CN203510011U - Joint locator for unmanned aerial vehicle cementing tool - Google Patents
Joint locator for unmanned aerial vehicle cementing tool Download PDFInfo
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- CN203510011U CN203510011U CN201320659378.3U CN201320659378U CN203510011U CN 203510011 U CN203510011 U CN 203510011U CN 201320659378 U CN201320659378 U CN 201320659378U CN 203510011 U CN203510011 U CN 203510011U
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- joint
- screw thread
- pin bushing
- guide post
- guide pin
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Abstract
The utility model discloses a joint locator for an unmanned aerial vehicle cementing tool. The joint locator comprises a locating joint, a support, a threaded guide rod, a locating pin and a rotary guide mechanism, the locating joint is connected with the threaded guide rod by interference fit, all parts are supported by the support which is fixedly mounted on a cementing assembly tool device, the rotary guide mechanism is fixed into a support sleeve through quick-setting cement, the threaded guide rod can easily and axially move front and back by rotating operation of the rotary guide mechanism, and the locating joint is driven to advance and retreat, so that locating and separating of the joint locator are effectively finished. The joint locator is simple in structure, accurate in locating, convenient and easy in separating operation and not easy to deform, and product assembly efficiency and reliability of process equipment are improved.
Description
Technical field
The present invention relates to unmanned plane equipment Technology field, specifically, relate to a kind of joint location device that glueds joint frock for unmanned plane.
Background technology
At present, unmanned plane is all being brought into play more and more important effect in dual-use field, and unmanned plane housing construction is also along with the development of new material, new technology constantly changes.Composite, owing to having the advantages such as strong, the good corrosion resistance of high specific strength, high specific stiffness, good, the plastic design of forming technology and electromagnetic wave penetrability, is adopted by increasing unmanned plane.Cementing structure is to take composite structure to be main unmanned plane conventional a kind of version when skeleton and covering assembling, therefore, adhesive technology equipment, as the special equipment that guarantees unmanned plane skeleton and covering assembly quality and efficiency of assembling, also becomes numerous model unmanned planes one of necessary equipment in Product Assembly process.Compare with mechanical connection manner, at unmanned plane, glued joint in assembling process, bonding mode deflection is larger, technical process is more complicated, the adhesive technology feature that meets, the better joint location device of operability need to be set on adhesive technology equipment and guarantee that unmanned plane body adhesive technology process carries out smoothly, and finally meet the coordination interchangeability requirement of each component joints docking of unmanned plane body.
What existing unmanned plane adhesive technology equipment above used is a kind of plug-in structural joint locator.Plug-in structural joint locator slides vertically by guide rod, coordinates fastening screw to realize product joint location.Although its version can realize product joint and accurately locate, but be that high-precision slide coordinates due to what adopt between guide rod and locator guide pin bushing, resistance to sliding is larger, operating personnel are when plug formula joint location device, move forward and backward vertically guide rod more difficult, all need to use compared with great strength at every turn, even by instrument, just can complete.Especially after product joint, skeleton and covering have assembled, when product component undercarriage, because parts overall structure exists erection stress, its miniature deformation can cause between product joint and joint location device laminating very tight, can only just can complete the separated of product joint and joint location device by instrument.Plug-in structural joint locator, when meeting the requirement of product joint location, has but brought difficulty to operating personnel's work, has reduced production efficiency.Meanwhile, often, by instrument products of separated joint and joint location device, not only do not meet technological equipment operation requirements, and easily cause joint location device connection loosing and distortion, after using after a while, just must overhaul by butt joint locator, even must change landing nipple.
Utility model content
Large in order to overcome the resistance to sliding of existing plug-in structural joint locator guide rod, operation joint location device moves forward and backward more difficult problem, the utility model proposes a kind of joint location device that glueds joint frock for unmanned plane.This joint location device is simple in structure, accurate positioning, and during operation, landing nipple moves forward and backward convenient and strength-savingly, has improved the reliability of Product Assembly efficiency and technological equipment.
