CN108818380A - A kind of low torsion multiple purpose aeroplane electrification wrench device - Google Patents

A kind of low torsion multiple purpose aeroplane electrification wrench device Download PDF

Info

Publication number
CN108818380A
CN108818380A CN201810562913.0A CN201810562913A CN108818380A CN 108818380 A CN108818380 A CN 108818380A CN 201810562913 A CN201810562913 A CN 201810562913A CN 108818380 A CN108818380 A CN 108818380A
Authority
CN
China
Prior art keywords
shell
group
hole
electromagnet
handle
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.)
Withdrawn
Application number
CN201810562913.0A
Other languages
Chinese (zh)
Inventor
苏亚斌
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cao Jiayang
Original Assignee
Cao Jiayang
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Cao Jiayang filed Critical Cao Jiayang
Priority to CN201810562913.0A priority Critical patent/CN108818380A/en
Publication of CN108818380A publication Critical patent/CN108818380A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B21/00Portable power-driven screw or nut setting or loosening tools; Attachments for drilling apparatus serving the same purpose
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B13/00Spanners; Wrenches
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B23/00Details of, or accessories for, spanners, wrenches, screwdrivers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B23/00Details of, or accessories for, spanners, wrenches, screwdrivers
    • B25B23/0007Connections or joints between tool parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B23/00Details of, or accessories for, spanners, wrenches, screwdrivers
    • B25B23/14Arrangement of torque limiters or torque indicators in wrenches or screwdrivers
    • B25B23/147Arrangement of torque limiters or torque indicators in wrenches or screwdrivers specially adapted for electrically operated wrenches or screwdrivers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Tyre Moulding (AREA)
  • Details Of Spanners, Wrenches, And Screw Drivers And Accessories (AREA)

Abstract

The invention discloses a kind of low torsion multiple purpose aeroplane electrification wrench devices, are related to spanner technical field.It includes handle, torquer, sizing fixing device;The torquer includes connection frame, the master control gear, motor of " V " font;It is connect in the middle part of connection frame with handle front end;The positioning shell of arc is respectively connected at left and right sides of connection frame front;It positions shell-side side indent and master control gear edge cooperates;Spliced eye is uniformly provided in guide groove;It slidably connects in through-hole and is locked with the control of spliced eye cooperation;The sizing fixing device includes the shell being fixedly connected with inner wall of the hole installing, multiple groups A group electromagnet and B group electromagnet;The elastomeric bladder of annular is nested and fixed in shell;Shear thickening liquid is filled in elastomeric bladder, even suspension is magnetic particle in shear thickening liquid;It is fixedly connected on the outside of elastomeric bladder with interior of shell.The beneficial effects of the invention are as follows:Specification is adjusted quickly, adaptable, easy to operate, time saving and energy saving.

