CN105291036A - Quick assembling and disassembling device for aviation plug - Google Patents
Quick assembling and disassembling device for aviation plug Download PDFInfo
- Publication number
- CN105291036A CN105291036A CN201510878719.XA CN201510878719A CN105291036A CN 105291036 A CN105291036 A CN 105291036A CN 201510878719 A CN201510878719 A CN 201510878719A CN 105291036 A CN105291036 A CN 105291036A
- Authority
- CN
- China
- Prior art keywords
- aviation plug
- opening
- closing part
- jaw
- datum axis
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B27/00—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Connector Housings Or Holding Contact Members (AREA)
- Automatic Assembly (AREA)
Abstract
The invention relates to a quick assembling and disassembling device for an aviation plug. The quick assembling and disassembling device comprises a handheld part extending along a datum axis and an opening-closing mechanism extending in a direction perpendicular to the datum axis, wherein the opening-closing mechanism comprises two opening-closing parts; one end of each opening-closing part extends out of a hand-held handle; and a first interval which changes along with rotation of opening-closing parts is provided between the two handles. One side of each opening-closing part is correspondingly connected with two clamping jaws which can clamp or be separated from the outer surface of the aviation plug; a second interval communicated with the first interval is provided between the two clamping jaws; during assembling and disassembling of the aviation plug, a cable is blocked into cavities for clamping the aviation plug of the clamping jaws through the intervals which are communicated with each other; the clamping jaws are clamped on the outer surface of the aviation plug, and the disassembling for the aviation plug can be realized by rotating the handle; when the handle is rotated, the cable in the cavities can be kept still without rotating with the handle; and the two clamping jaws which can shrink and stretch out in a radial direction clamp the outer surface of the aviation plug, so that the device has universality.
Description
Technical field
The present invention relates to a kind of aviation plug fast assembling and disassembling device for loading and unloading aviation plug.
Background technology
Airborne, Shipborne Electronic Equipment aviation plug in use and maintenance process needs to carry out Fast Installation and dismounting easily, the chucking power that handler of the prior art applies is not by aviation plug center, because of can not effective envelope clamping aviation plug external cylindrical surface and occur skidding during handling, simultaneously aviation plug volume is little and on electronic equipment multiple aviation plug arrangement is closely, so often there is no separation space, usually need to adopt to load and unload successively from outside to inside and solve problem, this just have impact on the ratess of loading & discharge of aviation plug.
Chinese patent CN201979441U discloses a kind of Special spanner for aviation plugs, this spanner comprises bare terminal end for clamping aviation plug and extends along the axis direction of driving end, for hand-held handle, bare terminal end comprises the loop overlapping shape driving end matched with the profile of aviation plug, therefore use this spanner can load and unload any aviation plug of closely arrangement and install and remove aviation plug from outside to inside successively without the need to the demand in order to meet separation space, the driving end suitable with aviation plug profile ensure that spanner is applied to the center of chucking power by aviation plug of aviation plug simultaneously.But the side panel sealing of the driving end of the loop overlapping shape of this spanner thus its for screwing aviation plug time its on cable can hinder the use of this spanner, so this spanner can only be used for the installation of aviation plug and can not be used for the dismounting of aviation plug; This spanner specificity is strong simultaneously, and a spanner can only be used for a kind of aviation plug of specification, does not thus have versatility.
Summary of the invention
The object of the present invention is to provide a kind of fexible unit being connected with the aviation plug of cable for rapid-assembling/disassembling to solve the problem that Special spanner for aviation plugs specificity of the prior art is strong, can not be used for dismantling the aviation plug being connected with cable.