The utility model solves the technical scheme that its technical problem adopts: comprise landing nipple, bearing, screw thread guide post, fastening screw, rotary steering mechanism; Rotary steering mechanism also comprises guide pin bushing, turning handle, handle nut, T-shaped guide; Bearing provides support for other each parts, is fixedly mounted on and glueds joint on tooling device; Landing nipple and screw thread guide post interference fit, during positioning product joint, coordinate with guide pin bushing, screw thread guide post by fastening screw, realizes the location of landing nipple; Guide pin bushing is positioned at support base sleeve barrel, by quick hardening cement and support base sleeve barrel, is connected, and guide pin bushing inwall and screw thread guide post external diameter are slidably matched; T-shaped guide is positioned at the installing hole of guide pin bushing one end, and is slidably matched with the gathering sill on screw thread guide post; Handle nut is arranged in the draw-in groove of guide pin bushing one end, and handle nut inner thread is trapezoidal thread, and cooperatively interacts with the external screw thread of screw thread guide post; Turning handle and handle nut are connected, and the rotation by handle nut in guide pin bushing draw-in groove realizes screw thread guide post and advances vertically or retreat, and drive the location of landing nipple with separated.
Beneficial effect
A kind of joint location device that glueds joint frock for unmanned plane the utility model proposes.By landing nipple, bearing, screw thread guide post, fastening screw and rotary steering mechanism, formed; Landing nipple is connected with screw thread guide post, adopts interference fit; Bearing, for each parts provide support, is fixedly mounted on and glueds joint on assembly tooling equipment; Rotary steering mechanism is fixed in support base sleeve barrel by quick hardening cement, by the rotating operation of rotary steering mechanism, can easily complete screw thread guide post moving forward and backward vertically, drive landing nipple to move forward and backward, thereby the location that effectively completes joint location device be with separated.Joint location device is simple in structure, accurate positioning, lock out operation convenient, laborsaving, be difficult for deformation occurs, improved the reliability of efficiency of assembling and the technological equipment of product.
Accompanying drawing explanation
Below in conjunction with drawings and embodiments, a kind of joint location device for unmanned plane splicing frock of the utility model is described in further detail.
Fig. 1 is the utility model joint location device structural representation.
Fig. 2 is the utility model joint location device cutaway view.
Fig. 3 is the three-dimensional exploded view of the utility model joint location device structure.
In figure:
1. landing nipple 2. screw thread guide post 3. bearing 4. guide pin bushing 5. fastening screw 6. handle nut 7. turning handle 8.T type guides
The specific embodiment
The present embodiment is a kind of joint location device that glueds joint frock for unmanned plane.
Consult Fig. 1, Fig. 2, Fig. 3, the utility model is a kind of joint location device that glueds joint frock for unmanned plane, landing nipple 1, screw thread guide post 2, bearing 3, fastening screw 5 and rotary steering mechanism, consists of; Wherein, rotary steering mechanism comprises guide pin bushing 4, handle nut 6, turning handle 7, T-shaped guide 8.Landing nipple 1 and screw thread guide post 2 adopts interference fit to be arranged on screw thread guide post one end, and reinforces with Type of Welding, and the structure of landing nipple 1 is according to different product joint form and difference; Between screw thread guide post 2 and guide pin bushing 4, adopt and be slidably matched, guaranteeing under the prerequisite of hi-Fix, make screw thread guide post 2 in guide pin bushing 4, be convenient to slide.On screw thread guide post 2, in prefabricated keyway and on guide pin bushing 4 between prefabricated hole, pack T-shaped guide 8 into, screw thread guide post 2 can only be moved forward and backward vertically; Bearing 3 is the supporting construction of whole joint location device, and joint location device is fixed on adhesive technology equipment by bearing 3.Between bearing 3 and guide pin bushing 4, adopting process equipment is installed conventional quick hardening cement and is fixed connection; Fastening screw 5 is joined after the pin-and-hole drilling and reaming on insertion guide pin bushing 4 and screw thread guide post 2, realizes the hi-Fix of locus that landing nipple 1 is determined.