Description

A kind of low torsion multiple purpose aeroplane electrification wrench device
Technical field
The present invention relates to spanner technical fields.
Background technique
Spanner is a kind of common installation and removal tool, twists bolt, screw, nut and other spiral shells using lever principle Line tightly holds the opening of bolt or nut or the hand tools of trepanning firmware.General spanner is divided into solid wrench and adjustable wrench, adjustable wrench The use that opening adapts to plurality of specifications can be adjusted in a certain range, but it is generally unstable using semi-surrounding mode, connection, it leads There are Problem of Failure in cause torque transmittance process, and when carrying out opening adjusting, quickly cannot disposably adjust in place, It makes troubles to operator, manually adjusts repeatedly and cause operation fatigue.In a kind of general low torsion multiple purpose aeroplane electrification spanner dress It sets when in use, quickly rotation can be divided into and large torque exerts a force two stages, therefore should be able to meet and between the two quickly cut It changes.
Summary of the invention
The technical problems to be solved by the invention are that it is multi-purpose to provide a kind of low torsion for above-mentioned technical deficiency Electromechanicsization wrench device.Specification is adjusted quickly, adaptable, easy to operate, time saving and energy saving.
The technical solution adopted by the present invention is that:A kind of low torsion multiple purpose aeroplane electrification wrench device, including handle, torque are provided Device, sizing fixing device;The torquer includes connection frame, the master control gear, motor of " V " font;In the middle part of connection frame It is connect with handle front end;The positioning shell of arc is respectively connected at left and right sides of connection frame front;Position shell-side side indent and master control tooth Take turns edge mate;Master control gear upper surface is provided with the guide groove of annular;Upper end is fixedly connected to the guiding of arc in positioning shell Item, gib block and guide groove are slidably connected;The positioning shell upper end of side is provided with through-hole, and through-hole runs through gib block and guide groove It is corresponding;Spliced eye is uniformly provided in guide groove;It slidably connects in through-hole and is locked with the control of spliced eye cooperation, control lock lower part is cut It locks end at right angled triangle, control and is fixed with swivel plate in face;The positioning shell upper end of side is fixedly connected with horizontal mounting plate; The output end of motor passes through mounting plate and is connected with driving gear downwards, and driving gear engages cooperation with master control gear;Master control gear Middle part is provided with mounting hole, installation sizing fixing device in mounting hole;The sizing fixing device includes solid with inner wall of the hole installing Surely shell, multiple groups A group electromagnet and the B group electromagnet connected;The elastomeric bladder of annular is nested and fixed in shell;It is filled out in elastomeric bladder Filled with shear thickening liquid, even suspension is magnetic particle in shear thickening liquid;It is fixedly connected on the outside of elastomeric bladder with interior of shell, bullet Property intracapsular side wall along annular be uniformly fixed with vertical joint strip;A group electromagnet is identical with B group electromagnet group number, and every group of A group Electromagnet and B group electromagnet include no less than about two electromagnet disposed in parallel;Even angular intervals on the wall of outer side of shell A group electromagnet is installed, every two is between adjacent A group electromagnet, installing one group of B group electromagnet on the wall of outer side of shell.
Advanced optimize the technical program, a kind of connection frame front left and right sides of low torsion multiple purpose aeroplane electrification wrench device It is rotatablely connected respectively with the positioning shell of two sides.
The technical program is advanced optimized, in the middle part of a kind of connection frame of low torsion multiple purpose aeroplane electrification wrench device and before handle End rotation connection.
Advanced optimize the technical program, a kind of handle of low torsion multiple purpose aeroplane electrification wrench device is divided into front and back two Point, it is connected between front and back two parts of handle for shaft.
Advanced optimize the technical program, a kind of left and right sides of the handle of low torsion multiple purpose aeroplane electrification wrench device covers It connects and is fixed with rubber strip.
Advanced optimize the technical program, a kind of middle handle of low torsion multiple purpose aeroplane electrification wrench device is uniformly provided with rule The different hexagon ring of lattice;Sliding friction is combined with hexagon prism in hexagon ring, and hexagon prism upper diameter is greater than lower diameter, hexagon prism Height value be not more than hexagon ring depth value.
Advanced optimize the technical program, a kind of handle rear portion of low torsion multiple purpose aeroplane electrification wrench device is provided with hexagon Sleeve joint hole.
Advanced optimize the technical program, a kind of low torsion multiple purpose aeroplane electrification wrench device in sleeve joint hole front and rear sides, Handle rear portion is symmetrically arranged with card slot, and card slot is connected to sleeve joint hole;Two card slot plug connections have the fixation of " n " font Plate;A word cutter head is fixed in the middle part of fixed plate downwards.
The beneficial effects of the invention are that:
1, torquer is connected with handle, realizes manual large torque force, convenient for loosening or stepping up, motor is driven in torquer Realize quickly small torque rotation, it is time saving and energy saving.The positioning shell of two sides plays position-limiting action, gib block and guide groove to master control gear With closing main guiding connection function, the cooperation of control lock and spliced eye is, it can be achieved that handle and master control gear one-directionally rotate Be fixedly connected, be easy to implement large torque force, while the active of master control gear not hindered rotate, switching is quick just between the two Just, convenient for opening the rotation after motor, motor can engaging by driving gear and master control gear, drive master control gear it is quick Rotation.Master control gear is fixedly connected with sizing fixing device, realizes torque transmitting.
It is formed in fixing device, using the characteristic of shear thickening liquid, realizes elastomeric bladder to the bolt head of plurality of specifications etc. It links closely after fitting, solidifies shear thickening liquid using the vibration that magnetic-particle drives, the sizing and solidifying of elastomeric bladder is realized, using complete Structure is surrounded, is transferred torque on the parts such as bolt, realizes and drives rotation, the bolt etc. of plurality of specifications can be adapted to simultaneously, is adapted to Property it is strong, adjust quickly, installation and removal are convenient and efficient.The setting of elastomeric bladder inner sidewall joint strip, can be such that joint strip connects with bolt surface Touching reduces the abrasion on elastomeric bladder surface, guarantees service life.It can be produced by control A group electromagnet and the power supply of the group electromagnet interval B Magnetisation makes magnetic-particle under the magnetic force of the opposite both direction of interval action, realizes fast vibration, so that shearing be made to increase Magma internal vibration realizes solidification;
2, the rotation connection at left and right sides of connection frame front with the rotation connection of positioning shell, connection frame middle part with handle, handle point For front and back two parts and shaft connects three kinds of structures and can be improved the adaptability to operating space structure, more practical;
3, the hexagon prism of different size is sliding combined in the hexagon ring of different size, surfacing is, it can be achieved that internal hexagonal spiral shell The operation of the connectors such as bolt, function is more, easy to use;
4, hexagonal sleeve joint hole can be adapted to the hex bolts of certain specification, be convenient to directly be socketed use, handle portion is not The hexagon ring of same specification can play phase same-action.
It is provided with card slot before and after sleeve joint hole and is combined with fixed plate, realize using a word cutter head to a word or plus screw etc. Device is operated, easy to operate, and function is more.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention;
Fig. 2 is present invention sizing fixing device decomposition texture schematic diagram;
Fig. 3 is sizing fixing device planar structure schematic diagram;
Fig. 4 is torquer part-structure decomposition diagram;
Fig. 5 is that control lock uses structural plan schematic diagram;
Fig. 6 is torquer using state structure diagram;
Fig. 7 is torquer another kind using state structure diagram;
In figure, 1, handle;2, connection frame;3, shell is positioned;4, master control gear;5, guide groove;6, gib block;7, through-hole;8, grafting Hole;9, control lock;10, swivel plate;11, mounting plate;12, driving gear;13, mounting hole;14, shell;15, A group electromagnet; 16, elastomeric bladder;17, joint strip;18, rubber strip;19, hexagon ring;20, hexagon prism;21, sleeve joint hole;22, card slot;23, fixed plate; 24, a word cutter head;25, B group electromagnet;26, magnetic-particle;27, motor.
Specific embodiment
The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.
As shown in figs. 1-7, a kind of low torsion multiple purpose aeroplane electrification wrench device, including handle 1, torquer, sizing link closely Device;The torquer includes the connection frame 2, master control gear 4, motor 27 of " V " font;Before 2 middle part of connection frame and handle 1 End connection;The positioning shell 3 of arc is respectively connected at left and right sides of 2 front of connection frame;Position 3 side indent of shell and 4 side of master control gear Edge cooperation;4 upper surface of master control gear is provided with the guide groove 5 of annular;Upper end is fixedly connected to the gib block of arc in positioning shell 3 6, gib block 6 and guide groove 5 are slidably connected;3 upper end of positioning shell of side is provided with through-hole 7, through-hole 7 through gib block 6 with Guide groove 5 is corresponding;Spliced eye 8 is uniformly provided in guide groove 5;The control lock 9 cooperated with spliced eye 8 is slidably connected in through-hole 7, Control 9 lower sections of lock are fixed with swivel plate 10 at right angled triangle, 9 upper ends of control lock;3 upper end of positioning shell of side is fixed to be connected It is connected to horizontal mounting plate 11;The output end of motor 27 passes through mounting plate 11 and is connected with driving gear 12, driving gear 12 downwards Cooperation is engaged with master control gear 4;Mounting hole 13 is provided in the middle part of master control gear 4, installation sizing fixing device in mounting hole 13;It is described Sizing fixing device include the shell 14 being fixedly connected with 13 inner wall of mounting hole, multiple groups A group electromagnet 15 and B group electromagnet 25;The elastomeric bladder 16 of annular is nested and fixed in shell 14;It is filled with shear thickening liquid in elastomeric bladder 16, in shear thickening liquid It is even to be suspended with magnetic-particle 26;The outside of elastomeric bladder 16 be fixedly connected inside shell 14,16 inner sidewall of elastomeric bladder is uniform along annular It is fixed with vertical joint strip 17;A group electromagnet 15 is identical with 25 groups of numbers of B group electromagnet, and every group of A group electromagnet 15 and B group Electromagnet 25 includes no less than about two electromagnet