For solving this technical problem, a kind of aviation plug fast assembling and disassembling device of the present invention by the following technical solutions:
A kind of aviation plug fast assembling and disassembling device, comprise retained part, retained part has along the datum axis consistent with the axis direction of aviation plug when clamping, described aviation plug fast assembling and disassembling device also comprises open-and-close mechanism, open-and-close mechanism comprises the two or more opening and closing part around datum axis distribution, described opening and closing part is coordinated by hinged or guiding and can be moved relative to datum axis folding on the direction perpendicular to described datum axis, the other end relative with described hinged end or the abutting end that leads on described opening and closing part comprises for hand-held with the handle driving described open-and-close mechanism to rotate around datum axis direction, described retained part comprises at least two jaws around datum axis distributing that connect corresponding to opening and closing part, described jaw extends along datum axis direction and has the development length making open-and-close mechanism folding and not interfered by aviation plug, described jaw crowds around into the clamping chamber that can be enclosed within aviation plug outer surface, folding with opening and closing part is moved described jaw and is had the open mode of expansion clamping chamber release aviation plug and draw the clamp position of clamping chamber clamping aviation plug in, between adjacent opening and closing part under open mode, extending and the gap of through retained part and open-and-close mechanism along datum axis of being interconnected is formed between the corresponding jaw connected with opening and closing part, this gap is communicated with described clamping chamber and is formed to be passed through for aviation plug and institute's tape cable thereof along the direction perpendicular to datum axis and aviation plug can be made to enter the opening clamping chamber.
Described opening and closing part has upper and lower two and extend along perpendicular to the direction of datum axis, the left end of two opening and closing parts is rotationally connected by hinged realization, the right-hand member of two opening and closing parts has the first interval, and the central axis of rotation parallels with datum axis, and corresponding jaw also has two.
Described opening and closing part comprises the straight-bar forming described handle and the hook portion with arc concave surface being connected in described straight-bar end, on two opening and closing parts, the inner concave of hook portion is positioned opposite, being rotationally connected by bearing pin realization away from handle end of two hook portions, the axis of described bearing pin is parallel with datum axis; Described retained part also comprises the transit bridge fishplate bar for jaw being connected in the arc on corresponding opening and closing part, the width of jaw and transit bridge fishplate bar is identical and all have inner concave inner surface positioned opposite, the inner surface of two jaws crowds around into described clamping chamber, two transit bridge fishplate bars surround the cavity be connected with described clamping chamber, the left and right sides of jaw and transit bridge fishplate bar all has the second interval, and second interval on right side and described first interval are communicated with and constitute described gap.
Described two jaws are respectively upper gripper jaw and lower jaw, described opening and closing part is corresponding upper and lower opening and closing part, upper engaging lug spaced apart is equipped with at the left end of upper opening and closing part, lower engaging lug spaced apart is equipped with at the left end of lower opening and closing part, on upper and lower engaging lug, correspondence offers the hinge hole installed along the described bearing pin of the confession that datum axis direction is mutually through, and upper engaging lug is positioned at the outside of lower engaging lug; Described bearing pin is arranged with the torsion spring be between two lower engaging lugs, the top, one end of described torsion spring presses engaging lug other end top pressure engaging lug to realize the self-return of upper and lower jaw.
One end of described bearing pin comprises the positioning table coordinated with the lateral surface block of upper engaging lug, and the other end is provided with the alignment pin installing hole for installing alignment pin.
Described handler also comprises the position-limit mechanism limited the folding scope of described open-and-close mechanism.
Described position-limit mechanism be included in be in described torsion spring homonymy two engaging lugs on the corresponding limit shaft locating hole offered and spacing hole and the limit shaft that is installed in described spacing hole and limit shaft locating hole, described limit shaft and limit shaft locating hole threaded engagement, described spacing hole is scallop hole.
The side panel sealing of the driving end of the loop overlapping shape of special spanner of the prior art thus its for screwing aviation plug time its on cable can hinder the use of this spanner, so this spanner can only be used for the installation of aviation plug and can not be used for the dismounting of aviation plug; The driving end of this spanner has the shape suitable with the outer surface of aviation plug simultaneously, and a spanner can only be used for a kind of installation of aviation plug of specification, thus this spanner specificity strong, do not have versatility.
A kind of aviation plug fast assembling and disassembling device of the present invention comprises retained part and open-and-close mechanism, open-and-close mechanism has at least two around the opening and closing part of datum axis distribution, opening and closing part comprises for hand-held with the handle driving open-and-close mechanism to rotate around datum axis, retained part comprises the jaw of at least two connections corresponding to opening and closing part, jaw can clamp or depart from the outer surface of aviation plug under the drive of open-and-close mechanism, retained part and folding part has the gap that mutually through current supply cable passes, cable enter through gap thus jaw for clamping in the cavity of aviation plug, on the outer surface again jaw being clamped in aviation plug and turning handle can realize aviation plug dismounting, the cable be in during turning handle in cavity can keep static and can not rotate thereupon, this handler is by can the outer surface of at least two jaws clamping aviation plugs of folding simultaneously, and thus this device can be adapted to the aviation plug of different size, has versatility within the specific limits.