Rotary steering mechanism is the core of whole joint location device operation.Guide pin bushing 4 is fixed by quick hardening cement and support base sleeve barrel, and guide pin bushing 4 inwalls and screw thread guide post 2 external diameters adopt being slidably matched with precision; T-shaped guide 8 is arranged in the pre-manufactured hole of guide pin bushing one end, and with screw thread guide post 2 on prefabricated gathering sill adopt being slidably matched with precision; Handle nut 6 is arranged in the draw-in groove of guide pin bushing 4 one end, and freely rotates in draw-in groove, and handle nut 6 internal threads are trapezoidal thread, and cooperatively interacts with the external screw thread of screw thread guide post 2 one end.Rotation by handle nut 6 in guide pin bushing 4 draw-in grooves, realizes screw thread guide post 2 and advances vertically or retreat, and drives the location of landing nipple with separated.Turning handle 7 is threaded connection with handle nut 6, is fixed in the prefabricated screwed hole of handle nut 6, makes operating personnel when turning handle nut 6, convenient, laborsaving.
Operating process:
The utility model joint location device is mainly used in the location of product joint in adhesive technology equipment.When using joint location device to carry out product joint location, first being rotated in the forward by rotary steering mechanism handle nut 6, drive screw thread guide post 2 to move forward vertically in guide pin bushing 4, drive landing nipple 1 to move forward, at landing nipple 1, reach behind corresponding locus, use fastening screw 5 that the position of the landing nipple of joint location device 1 is fixed, guarantee the accuracy of landing nipple 1 locus and coordinate interchangeability; Then, product joint is positioned on landing nipple 1 by corresponding ladder latch, by size, transmits, guaranteed the accuracy of product joint locus and coordinated interchangeability.After the locus accurate positioning of product joint, can carry out the assembly connection operation between product joint and parts skeleton.
After between product joint and parts skeleton, assembly connection has operated, first fastening screw 5 and ladder latch corresponding to product joint are extracted, by the reverse rotation of rotary steering mechanism handle nut 6, drive screw thread guide post 2 to move backward vertically in guide pin bushing 4, drive landing nipple 1 to move backward, thereby realize the separated of landing nipple 1 and product joint, guaranteed the smooth undercarriage of product component after assembling completes.
Claims (1)
1. for unmanned plane, glued joint a joint location device for frock, it is characterized in that: comprise landing nipple, bearing, screw thread guide post, fastening screw, rotary steering mechanism; Rotary steering mechanism also comprises guide pin bushing, turning handle, handle nut, T-shaped guide; Bearing provides support for other each parts, is fixedly mounted on and glueds joint on tooling device; Landing nipple and screw thread guide post interference fit, during positioning product joint, coordinate with guide pin bushing, screw thread guide post by fastening screw, realizes the location of landing nipple; Guide pin bushing is positioned at support base sleeve barrel, by quick hardening cement and support base sleeve barrel, is connected, and guide pin bushing inwall and screw thread guide post external diameter are slidably matched; T-shaped guide is positioned at the installing hole of guide pin bushing one end, and is slidably matched with the gathering sill on screw thread guide post; Handle nut is arranged in the draw-in groove of guide pin bushing one end, and handle nut inner thread is trapezoidal thread, and cooperatively