CN201385321Y

CN201385321Y - Shearing tool

Info

Publication number: CN201385321Y
Application number: CN 200920006161
Authority: CN
Inventors: 张士松; 李祥庆; 霍立祥
Original assignee: Positec Power Tools Suzhou Co Ltd
Current assignee: Positec Power Tools Suzhou Co Ltd
Priority date: 2009-03-09
Filing date: 2009-03-09
Publication date: 2010-01-20
Anticipated expiration: 2019-03-09

Abstract

The utility model relates to a shearing tool, which is detachably connected with a hand-held power tool. The hand-held power tool comprises a head capsule (12) and an output shaft (13) which extends out of the head capsule (12) and provided with an axial lead X. The output shaft (13) can perform rotating swing around the axial lead X; and the shearing tool comprises a fixed blade (4) and a movable blade (5), wherein the movable blade (5) is connected with the output shaft (13), the fixed blade (4) is connected with the head capsule (12), and the movable blade (5) can perform rotating swing around the axial lead X relative to the fixed blade (4). The shearing tool can be detachably arranged on the hand-held power tool, in particular to a multifunctional machine as an accessory, and thereby, the application range of the multifunctional machine is expanded. Since the movable blade connected with the output shaft performs the swing motion, compared with the prior electrical shear, the shearing tool has simpler structure and more convenient use.

Description

Shearing tool

Technical field

The utility model relates to a kind of annex of hand-hold power tool, especially a kind of annex of swinging the class power tool, more particularly a kind of shearing tool of using on swing class power tool.

Background technology

Multi Role Aircraft is the common swing class power tool of industry, because its output shaft is done rotational oscillating motion around axial line, therefore, after different annex working heads is being installed on the output shaft, can realize multiple different operating function, as sawing, cut, grind, scrape etc., to adapt to different work requirements.

Shearing also is one of common operational means, common shearing manipulation is realized by scissors class instrument, such scissors comprises two blades, and adopt pivotally connected between these two blades, one end of two blades is equipped with cutting edge, and cutting edge is and is oppositely arranged, and the other end then is an operating portion.When the user struts two blades relatively, can realize the action of opening of shearing, and after the user closes up two blades, can realize the closed action sheared again, so go round and begin again, can realize the shear action of scissors to workpiece.

Certainly, industry common electric shear adopts is another cut mode, in two blade, have one to be ledger-plate usually, another is a cutting blade with respect to ledger-plate then.Cutting blade is connected with power transmission shaft, can produce reciprocating motion under the effect of motor, and ledger-plate then is maintained fixed motionless.Thus, by the reciprocating motion of cutting blade, realize the shear action of scissors.

Also do not have shearing tool on the Multi Role Aircraft at present, be necessary to develop a shearing-type cutter in fact, with the range of application of expansion Multi Role Aircraft.

The utility model content

The purpose of this utility model is to provide a kind of shearing tool, as the annex of Multi Role Aircraft, and its dismountable being installed on the swing class power tool, with the range of application of expansion Multi Role Aircraft.

For achieving the above object, the utility model provides a kind of shearing tool, dismountable being connected on a kind of hand-hold power tool, described hand-hold power tool comprises head capsule and extended output shaft with axial line X in the head capsule, described output shaft can be done rotary oscillation around described axial line X, described shearing tool comprises ledger-plate and cutting blade, wherein, cutting blade produces with output shaft and is connected, ledger-plate produces with head capsule and is connected, and cutting blade can be done rotary oscillation around axial line X with respect to ledger-plate.

As improvement to such scheme:

Described shearing tool also comprises Connection Block and terminal pad, and wherein, Connection Block is connected with ledger-plate with head capsule simultaneously, and terminal pad is connected with cutting blade with output shaft simultaneously.

Described Connection Block comprise the sidewall that is circular and by sidewall around the reception room that forms, described terminal pad is arranged in the reception room, and also is provided with bearing between Connection Block and terminal pad, and makes terminal pad produce motion with respect to Connection Block.