Accompanying drawing explanation
Fig. 1 is that an embodiment of a kind of aviation plug fast assembling and disassembling device in the present invention is for loading and unloading three-dimensional structure schematic diagram during aviation plug;
Fig. 2 is the front view of a kind of aviation plug fast assembling and disassembling device in Fig. 1;
Fig. 3 is the left view of Fig. 2;
Fig. 4 is structural representation when a kind of aviation plug fast assembling and disassembling device opening is normal in Fig. 2;
Fig. 5 be in Fig. 2 a kind of aviation plug fast assembling and disassembling device opening normal maximum time structural representation;
Fig. 6 is structural representation when a kind of aviation plug fast assembling and disassembling device opening is minimum in Fig. 2;
Fig. 7 is the syndeton schematic diagram of upper opening and closing part, upper gripper jaw and upper transit bridge fishplate bar in Fig. 2;
Fig. 8 is the right view of Fig. 7;
Fig. 9 is the F direction view of Fig. 7;
Figure 10 is the G direction view of Fig. 7;
Figure 11 is the E direction view of Fig. 8;
Figure 12 is the structural representation of spacer pin in Fig. 2;
Figure 13 is the structural representation of bearing pin in Fig. 2;
Figure 14 is the top view of Figure 13;
Figure 15 is the structural representation of the torsion spring in Fig. 2;
Figure 16 is the syndeton schematic diagram of lower opening and closing part, lower jaw and lower transit bridge fishplate bar in Fig. 2;
Figure 17 is the left view of Figure 16;
Figure 18 is the top view of Figure 16;
Figure 19 is that the A of Figure 16 is to sectional view;
Figure 20 is that the B of Figure 16 is to sectional view;
Figure 21 is the structural representation of alignment pin in Fig. 2.
Detailed description of the invention
A kind of embodiment of aviation plug fast assembling and disassembling device:
A kind of structure of aviation plug fast assembling and disassembling device is as shown in Fig. 1 ~ 21, the open-and-close mechanism comprising retained part and be connected with retained part, retained part comprises the upper gripper jaw 11 that the corresponding axis direction along aviation plug (i.e. datum axis) extends, lower jaw 21 and be connected in the upper transit bridge fishplate bar 13 of corresponding jaw rear end and lower transit bridge fishplate bar 23, the width of transit bridge fishplate bar is identical with the width of corresponding jaw, open-and-close mechanism comprises the upper opening and closing part 7 and lower opening and closing part 8 that are connected in corresponding transit bridge fishplate bar rear end, opening and closing part comprises the hook portion (comprising hook portion 71 and lower hook portion 81) with arc-shaped inner surface of left part and the straight-bar of right-hand member, on, the left end of lower opening and closing part realizes being rotationally connected by lock shaft 3, the straight-bar of the right-hand member of opening and closing part is for hand-held handle, corresponding handle comprises upper handle 72, lower handle 82, on, lower handle is (namely perpendicular to the direction of datum axis) extension all in left-right direction.Stretch out one section of upper mounting plate 73 outside the left end of upper opening and closing part 7 and be installed with engaging lug 14 on this platform, upper engaging lug 14 is intervally distributed with two along the longitudinal direction and erects on the downside of upper mounting plate 73; Correspondingly descend and stretch out one section of lower platform 83 outside the left end of opening and closing part 8 and on this platform, be installed with lower engaging lug 84, lower engaging lug 84 is intervally distributed with two along the longitudinal direction and erects on the downside of lower platform 83, and lower engaging lug 84 is on two between engaging lug 14.On upper engaging lug 74 and lower engaging lug 84, correspondence offers bearing pin installing hole, and bearing pin 3 is inserted in bearing pin installing hole.
