site direction movement so that the component 18 of sucker 182 can be adsorbed preferably The outer surface of fuselage 20 of different shapes, especially cylindrical body 20, the adsorption effect of the component 18 of sucker 182 is improved, it is excellent Selection of land, spacing hole are screwed hole, and pole 184 is provided with relative external screw thread, and the second fastener is nut.

In one embodiment of the present utility model, it is preferable that as shown in Figures 4 to 6, the top of support frame 10 sets peace Fixed plate 102 is filled, mounting plate 102 is connected with mechanical arm, sensor is positioned proximate on mounting plate 102, to prevent machine Body 20 collides with support frame 10.

In this embodiment, the top of support frame 10 sets mounting plate 102, and mounting plate 102 and mechanical arm Connection so that robot etc. can control fixture carry out carrying upset to the fuselage 20 of air conditioner by mechanical arm, be advantageous to pair Air conditioner assembles, and improves the throughput rate of air conditioner, in addition, being positioned proximate to sensor on mounting plate 102, can keep away Exempt from fixture during fuselage 20 is gripped, support frame 10 collides with fuselage 20 and damages fuselage 20, improves air conditioner The security of assembling.

In the utility model, term " multiple " then refers to two or more, is limited unless otherwise clear and definite.Term The orientation or position relationship of instructions such as " on ", " under " are based on orientation shown in the drawings or position relationship, are for only for ease of and retouch State the utility model and simplify and describe, rather than instruction or imply signified device or element must have specific orientation, with Specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model；Term " installation ", " connected ", " company Connect ", the term such as " fixation " all should be interpreted broadly, for example, " connection " can be fixedly connected or be detachably connected, Or it is integrally connected；" connected " can be joined directly together, and can also be indirectly connected by intermediary.For the common of this area For technical staff, concrete meaning of the above-mentioned term in the utility model can be understood as the case may be.

In the description of this specification, the description of term " one embodiment ", " some embodiments ", " specific embodiment " etc. Mean that combining specific features, structure, material or feature that the embodiment or example describe is contained in of the present utility model at least one In individual embodiment or example.In this manual, identical embodiment is not necessarily referring to the schematic representation of above-mentioned term Or example.Moreover, specific features, structure, material or the feature of description can be in any one or more embodiments or example In combine in an appropriate manner.

Preferred embodiment of the present utility model is the foregoing is only, is not limited to the utility model, for this For the technical staff in field, the utility model can have various modifications and variations.It is all in the spirit and principles of the utility model Within, any modification, equivalent substitution and improvements made etc., it should be included within the scope of protection of the utility model.

Claims

A kind of 1. fixture, for clamping the fuselage of air conditioner, it is characterised in that including：

Support frame, two slide rails being parallel to each other are arranged at intervals on support frame as described above；

Two groups of clamp assemblies, it is connected and perpendicular to the slide rail with two slide rails；

Drive component, it is connected with clamp assembly described in two groups, the drive component drives clamp assembly described in two groups described in Slide rail moves, to clamp the fuselage with plane between clamp assembly described in two groups；With

Two groups of clip claw assemblies, the bottom of clamp assembly described in two groups being separately positioned on, clip claw assembly described in two groups is oppositely arranged, And the opposite face for two clamping jaws being oppositely arranged in clip claw assembly described in two groups has cambered surface, with clip claw assembly described in two groups it Between clamp with cambered surface the fuselage.
2. fixture according to claim 1, it is characterised in that

The distance between clamp assembly described in two groups is less than or equal to the distance between clip claw assembly described in two groups.
3. fixture according to claim 1, it is characterised in that

The cambered surface of the clamping jaw is the cambered surface gradually extended to the direction where the clamping position of the fuselage from top to bottom, The vertical plane extended downwardly is provided with the lower end of the cambered surface.
4. fixture according to claim 1, it is characterised in that

The number of clamping jaw described in clip claw assembly described in every group is at least one, and each clamping jaw is fastened by the first fastener In on the clamp assembly, wherein, each clamping jaw moves up and down along the clamp assembly and by first fastener It is fixed.
5. fixture according to any one of claim 1 to 4, it is characterised in that

Clamp assembly described in every group includes mounting bracket, at least one connecting bracket and at least one clamping section, the mounting bracket with Two slide rails are slidably connected, and at least one connecting bracket is arranged on the lower surface of the mounting bracket and perpendicular to described Mounting bracket, at least one clamping section are arranged at least one connecting bracket close to the one of the fuselage clamping position Side, for clamping the fuselage with plane.
6. fixture according to claim 5, it is characterised in that

When the number of the connecting bracket is multiple, multiple connecting bracket intervals are arranged on the mounting bracket；Work as institute When the number for stating clamping section is one, a clamping section is arranged in multiple connecting brackets simultaneously, or when the folder When the number in tight portion is multiple, multiple clamping sections are corresponding at the same time or separately to be arranged in multiple connecting brackets.
7. fixture according to claim 5, it is characterised in that

The number phase of the number of clamping jaw described in clip claw assembly and the connecting bracket of clamp assembly described in every group described in every group Together, and at least one clamping jaw is corresponding is arranged at least one connecting bracket, and positioned at the clamping section Lower section.
8. fixture according to claim 5, it is characterised in that

Each connecting bracket is provided with least one the first slideway set along its short transverse, and each clamping jaw passes through First fastener is anchored at least one first slideway, wherein, each clamping jaw is slided along at least one described first Road is shifted and fixed by first fastener up and down.
9. fixture according to any one of claim 1 to 4, it is characterised in that

The clamping face of the side of the close fuselage clamping position of the clamp assembly and the clamping jaw is provided with flexure strip.
10. fixture according to any one of claim 1 to 4, it is characterised in that also include：

Two groups of Suction cup assemblies, clamp assembly bottom described in two groups is separately positioned on, Suction cup assembly described in two groups is oppositely arranged, and is used In the both sides for adsorbing the fuselage.
11. fixture according to claim 10, it is characterised in that

Suction cup assembly described in every group includes at least one sucker, at least one pole and connecting rod, at least one pole phase The corresponding back for being arranged at least one sucker, at least one pole are arranged in the connecting rod, the company Extension bar is arranged on the clamp assembly.
12. fixture according to claim 11, it is characterised in that also include：

Getter device, it is connected with least one pole, the pole is hollow stem, and the pole is connected with the sucker Logical, the getter device is used to draw the gas in the sucker.
13. fixture according to claim 12, it is characterised in that also include：

At least one magnetic valve, the magnetic valve is connected with least one pole, for discharging the gas in the pole Body.
14. fixture according to claim 11, it is characterised in that

Clamp assembly described in every group is provided with least one the second slideway set along its short transverse, and the connecting rod is along at least One second slideway moves up and down.
15. fixture according to claim 11, it is characterised in that

Second fastener is set on the pole, and the pole is arranged in the spacing hole of the connecting rod, and the pole is along institute The centerline direction for stating spacing hole moves through second fastener and fixed.
16. fixture according to any one of claim 1 to 4, it is characterised in that

The top of support frame as described above sets mounting plate, and the mounting plate is connected with mechanical arm, the mounting plate On be positioned proximate to sensor, to prevent the fuselage and support frame as described above from colliding.