The outside extension of the sidewall of described Connection Block is provided with several screws, and a baffle plate is fixedly connected on the sidewall by screw.

The outside of the sidewall of described Connection Block is also extended and is provided with first boss, and first boss is provided with first installing hole, and described ledger-plate is fixedly connected on first boss by screw.

Described terminal pad has two faces, and wherein the one side towards output shaft is formed with groove, and the another side of output shaft is provided with connecting hole dorsad, and is provided with positioning convex between connecting hole.

On the described cutting blade, corresponding connecting hole is provided with perforation, and corresponding positioning convex is provided with locating hole, and described cutting blade is fixedly connected on the terminal pad by screw.

Described ledger-plate is trapezoidal, comprise connecting portion and cutting edge, and cutting edge is positioned on the hypotenuse of trapezium structure, described cutting blade is L-shaped, comprises two free ends, and one of them free end is a connecting portion, and another free end is with respect to the trapezium structure of ledger-plate, form inverted trapezium structure, what its cutting edge was same is formed on the trapezoidal hypotenuse, and described cutting edge is staggered contacting.

Described shearing tool also comprises bracing frame, comprises connecting portion and the gripper shoe of extending perpendicular to connecting portion, extends at the side of gripper shoe to be provided with a projection, and described projection closely contacts with the back side of ledger-plate.

The utility model also provides a kind of shearing tool, comprise two blades, between described two blades by indirect the connecting as one of bearing, and make one of them blade can produce motion with respect to another blade, and described two blades can being connected on the power tool or from described power tool of while be dismantled.

Shearing tool in the utility model, dismountable being installed on the Multi Role Aircraft used the range of application of having expanded Multi Role Aircraft as annex.And, do rotational oscillating motion owing to connect the cutting blade of output shaft, with respect to existing electric shear, structure is more simple, uses also more convenient.

Description of drawings

Fig. 1 is in the preferred embodiment of the present utility model, adopts the stereogram of the Multi Role Aircraft of shearing tool, and the Multi Role Aircraft in the diagram is that side direction is used.

Fig. 2 is the stereogram of the head capsule of the Multi Role Aircraft of connection shearing tool.

Fig. 3 a is the stereogram (front) of shearing tool.

Fig. 3 b is the stereogram (back side) of shearing tool.

Fig. 4 is the three-dimensional explosive view of shearing tool.

Fig. 5 a is that shearing tool is connected the front view on the Multi Role Aircraft.

Fig. 5 b is that shearing tool is connected the cross section view on the Multi Role Aircraft.

Fig. 6 a is the user mode reference diagram of shearing tool, and at this moment, cutting blade moves the position in left side as shown in the figure with respect to ledger-plate.

Fig. 6 b is the user mode reference diagram of shearing tool, and at this moment, cutting blade does not produce mobile with respect to ledger-plate.

Fig. 6 c is the user mode reference diagram of shearing tool, and at this moment, cutting blade moves the position on right side as shown in the figure with respect to ledger-plate.

Related elements reference numeral in the diagram is as follows:

1, shearing tool 2, Connection Block 3, terminal pad

4, ledger-plate 5, cutting blade 6, bracing frame

10, Multi Role Aircraft 11, casing 12, head capsule

13, output shaft 14, cable 21, sidewall

22, reception room 23, screw 24, baffle plate

25, first boss 26, first installing hole 27, second boss

28, second installing hole 30, bearing 31, groove

32, connecting hole 33, locating hole 41, connecting portion

42, cutting edge 51, connecting portion 52, perforation

53, locating hole 54, cutting edge 55, through hole

61, connecting portion 62, gripper shoe 63, projection

The specific embodiment

The utility model is described in further detail below in conjunction with drawings and the specific embodiments.