Retained part has two symmetrical the second intervals of the left and right sides, and the right-hand member of two opening and closing parts has the first interval, and the second interval and first interval on right side are communicated with the gap defining and pass with current supply cable 10; Jaw and transit bridge fishplate bar all have inner concave inner surface positioned opposite, the inner surface of two jaws and two transit bridge fishplate bars has been crowded around into clamping chamber, and this clamping chamber and above-mentioned gap area, gap and clamping chamber define for aviation plug and institute tape cable thereof along perpendicular to datum axis direction by and aviation plug can be made to enter the opening clamping chamber, so cable can not rotate with the rotation of this handler in this handler can insert with cable aviation plug and when turning handle.Torsion spring 4 is sleeved on bearing pin 3 to make this handler to automatically reset, torsion spring 4 is between two lower engaging lugs 84, the top, a termination of torsion spring 4 is pressed in the upper engaging lug 74 of front side, the lower engaging lug 84 of top, another termination pressure rear side, for ease of top, torsion spring 4 two terminations pressure, the upper engaging lug 74 of front side is installed with convex platform 75, the lower engaging lug 84 of rear side is installed with lower convex platform 85.Limit shaft 5 is inserted into, in order in restriction in the perforation that lower opening and closing part is offered, the opening range of lower opening and closing part, the lower engaging lug 84 of rear side offers fan-shaped spacing hole 86, the upper engaging lug 74 of rear side offers limit shaft locating hole 76 corresponding with it, limit shaft 5 to be inserted in limit shaft locating hole 76 and spacing hole 86 and its threaded shaft section and limit shaft locating hole 76 threaded engagement, because the inserting of limit shaft 5 screw thread is in limit shaft locating hole 76, therefore the position of limit shaft 5 can be moved with upper opening and closing part 7, instantly opening and closing part 8 spacing hole 86 when upper opening and closing part 7 rotates towards the direction increasing opening moves relative to limit shaft 5, after moving to relevant position, the fan-shaped border of spacing hole 86 can coordinate with limit shaft 5 block and hinder opening further of lower opening and closing part 8, and then limit, the maximum of opening between lower opening and closing part.The front end of bearing pin 3 is provided with the positioning table 31 with the perforation limit block on upper opening and closing part 7, the rear end of bearing pin 3 is provided with alignment pin perforation 32, alignment pin 6 to be installed in alignment pin perforation 32 and state two is bent into as shown in figure 21 in case the handler that shotpin axle 3 gets loose and causes can not use.
Upper gripper jaw 11 has the upper inner concave 12 concentric with the outer peripheral face of aviation plug of arc, with the wide upper transit bridge fishplate bar 13 be connected, also there is the inner concave of arc with it and upper gripper jaw be connected on the leading flank of upper opening and closing part 7, when the length that the length of upper gripper jaw 11 and upper transit bridge fishplate bar 13 is greater than aviation plug is to ensure that this handler has the operative position of getting out of the way aviation plug thus makes the open-and-close mechanism of this device move in folding and rotate around datum axis can not interfere by aviation plug.Lower jaw 21 has the structure similar with upper gripper jaw 11, there is the lower inner concave 22 of downward arc, and being connected on the leading flank of upper opening and closing part 8 by lower transit bridge fishplate bar 23, the concave surface of upper and lower inner concave relatively symmetric clamp realizes the clamping to aviation plug 9 on the outer surface of aviation plug 9.
The assemble method of above-mentioned handler is as follows: by the bearing pin installing hole that the upper engaging lug 74 of the lower engaging lug 84 of the bearing pin installing hole that the lower engaging lug 84 of bearing pin 3 successively through the upper engaging lug 74 of rear side, rear side is offered, torsion spring 4, front side, front side is offered, again by alignment pin 6 through by two bending in case shotpin axle 3 gets loose, firmly upper and lower opening and closing part being closed up to normal specifications state around bearing pin 3 and namely spacer pin 5 is completed assembling process through in limit shaft locating hole 76 and spacing hole 86 successively in the alignment pin perforation of bearing pin 3 front end.
When having assembled rear use above-mentioned handler installation aviation plug 9, the gap on retained part and open-and-close mechanism only need be utilized to pass aviation plug 9 cable 10 below, then upper and lower jaw is reached the external cylindrical surface place of aviation plug 9, rotate to close up around bearing pin 3 again and the external cylindrical surface of aviation plug 9 is clamped, then whole device is rotated clockwise the Fast Installation that can realize aviation plug on air environment 9 around the center of aviation plug 9.When aviation plug 9 is dismantled, closed up the clamping of the external cylindrical surface of aviation plug 9 around bearing pin 3 rotation by upper and lower jaw, then whole device is rotated counterclockwise the quick-detachment that can realize aviation plug on air environment 9 around aviation plug 9 center.