disposed in parallel;Even angular intervals install A group on 14 lateral wall of shell Electromagnet 15, every two install one group of B group electromagnet 25 between adjacent A group electromagnet 15 on 14 lateral wall of shell;Connection frame 2 It is rotatablely connected respectively with the positioning shell 3 of two sides at left and right sides of front;2 middle part of connection frame is rotatablely connected with 1 front end of handle;Handle 1 It is divided into front and back two parts, is connected between front and back two parts of handle 1 for shaft;Rubber is nested and fixed in the left and right sides of handle 1 Adhesive tape 18;1 middle part of handle is uniformly provided with hexagon ring 19 diversified in specifications;Sliding friction is combined with hexagon prism 20 in hexagon ring 19, 20 upper diameter of hexagon prism is greater than lower diameter, and the height value of hexagon prism 20 is not more than the depth value of hexagon ring 19;1 rear portion of handle It is provided with hexagonal sleeve joint hole 21;In 21 front and rear sides of sleeve joint hole, 1 rear portion of handle is symmetrically arranged with card slot 22, card slot 22 and set Connect the connection of hole 21;Two 22 plug connections of card slot have the fixed plate 23 of " n " font;23 middle part of fixed plate is fixed with downwards one Word cutter head 24.
In the use of the present invention, for being operated to bolt, as shown in Figure 1-3, by 16 sets of elastomeric bladder outside bolt Side is realized by the elasticity of elastomeric bladder 16 itself and is adjacent to package on the outside of bolt, due to the elasticity of elastomeric bladder 16 itself, in Diameter can be changed to the larger value by smaller value, and it is semi-surrounding structure with elastomeric bladder 16, upper space can be that shell section, which is " C " shape, Compressive deformation provides deformation space, then controls A group electromagnet 15 and B group electromagnet 25, and the vibration of magnetic-particle 26 makes elastomeric bladder Shear thickening liquid vibration solidification in 16, elastomeric bladder 16 is formed immediately, can carry out the transmitting of torque, realizes the torsion to bolt.Patch Item 17 should not be arranged too much, and a large amount of joint strip 17 then influences whether the contraction of 16 internal diameter of elastomeric bladder, and joint strip 17 can be steel bar etc..Magnetic Property particle 26 be magnetic material, such as magnet grains can be in this suspension of shear thickening liquid, and magnet grains etc. can be formed Divide and suspends.
As shown in figure 3, by the way of the power supply of the two interval, opening A when control A group electromagnet 15 and B group electromagnet 25 Group electromagnet 15, then A group electromagnet 15 generates rapidly magnetic, attracts magnetic-particle 26 to move to A group electromagnet 15, then cuts off The power supply of A group electromagnet 15 is powered B group electromagnet 25, then 26 stress of magnetic-particle is moved to B group electromagnet, so Back and forth, quickly commutation, realizes vibration at high speed.
As shown in figures 1,4 and 5, when being installed to bolt it is last tighten or most start when dismantling when unscrewing, need Biggish torque is provided, is exerted a force at this time by handle 1, remaining can drive rotation by the rotation of motor 27.To tighten clockwise For, motor 27 is first turned on, drives driving gear 12 to rotate counterclockwise, is engaged with master control gear 4, drives master control gear 4 suitable Rotation is transferred to bolt by elastomeric bladder 16, bolt rotation is driven to tighten, at this time by the side of 9 lower parts of control lock by hour hands rotation Position it is found that master control gear 4 rotation, drive inclined surface that control lock will be made 9 to move up, control lock 9 will not stop master control gear 4 It actively rotates clockwise, after turning to a certain degree, when need to apply large torque, closes motor 27, left and right slight oscillatory handle 1, slide positioning shell 3 in the guide groove 5 of master control gear 4, the effect of pressure under control 9 self gravitys of lock or application Under, make then to apply the power rotated clockwise in the spliced eye 8 below 9 insertion of control lock to handle 1 manually, be transmitted to positioning Shell 3, by the connection at control lock 9, control 9 vertical planes of lock drive master control gear 4 to continue to rotate clockwise, by what is applied manually Large torque is transmitted on bolt, completes to tighten.Control lock 9 can be transition fit or clearance fit with through-hole 7.
When needing to unscrew counterclockwise, 10 1 hundred 80 degree of swivel plate are rotated, control lock 9 is made to exchange the orientation of inclined surface, Motor 27 inverts, remaining Principle of Process is same as above, and suitably operate.
Motor 27 and control lock 9 can do two groups of settings of bilateral symmetry.
As shown in Figure 6,7, handle 1 can realize the force control in a variety of orientation after rotation, and the setting of rubber strip 18 can mention The hand-held comfort of height.
Hexagon socket head cap screw etc. is common connector, and is the lesser interior hexagonal of specification in, on handle 1 The lower part for the hexagon prism 20 being coupled can be adapted to several regular sizes of hexagon socket head cap screw, be easy to use, hexagon prism 20 tops are greater than lower part, can slide up and down in hexagon ring 19, and the lower part of hexagon prism 20 is made to expose and cooperate with interior hexagonal, rotation Handle 1 provides torque.The use of sizing fixing device can be reduced, it is energy saving, or make up to the connector of specification very little Applicability.
It when encountering the word or plus screw of oval head, is operated using fixed plate 23,21 sets of sleeve joint hole is existed On the outside of screw, push fixed plate 23, make in a word cutter head 24 insertion screw, rotating handle 1 can applied force, a word cutter head 24 is right Minus screw and plus screw have adaptability.