See also Fig. 1 to Fig. 2, the utility model has disclosed a kind of shearing tool 1 that is applied on the Multi Role Aircraft, goes for shearing manipulation.This Multi Role Aircraft is appointed as label 10, the head capsule 12 that it comprises tubular casing 11 and is connected casing 11 front ends, head capsule 12 self is 90 ° of angles and is provided with, and wherein extends output shaft 13 (as shown in Figure 2), the free end of this output shaft 13 is regular hexagon, and has axial line X.In the casing 11 of this Multi Role Aircraft 10, be provided with the motor that driving force is provided and the transmission component of driving torque, be connected with cable 14, be used for providing electric power to motor at the end of casing 11.After motor was connected and produced driving force, the moment of torsion of this driving force was passed to output shaft 13 through transmission component.Under the effect of this moment of torsion, output shaft 13 is done rotational oscillating motion around axial line X, shown in the double-head arrow A-A direction among Fig. 1.

Need to prove, here the Multi Role Aircraft that the Multi Role Aircraft 10 that is adopted is used always for industry, Multi Role Aircraft is to use the power tool that the swing principle is taken exercises, owing to itself be not the utility model point place that the utility model is created, no longer do too much description for the concrete structure applicant of Multi Role Aircraft 10.

See also Fig. 3 to Fig. 4, shearing tool 1 is the additional element that is connected on the head capsule 12, belongs to dismountable annex that is connected on the head capsule 12.This shearing tool 1 comprises Connection Block 2, be arranged on the terminal pad 3 of Connection Block 2 inside, be connected ledger-plate 4 on the Connection Block 2, be connected the cutting blade 5 and the bracing frame 6 that connect on the attic base 3.Wherein, it is cylindric that Connection Block 2 roughly is, comprise the sidewall 21 that is circular and by sidewall 21 around the reception room 22 that forms, when Connection Block 2 was connected on the head capsule 12 of Multi Role Aircraft 10, the end of head capsule 12 was housed in the reception room 22.Simultaneously, the output shaft 13 of Multi Role Aircraft 10 also is positioned at reception room 22.In the outside of sidewall 21, the position extension that is 90 ° of angles at interval is provided with three screws 23 and one first boss 25, and these three screws 23 are used for fixing and connect a baffle plate 24 with sealing support and connection dish 3.First boss 25 is provided with first installing hole 26, is used for screw and connects ledger-plate 4 and bracing frame 6.And with first boss 25 position at 90 ° of angles at interval, that also extends in the outside of sidewall 21 is provided with second boss 27, and second boss 27 is provided with second installing hole 28, is used for Connection Block 2 is fixedly connected on the head capsule 12 of Multi Role Aircraft 10.

Corresponding output shaft 13, terminal pad 3 is arranged on the inside of Connection Block 2, promptly in the reception room 22, and also is provided with bearing 30 between sidewall 21 and terminal pad 3, thereby terminal pad 3 can be rotated with respect to sidewall 21.One side towards output shaft 13 on the terminal pad 3 is provided with groove 31 (shown in Fig. 2 a), and in the present embodiment, the free end of groove 31 corresponding output shafts 13 also is a regular hexagon, thereby can make output shaft 13 lucky being inserted in this groove 31.Be provided with two connecting holes 32 at the another side of terminal pad 3, and between two connecting holes 32, be provided with equally two positioning convex 33 with respect to groove 31 symmetries with respect to groove 31 symmetries.In a preferred embodiment, such connecting hole 32 and positioning convex 33 all are set to two, and interruption-like layout.Certainly, in the utility model, their quantity is not done concrete qualification.

Please continue to consult Fig. 4, ledger-plate 4 is fixedly connected on by screw on first boss 25 on the sidewall 21 of Connection Block 2, and this ledger-plate 4 roughly is trapezoidal, comprises connecting portion 41 and cutting edge 42, and cutting edge 42 is positioned on the hypotenuse of trapezium structure.In addition, this ledger-plate 4 is made of flexible material, can produce the bending of definite shape.