In other embodiments, two opening and closing parts are also by the guiding movement mechanism of ensured opening and closing part disposed thereon edge perpendicular to the movement of datum axis direction; Described jaw can be the open-and-close mechanism that other can radial actuate, as elasticity fingertip; Described jaw also can be three, four or more; The bearing of trend of described handle also can not along the radial direction of aviation plug but along the axis direction of aviation plug or other directions; Also self-return torsion spring can not be established between upper and lower jaw; Described position-limit mechanism can also be the block fit structure that correspondence is arranged on upper gripper jaw and lower jaw, and block fit structure can be opened on opening and closing part, lower opening and closing part or on upper and lower opening and closing part and offer simultaneously; Also can save the spacing hole of restriction handler openings of sizes and spacing bearing pin.
Claims (7)
1. an aviation plug fast assembling and disassembling device, comprise retained part, retained part has along the datum axis consistent with the axis direction of aviation plug when clamping, it is characterized in that: described aviation plug fast assembling and disassembling device also comprises open-and-close mechanism, open-and-close mechanism comprises the two or more opening and closing part around datum axis distribution, described opening and closing part is coordinated by hinged or guiding and can be moved relative to datum axis folding on the direction perpendicular to described datum axis, the other end relative with described hinged end or the abutting end that leads on described opening and closing part comprises for hand-held with the handle driving described open-and-close mechanism to rotate around datum axis direction, described retained part comprises at least two jaws around datum axis distributing that connect corresponding to opening and closing part, described jaw extends along datum axis direction and has the development length making open-and-close mechanism folding and not interfered by aviation plug, described jaw crowds around into the clamping chamber that can be enclosed within aviation plug outer surface, folding with opening and closing part is moved described jaw and is had the open mode of expansion clamping chamber release aviation plug and draw the clamp position of clamping chamber clamping aviation plug in, between adjacent opening and closing part under open mode, extending and the gap of through retained part and open-and-close mechanism along datum axis of being interconnected is formed between the corresponding jaw connected with opening and closing part, this gap is communicated with described clamping chamber and is formed to be passed through for aviation plug and institute's tape cable thereof along the direction perpendicular to datum axis and aviation plug can be made to enter the opening clamping chamber.
2. a kind of aviation plug fast assembling and disassembling device according to claim 1, it is characterized in that: described opening and closing part has upper and lower two and extend along perpendicular to the direction of datum axis, the left end of two opening and closing parts is rotationally connected by hinged realization, the right-hand member of two opening and closing parts has the first interval, the central axis rotated parallels with datum axis, and corresponding jaw also has two.
3. a kind of aviation plug fast assembling and disassembling device according to claim 2, it is characterized in that: described opening and closing part comprises the straight-bar forming described handle and the hook portion with arc concave surface being connected in described straight-bar end, on two opening and closing parts, the inner concave of hook portion is positioned opposite, being rotationally connected by bearing pin realization away from handle end of two hook portions, the axis of described bearing pin is parallel with datum axis; Described retained part also comprises the transit bridge fishplate bar for jaw being connected in the arc on corresponding opening and closing part, the width of jaw and transit bridge fishplate bar is identical and all have inner concave inner surface positioned opposite, the inner surface of two jaws crowds around into described clamping chamber, two transit bridge fishplate bars surround the cavity be connected with described clamping chamber, the left and right sides of jaw and transit bridge fishplate bar all has the second interval, and second interval on right side and described first interval are communicated with and constitute described gap.
4. a kind of aviation plug fast assembling and disassembling device according to claim 3, it is characterized in that: described two jaws are respectively upper gripper jaw and lower jaw, described opening and closing part is corresponding upper and lower opening and closing part, upper engaging lug spaced apart is equipped with at the left end of upper opening and closing part, lower engaging lug spaced apart is equipped with at the left end of lower opening and closing part, on upper and lower engaging lug, correspondence offers the hinge hole installed along the described bearing pin of the confession that datum axis direction is mutually through, and upper engaging lug is positioned at the outside of lower engaging lug; Described bearing pin is arranged with the torsion spring be between two lower engaging lugs, the top, one end of described torsion spring presses engaging lug other end top pressure engaging lug to realize the self-return of upper and lower jaw.