Claims (1)

1. a kind of low torsion multiple purpose aeroplane electrification wrench device, it is characterised in that:Including handle, torquer, sizing fixing device; The torquer includes connection frame, the master control gear, motor of " V " font;It is connect in the middle part of connection frame with handle front end;Connection The positioning shell of arc is respectively connected at left and right sides of frame front;It positions shell-side side indent and master control gear edge cooperates;Master control gear Upper surface is provided with the guide groove of annular;Upper end is fixedly connected to the gib block of arc in positioning shell, and gib block and guide groove are sliding It is dynamic to be cooperatively connected;The positioning shell upper end of side is provided with through-hole, and through-hole is corresponding with guide groove through gib block;It is uniformly opened in guide groove There is spliced eye;It slidably connects in through-hole and is locked with the control of spliced eye cooperation, control lock lower section is at right angled triangle, control It locks end and is fixed with swivel plate;The positioning shell upper end of side is fixedly connected with horizontal mounting plate;The output end of motor passes through peace Loading board is connected with downwards driving gear, and driving gear engages cooperation with master control gear;It is provided with mounting hole in the middle part of master control gear, is installed Installation sizing fixing device in hole;The sizing fixing device includes the shell being fixedly connected with inner wall of the hole installing, multiple groups A group Electromagnet and B group electromagnet;The elastomeric bladder of annular is nested and fixed in shell;Shear thickening liquid, shearing are filled in elastomeric bladder Even suspension is magnetic particle in thickening fluid;It is fixedly connected on the outside of elastomeric bladder with interior of shell, elastomeric bladder inner sidewall is equal along annular It is even to be fixed with vertical joint strip;A group electromagnet is identical with B group electromagnet group number, and every group of A group electromagnet and B group electromagnet Including being no less than about two electromagnet disposed in parallel;Even angular intervals installation A group electromagnet on the wall of outer side of shell, every two It is a between adjacent A group electromagnet, installing one group of B group electromagnet on the wall of outer side of shell;Middle handle is uniformly provided with diversified in specifications Hexagon ring;Sliding friction is combined with hexagon prism in hexagon ring, and hexagon prism upper diameter is greater than lower diameter, the height value of hexagon prism No more than the depth value of hexagon ring;Handle rear portion is provided with hexagonal sleeve joint hole;In sleeve joint hole front and rear sides, handle rear portion is symmetrical It is provided with card slot, card slot is connected to sleeve joint hole;Two card slot plug connections have the fixed plate of " n " font;In the middle part of fixed plate It is fixed with a word cutter head downwards.
CN201810562913.0A 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device Withdrawn CN108818380A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810562913.0A CN108818380A (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201810562913.0A CN108818380A (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device
CN201710515367.0A CN107309832B (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CN201710515367.0A Division CN107309832B (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device