Cutting blade 5 is roughly L-shaped, comprises two free ends, and one of them free end forms connecting portion 51, and the connecting hole 32 on its corresponding terminal pad 3 is provided with perforation 52, and corresponding positioning convex 33 is provided with locating hole 53.When cutting blade 5 is fixedly mounted on the terminal pad 3, be inserted in the locating hole 53 by positioning convex 33 and position, then pass perforation 52 by screw, cutting blade 5 is fixedly connected on the terminal pad 3.Another free end of this cutting blade 5 is with respect to the trapezium structure of ledger-plate 4, form inverted trapezium structure, its cutting edge 54 same being formed on the trapezoidal hypotenuse, thus the cutting edge 42 of ledger-plate 4 and the cutting edge 54 of cutting blade 5 are staggered contacting.Because connecting the terminal pad 3 of cutting blade 5 can rotate with respect to Connection Block 2, so, cutting blade 5 also can rotate with respect to the ledger-plate 4 that is connected on the Connection Block 2, can conversion between the opening and closing two states thereby make between cutting edge 42 and the cutting edge 54, realize shear action.

In addition, at the middle part of cutting blade 5, the middle part of L shaped structure just, first boss 25 on the corresponding Connection Block 2 is provided with through hole 55, its purpose is after ledger-plate 4 is installed on first boss 25, because screw can produce certain height, hinders the motion of cutting blade 5.Therefore, through hole 55 is set on cutting blade 5, the screw that installs and fixes ledger-plate 4 is housed in this through hole 55, thereby avoid it to influence the rotation of cutting blade 5.

See also Fig. 5, bracing frame 6 is to be fixedly connected on first boss 25 in sidewall 21 outsides of Connection Block 2 by screw equally, this bracing frame 6 is roughly L-shaped, comprise the connecting portion 61 that is connected with first boss 25 and perpendicular to the gripper shoe 62 of connecting portion 61, side extension in gripper shoe 62 is provided with a projection 63, this projection 63 closely contacts with the back side of ledger-plate 4, again because ledger-plate 4 is to adopt flexible material to constitute, thereby ledger-plate 4 always can be promoted towards cutting blade 5, to keep ledger-plate 4 cutting blade 5 of always fitting, guarantee the effect of shearing.

In addition, gripper shoe 62 can be used as support and is placed on and desires to carry out to be user-friendly on the workbench surface of shearing manipulation.

The specific structural features of shearing tool of the present utility model as previously mentioned.See also Fig. 6, be the operation principle schematic diagram of this shearing tool.Shown in Fig. 6 b, when Multi Role Aircraft 10 does not start, output shaft 13 is not done oscillating motion, thereby, the terminal pad 3 that connects output shaft 13 is not done oscillating motion equally, the cutting blade 5 that is connected on the terminal pad 3 remains on initial position, the position when promptly cutting blade 5 as shown in FIG. and the cutting edge angle between the ledger-plate 4 are 45 °.

Shown in Fig. 6 a, when output shaft 13 drive terminal pads 3 are done clockwise swing, cutting blade 5 will be the center of circle with axial line X, left direction swing in diagram, its cutting edge 54 produces with respect to ledger-plate 4 and moves, thereby, make the cutting edge angle between the two be extended to 47 °, constitute the operation of opening in the shearing motion.

And for example shown in Fig. 6 c, when output shaft 13 generations are swung in the other direction, be that output shaft 13 is when driving terminal pads 3 and doing counter-clockwise swing, cutting blade 5 will be the center of circle with axial line X, right direction swing in diagram, its cutting edge 54 produce with respect to ledger-plate 4 and move down, thereby, make the cutting edge angle between the two be contracted to 43 °, constitute the closed procedure in the shearing motion.

Certainly, the angle here only is in order to be beneficial to the clearly sign that explanation is taked, and is exactly to adopt such angle setting but be not defined in, and it can also be other angles that realize shear action.

Along with the reciprocally swinging of output shaft 13, it drives terminal pad 3 and also does reciprocally swinging, therefore, is connected the swing of cutting blade 5 within above-mentioned angular range on the terminal pad 3, goes round and begins again, and realizes shear action.