interacts with the external screw thread of screw thread guide post; Turning handle and handle nut are connected, and the rotation by handle nut in guide pin bushing draw-in groove realizes screw thread guide post and advances vertically or retreat, and drive the location of landing nipple with separated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320659378.3U CN203510011U (en) | 2013-10-24 | 2013-10-24 | Joint locator for unmanned aerial vehicle cementing tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320659378.3U CN203510011U (en) | 2013-10-24 | 2013-10-24 | Joint locator for unmanned aerial vehicle cementing tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203510011U true CN203510011U (en) | 2014-04-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320659378.3U Expired - Fee Related CN203510011U (en) | 2013-10-24 | 2013-10-24 | Joint locator for unmanned aerial vehicle cementing tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203510011U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106181832A (en) * | 2016-09-23 | 2016-12-07 | 江西洪都航空工业集团有限责任公司 | Belt lock catch clamp termination joint |
| CN106272183A (en) * | 2016-09-22 | 2017-01-04 | 无锡威孚力达催化净化器有限责任公司 | Synchronizing moving attitude reference device |
| CN106392950A (en) * | 2016-10-10 | 2017-02-15 | 北京航空航天大学 | Connection structure for positioners of aircraft assembly fixture |
| CN107293872A (en) * | 2016-04-13 | 2017-10-24 | 甘国强 | Conductor cable joint |
| CN108839814A (en) * | 2018-06-13 | 2018-11-20 | 江西昌河航空工业有限公司 | It is a kind of for changeing the device of tail boom connector |
| CN109703776A (en) * | 2019-01-30 | 2019-05-03 | 西安爱生技术集团公司 | The terminal position of small and medium size unmanned aerial vehicles wing assembly tooling |
| CN110239736A (en) * | 2019-05-17 | 2019-09-17 | 陕西飞机工业（集团）有限公司 | One kind changes the outfit tooling and costume changing method |
| CN110370218A (en) * | 2019-08-07 | 2019-10-25 | 沈阳飞机工业（集团）有限公司 | A kind of scalable turnover device for positioning support product |
-
2013
- 2013-10-24 CN CN201320659378.3U patent/CN203510011U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107293872A (en) * | 2016-04-13 | 2017-10-24 | 甘国强 | Conductor cable joint |
| CN106272183A (en) * | 2016-09-22 | 2017-01-04 | 无锡威孚力达催化净化器有限责任公司 | Synchronizing moving attitude reference device |
| CN106272183B (en) * | 2016-09-22 | 2017-11-10 | 无锡威孚力达催化净化器有限责任公司 | Synchronizing moving attitude reference device |
| CN106181832A (en) * | 2016-09-23 | 2016-12-07 | 江西洪都航空工业集团有限责任公司 | Belt lock catch clamp termination joint |
| CN106392950A (en) * | 2016-10-10 | 2017-02-15 | 北京航空航天大学 | Connection structure for positioners of aircraft assembly fixture |
| CN106392950B (en) * | 2016-10-10 | 2018-04-17 | 北京航空航天大学 | A kind of aircraft assembly fixture locator connection structure |
| CN108839814A (en) * | 2018-06-13 | 2018-11-20 | 江西昌河航空工业有限公司 | It is a kind of for changeing the device of tail boom connector |
| CN108839814B (en) * | 2018-06-13 | 2021-07-02 | 江西昌河航空工业有限公司 | Device for dismounting and replacing tail beam joint of helicopter |
| CN109703776A (en) * | 2019-01-30 | 2019-05-03 | 西安爱生技术集团公司 | The terminal position of small and medium size unmanned aerial vehicles wing assembly tooling |
| CN109703776B (en) * | 2019-01-30 | 2024-04-16 | 西安爱生技术集团公司 | Joint positioner of middle-size and small-size unmanned aerial vehicle wing assembly fixture |
| CN110239736A (en) * | 2019-05-17 | 2019-09-17 | 陕西飞机工业（集团）有限公司 | One kind changes the outfit tooling and costume changing method |
| CN110370218A (en) * | 2019-08-07 | 2019-10-25 | 沈阳飞机工业（集团）有限公司 | A kind of scalable turnover device for positioning support product |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140402 Termination date: 20141024 |
|
| EXPY | Termination of patent right or utility model |