5. a kind of aviation plug fast assembling and disassembling device according to claim 4, is characterized in that: one end of described bearing pin comprises the positioning table coordinated with the lateral surface block of upper engaging lug, and the other end is provided with the alignment pin installing hole for installing alignment pin.
6. a kind of aviation plug fast assembling and disassembling device according to claim 5, is characterized in that: described handler also comprises the position-limit mechanism limited the folding scope of described open-and-close mechanism.
7. a kind of aviation plug fast assembling and disassembling device according to claim 6, it is characterized in that: described position-limit mechanism be included in be in described torsion spring homonymy two engaging lugs on the corresponding limit shaft locating hole offered and spacing hole and the limit shaft that is installed in described spacing hole and limit shaft locating hole, described limit shaft and limit shaft locating hole threaded engagement, described spacing hole is scallop hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510878719.XA CN105291036B (en) | 2015-12-04 | 2015-12-04 | Quick assembling and disassembling device for aviation plug |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510878719.XA CN105291036B (en) | 2015-12-04 | 2015-12-04 | Quick assembling and disassembling device for aviation plug |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105291036A true CN105291036A (en) | 2016-02-03 |
| CN105291036B CN105291036B (en) | 2017-05-10 |
Family
ID=55189206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510878719.XA Active CN105291036B (en) | 2015-12-04 | 2015-12-04 | Quick assembling and disassembling device for aviation plug |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105291036B (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107538548A (en) * | 2016-06-24 | 2018-01-05 | 万象设计江苏有限责任公司 | A kind of quick dicing tools for beefsteak |
| CN109850172A (en) * | 2018-12-08 | 2019-06-07 | 中国航空工业集团公司洛阳电光设备研究所 | A kind of photoelectric nacelle platform locking mechanism |
| CN110561333A (en) * | 2019-09-23 | 2019-12-13 | 翟维 | Quick dismounting device of aviation plug |
| CN110744494A (en) * | 2019-11-20 | 2020-02-04 | 郑州德睿航联电子技术有限公司 | Quick assembly and disassembly device for aviation plug |
| CN111224714A (en) * | 2018-11-23 | 2020-06-02 | 无锡科晟光子科技有限公司 | Online centralized detection and management equipment by using OTDR (optical time domain reflectometer) |
| CN112894696A (en) * | 2021-01-14 | 2021-06-04 | 中国建筑第八工程局有限公司 | Tower crane snap ring unbinding device and unbinding method thereof |
| CN116581624A (en) * | 2023-07-13 | 2023-08-11 | 中北大学 | Manipulator special for aviation plug butt joint |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2749144Y (en) * | 2004-03-23 | 2005-12-28 | 华为技术有限公司 | A plug-pull tool |
| CN201061072Y (en) * | 2007-06-05 | 2008-05-14 | 中兴通讯股份有限公司 | High-density connector plug-in instrument |
| CN201741974U (en) * | 2010-09-10 | 2011-02-09 | 惠州住成电装有限公司 | Mistake proofing jig for plug mounting |
| CN201979441U (en) * | 2011-01-07 | 2011-09-21 | 中兴通讯股份有限公司 | Special spanner for aviation plugs |
| CN202004308U (en) * | 2010-07-13 | 2011-10-05 | 北京市电力公司 | Tool for pulling out and inserting aviation plug |
| EP2915618A1 (en) * | 2014-03-06 | 2015-09-09 | Orbis Will GmbH + Co. KG | Pliers or scissors |
| CN204976399U (en) * | 2015-09-11 | 2016-01-20 | 中国船舶重工集团公司第七0九研究所 | Clamp for circular circular connector of plug |
-
2015
- 2015-12-04 CN CN201510878719.XA patent/CN105291036B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2749144Y (en) * | 2004-03-23 | 2005-12-28 | 华为技术有限公司 | A plug-pull tool |
| CN201061072Y (en) * | 2007-06-05 | 2008-05-14 | 中兴通讯股份有限公司 | High-density connector plug-in instrument |