It should be noted that, because the ledger-plate 4 of this shearing tool 1 is connected on the Connection Block 2, simultaneously, Connection Block 2 itself is again to be fixedly coupled on the head capsule 12 of Multi Role Aircraft 10, therefore, in the process of shear action, ledger-plate 4 is to keep motionless always, and only cutting blade 5 is to produce swing with respect to ledger-plate 4.

Shearing tool disclosed in the utility model is an additional accessory of Multi Role Aircraft, and the swing in high frequency by Multi Role Aircraft provides can realize shear action, thereby provides the more applications direction for Multi Role Aircraft.

Claims

1, a kind of shearing tool, dismountable being connected on a kind of hand-hold power tool, described hand-hold power tool comprises head capsule (12) and extended output shaft (13) with axial line X in the head capsule (12), described output shaft (13) can be done rotary oscillation around described axial line X, it is characterized in that: described shearing tool comprises ledger-plate (4) and cutting blade (5), wherein, cutting blade (5) produces with output shaft (13) and is connected, ledger-plate (4) produces with head capsule (12) and is connected, and cutting blade (5) can be done rotary oscillation around axial line X with respect to ledger-plate (4).

2, shearing tool as claimed in claim 1, it is characterized in that: described shearing tool also comprises Connection Block (2) and terminal pad (3), wherein, Connection Block (2) is connected with ledger-plate (4) with head capsule (12) simultaneously, and terminal pad (3) is connected with cutting blade (5) with output shaft (13) simultaneously.

3, shearing tool as claimed in claim 2, it is characterized in that: described Connection Block (2) comprise the sidewall (21) that is circular and by sidewall (21) around the reception room (22) that forms, described terminal pad (3) is arranged in the reception room (22), and between Connection Block (2) and terminal pad (3), also be provided with bearing (30), and make terminal pad (3) produce motion with respect to Connection Block (2).

4, shearing tool as claimed in claim 3 is characterized in that: the outside extension of the sidewall (21) of described Connection Block (2) is provided with several screws (23), and a baffle plate (24) is fixedly connected on the sidewall (21) by screw.

5, shearing tool as claimed in claim 4, it is characterized in that: the outside of the sidewall (21) of described Connection Block (2) is also extended and is provided with first boss (25), first boss (25) is provided with first installing hole (26), and described ledger-plate (4) is fixedly connected on first boss (25) by screw.

6, shearing tool as claimed in claim 5, it is characterized in that: described terminal pad (3) has two faces, wherein the one side towards output shaft (13) is formed with groove (31), and the another side of output shaft (13) is provided with connecting hole (32) dorsad, and is positioned at and is provided with positioning convex (33) between the connecting hole (32).

7, shearing tool as claimed in claim 6, it is characterized in that: on the described cutting blade (5), corresponding connecting hole (32) is provided with perforation (52), and corresponding positioning convex (33) is provided with locating hole (53), and described cutting blade (5) is fixedly connected on the terminal pad (3) by screw.

8, shearing tool as claimed in claim 1, it is characterized in that: described ledger-plate (4) is trapezoidal, comprise connecting portion (41) and cutting edge (42), and cutting edge (42) is positioned on the hypotenuse of trapezium structure, described cutting blade (5) is L-shaped, comprise two free ends, one of them free end is connecting portion (51), and another free end is with respect to the trapezium structure of ledger-plate (4), form inverted trapezium structure, what its cutting edge (54) was same is formed on the trapezoidal hypotenuse, and described cutting edge (42,54) is staggered contacting.

9, shearing tool as claimed in claim 1, it is characterized in that: described shearing tool also comprises bracing frame (6), comprise connecting portion (61) and the gripper shoe (62) of extending perpendicular to connecting portion (61), side extension in gripper shoe (62) is provided with a projection (63), and described projection (63) closely contacts with the back side of ledger-plate (4).

10, a kind of shearing tool, comprise two blades, it is characterized in that: between described two blades by indirect the connecting as one of bearing (30), and make one of them blade can produce motion with respect to another blade, and described two blades can being connected on the power tool or from described power tool of while be dismantled.