Publications (1)

Publication Number Publication Date
CN108818380A true CN108818380A (en) 2018-11-16

Family

ID=60179856

Family Applications (4)

Application Number Title Priority Date Filing Date
CN201710515367.0A Active CN107309832B (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device
CN201810562913.0A Withdrawn CN108818380A (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device
CN201810563641.6A Withdrawn CN108818383A (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device
CN201810563612.XA Withdrawn CN108818382A (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device

Family Applications Before (1)

Application Number Title Priority Date Filing Date
CN201710515367.0A Active CN107309832B (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device

Family Applications After (2)

Application Number Title Priority Date Filing Date
CN201810563641.6A Withdrawn CN108818383A (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device
CN201810563612.XA Withdrawn CN108818382A (en) 2017-06-29 2017-06-29 A kind of low torsion multiple purpose aeroplane electrification wrench device

Country Status (1)

Country Link
CN (4) CN107309832B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE542281C2 (en) * 2018-07-12 2020-03-31 Atlas Copco Ind Technique Ab Power tool attachment part

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2101562U (en) * 1991-09-08 1992-04-15 卢晓锋 Electric quick wrench
US6374710B2 (en) * 1999-12-29 2002-04-23 Teng-Tang Kuo Universal cavity pit wrench
CN204248750U (en) * 2014-11-24 2015-04-08 武汉钢铁(集团)公司 Flexible handle sleeve spanner
CN205380606U (en) * 2016-02-24 2016-07-13 崔维群 Electric power overhauls uses portable spanner
CN106425959B (en) * 2016-12-16 2018-09-21 诸暨天雅科技有限公司 Round universal spanner
CN106737332B (en) * 2016-12-16 2018-08-14 李彩琴 Profile spanner

Also Published As

Publication number Publication date
CN107309832A (en) 2017-11-03
CN108818383A (en) 2018-11-16
CN108818382A (en) 2018-11-16
CN107309832B (en) 2018-07-10

Similar Documents

Publication Publication Date Title
CN207983230U (en) A kind of shared sleeve of screw bolt and nut
US20160067849A1 (en) Apparatus for tightening threaded fasteners
CN107571183B (en) Bolt screwing device
CN103029086A (en) Multi-nut fixed torque mounting device
CN111601682A (en) Zero-distance tool
CN108818380A (en) A kind of low torsion multiple purpose aeroplane electrification wrench device
DE202020103844U1 (en) Side turning key
CN109396324A (en) A kind of device and method for chain disassembly
CN107234578B (en) A kind of low torsion multiple purpose aeroplane electrification wrench device
CN112658665A (en) Self-adaptive electric sleeve for robot and robot
CN209638196U (en) Facilitate the bolt of taking-up after a kind of stripped thread
CN107081704B (en) A kind of low torsion multiple purpose aeroplane electrification wrench device
US5083358A (en) Method of preventing twisted-off bolt head while tightening a bolt
CN202402750U (en) Portable valve opening device
CN203635968U (en) Double-edge adjustable boring cutter bidirectional adjusting and compressing structure
CN102284711B (en) Automatic limiting device of hexagonal nut
CN206123509U (en) Spanner and pneumatic wrench
CN206527709U (en) A kind of variable-angle installs auxiliary fixture
CN109159059B (en) Labor-saving socket wrench
CN202192266U (en) Automatic material limiting device for hexagon nut
CN213106591U (en) Electric screwdriver tightening head and electric screwdriver component
CN111015563B (en) Socket spanner
CN219768159U (en) Nut installation auxiliary tool for narrow space
CN214186939U (en) Adjustable spanner
CN220613822U (en) Dual-purpose wrench

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WW01 Invention patent application withdrawn after publication

Application publication date: 20181116

WW01 Invention patent application withdrawn after publication