| CN202004308U (en) * | 2010-07-13 | 2011-10-05 | 北京市电力公司 | Tool for pulling out and inserting aviation plug |
| CN201741974U (en) * | 2010-09-10 | 2011-02-09 | 惠州住成电装有限公司 | Mistake proofing jig for plug mounting |
| CN201979441U (en) * | 2011-01-07 | 2011-09-21 | 中兴通讯股份有限公司 | Special spanner for aviation plugs |
| EP2915618A1 (en) * | 2014-03-06 | 2015-09-09 | Orbis Will GmbH + Co. KG | Pliers or scissors |
| CN204976399U (en) * | 2015-09-11 | 2016-01-20 | 中国船舶重工集团公司第七0九研究所 | Clamp for circular circular connector of plug |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107538548A (en) * | 2016-06-24 | 2018-01-05 | 万象设计江苏有限责任公司 | A kind of quick dicing tools for beefsteak |
| CN111224714A (en) * | 2018-11-23 | 2020-06-02 | 无锡科晟光子科技有限公司 | Online centralized detection and management equipment by using OTDR (optical time domain reflectometer) |
| CN111224714B (en) * | 2018-11-23 | 2021-03-05 | 无锡科晟光子科技有限公司 | Online centralized detection and management equipment by using OTDR (optical time domain reflectometer) |
| CN109850172A (en) * | 2018-12-08 | 2019-06-07 | 中国航空工业集团公司洛阳电光设备研究所 | A kind of photoelectric nacelle platform locking mechanism |
| CN110561333A (en) * | 2019-09-23 | 2019-12-13 | 翟维 | Quick dismounting device of aviation plug |
| CN110744494A (en) * | 2019-11-20 | 2020-02-04 | 郑州德睿航联电子技术有限公司 | Quick assembly and disassembly device for aviation plug |
| CN110744494B (en) * | 2019-11-20 | 2021-08-03 | 南京溧水高新产业股权投资有限公司 | Quick assembly and disassembly device for aviation plug |
| CN112894696A (en) * | 2021-01-14 | 2021-06-04 | 中国建筑第八工程局有限公司 | Tower crane snap ring unbinding device and unbinding method thereof |
| CN112894696B (en) * | 2021-01-14 | 2024-03-12 | 中国建筑第八工程局有限公司 | Tower crane snap ring unbinding device and unbinding method thereof |
| CN116581624A (en) * | 2023-07-13 | 2023-08-11 | 中北大学 | Manipulator special for aviation plug butt joint |
| CN116581624B (en) * | 2023-07-13 | 2023-09-22 | 中北大学 | Manipulator special for aviation plug butt joint |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105291036B (en) | 2017-05-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105291036A (en) | Quick assembling and disassembling device for aviation plug | |
| US10000955B2 (en) | Biaxial hinge and terminal device using the same | |
| CN107614143B (en) | Product turnover mechanism | |
| CN103090115A (en) | Method and structure for quickly fixing hoop | |
| CN108214377B (en) | Screwdriver | |
| EP3037212B1 (en) | Wrench combining sleeve | |
| US20160113133A1 (en) | Housing locking apparatus | |
| CN104827974A (en) | Glove box limiter and glove box assembly having same | |
| CN108724100A (en) | Pressure ring attaching/detaching apparatus and equipment | |
| CN206998807U (en) | Circlip tongs | |
| US9689526B2 (en) | Housing with support assembly | |
| CN105489234A (en) | Built-in plug device for storage disk of airborne recording device | |
| CN102427187A (en) | Anti-misplug quick lock connector assembly and plug and socket thereof | |
| CN210819304U (en) | Combined socket wrench | |
| CN208681492U (en) | Pressure ring attaching/detaching apparatus and equipment | |
| CN201475155U (en) | Pivot device | |
| CN201391539Y (en) | Hinge device | |
| CN210704518U (en) | Socket spanner | |
| CN100505997C (en) | Arrangement for detachably fastening a component to a frame part | |
| US9770797B2 (en) | Tool positioning and holding mechanism | |
| CN211841740U (en) | Novel hexagonal wrench | |
| CN209617524U (en) | A kind of unmanned machine head quick-disassembly structure | |
| CN207851733U (en) | A kind of 1U servers easy to repair for replacing Wiring port | |
| CN205291005U (en) | Stamping manipulator and press from both sides tool quick detach mechanism thereof | |
| CN110000597B (en) | Manual flexible clamping mechanism |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |