CN201483083U - reciprocating saw - Google Patents

reciprocating saw Download PDF

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Publication number
CN201483083U
CN201483083U CN2009201774324U CN200920177432U CN201483083U CN 201483083 U CN201483083 U CN 201483083U CN 2009201774324 U CN2009201774324 U CN 2009201774324U CN 200920177432 U CN200920177432 U CN 200920177432U CN 201483083 U CN201483083 U CN 201483083U
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CN
China
Prior art keywords
clamping element
support member
clamping
fuselage
reciprocating
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Expired - Fee Related
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CN2009201774324U
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Chinese (zh)
Inventor
于英林
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.)
Positec Power Tools Suzhou Co Ltd
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Positec Power Tools Suzhou Co Ltd
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Priority to CN2009201774324U priority Critical patent/CN201483083U/en
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Publication of CN201483083U publication Critical patent/CN201483083U/en
Anticipated expiration legal-status Critical
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Abstract

The utility model relates to a reciprocating saw, which comprises a body, a motor, a saw blade, a supporting piece, a connecting piece, a clamping device and an adjusting piece, wherein the motor is installed in the body; the saw blade is driven by the motor and does reciprocating movement relative to the body; the supporting piece leans against a supporting surface; the connecting piece connects the supporting piece and the body; the clamping piece is connected with the connecting piece and can operationally move to clamp the supporting piece relative to the body; and the adjusting piece drives the clamping piece to move in the clamping direction of the clamping piece to clamp the supporting piece. The utility model is characterized in that a clutch mechanism is arranged between the adjusting piece and the clamping piece, the clutch mechanism is provided with a preset critical toque, and the adjusting piece cannot drive the clamping piece to move in the clamping direction when the toque required for the movement of the clamping piece in the clamping direction reaches the critical torque. The utility model has the advantages that only one independent adjusting piece is required to realize the adjustment of the supporting piece, and the adjustment can be complete in one step and is convenient and fast.

Description

Reciprocating-type saw
Technical field
The utility model relates to a kind of reciprocating-type saw.Particularly relate to a kind of reciprocating-type saw with support member adjustment structure.
Background technology
In the prior art, reciprocating-type saw, especially the support member of sweep-saw has an arcuate part that makes progress, and long and narrow through hole is arranged at its top, has corresponding arch depression on sweep-saw fuselage and the face that support member matches, the through hole that bolt passes the support member arcuate part is connected on the fixed block or nut that is fixed in the fuselage, thereby realizes fixedlying connected of support member and fuselage.When needs are regulated the gradient of support member or front and back position, need unclamp bolt, after being adjusted to the position that needs, support member tights a bolt again.Tightening in the prior art or unclamp bolt often need be by bottle opener, and instruments such as spanner are realized, complicated operation.
Therefore, prior art has disclosed a kind of improved sweep-saw support member fast adjuster, and it is connected support member on the fuselage by bolt equally.Yet it also has a quick change spanner, the fixedly connected cam ring of quick change spanner, also be provided with a circumferentially fixing cam bit on the fuselage, the cam surface separately of cam bit and cam ring matches mutually, when needs are regulated the gradient of support member, need pull spanner the male and female face of cam ring and cam bit is fitted mutually, unclamp support member, pull spanner once more after support member is adjusted to the position that needs, make the convex surface of cam ring and cam bit and convex surface connect clamp supports.This kind support member fast adjuster need can not realized the support member adjusting by extra instrument, yet, in use, friction between the cam surface can cause cam ring and cam bit to wear and tear gradually, and finally causing can't clamp supports only according to the cooperation between the cam surface, in order to address this problem, a thumb wheel is provided in the prior art in addition, thumb wheel is mounted on nut or the fixed block in the fuselage, to regulate bolt, cooperates the camming clamping or unclamps support member.Such design makes number of elements increase, complex structure, and realize that support member regulates often needing to operate two adjusting devices, comparatively loaded down with trivial details.
The utility model content
The purpose of this utility model is to provide a kind of reciprocating-type saw, and it has the support member governor motion, and this support member governor motion can not cause clamping not tight because of the wearing and tearing of clamping part, and only depends on a regulating part to finish the operation of support member governor motion.
The utility model provides a kind of reciprocating-type saw, comprising: fuselage; Be installed on the motor in the fuselage; Driven with respect to the reciprocating saw blade of fuselage by motor; Be resisted against the support member of bearing-surface; The connector that connects described support member and fuselage; Connect described connector, exercisable motion is with the clamping element with respect to the fuselage clamp supports; Driving clamping element moves on the clamping direction of clamping element with the regulating part of clamp supports, it is characterized in that: be provided with clutch between described regulating part and the clamping element, clutch has default critical torque, when clamping element motion required torque on clamping direction reaches described critical torque, regulating part can not drive clamping element and move on clamping direction.
Further, described connector is the axle that vertically is arranged in the coupling part of fuselage and support member, and described clamping element is connected on the described axle, has eccentric part, and the motion of clamping element pivot drive eccentric part is with clamping or unclamp support member.
Further, the bottom of described support member is recessed to form arch portion to the fuselage direction, described axle passes supporting member and extends and arrive in the arch portion, and the part that axle is arranged in arch portion vertically is equipped with bearing pin, and aforesaid regulating part and clamping element are socketed on the bearing pin and adjustablely pivot around bearing pin.
Further, described connector is for vertically being arranged in the axle of the coupling part of fuselage and support member, and described clamping element is socketed on the axle, sway threadably and axle axially on move, with clamping or unclamp support member.
Further, comprise the movable moving cam of relative fuselage, described moving cam connects described axle, have axle axially on high plane and low plane.
Further, comprise the quiet cam that relative fuselage is static, described quiet cam has the high plane and the low plane that match with described moving cam between the bottom of connector and clamping element and in abutting connection with described moving cam, described moving cam be positioned at be fixedly connected on clamping element the bottom to move with clamping element.
Further, described clutch comprises first clutch part of fixedlying connected with described regulating part and second clutch part of fixedlying connected with described clamping element, and oppress first clutch part and second clutch part elastic component close to each other, described first clutch part and second clutch part have relative static with the moment of torsion that transmits regulating part to first state of clamping element and relative activity with the moment of torsion of cut-out regulating part second state to clamping element.
Further, the end face that connects mutually of described first clutch part and second clutch part is the end tooth face, have a plurality of end teeth on it respectively, with the applying each other that matches, described each end tooth week upwards joins end to end and the shape unanimity, have two that the angle of inclination do not wait domatic, each end tooth arbitrary domatic adjacent to the angle of inclination of adjacent end tooth do not wait domatic.
Further, described regulating part one end is connected with described clamping element, and the other end is positioned at fuselage appearance and becomes spanner portion.
Further, the exercisable relative fuselage of described support member is around himself longitudinal axis pivot.
Further, described elastomeric element is a spring.
Further, the eccentric part of described clamping element is socketed on bearing pin in the form of a ring, have the pivot axle center that is parallel to the bearing pin longitudinal axis, the circumference of described eccentric part gradually changes apart from the distance in pivot axle center, has apart from nearer near-end in pivot axle center and the far-end far away apart from the pivot axle center.
Further, the exercisable drive clamping element of described regulating part pivot with optionally make described near-end and far-end one of them axle axially on towards support member, with unclamping or clamp supports of correspondence.
Further, be socketed with pad on the described axle, pad is between bearing pin and support member.
Further, the exercisable drive clamping element of described regulating part is moving to unclamp support member on the direction of clamping direction.
Further, described clamping element is a clamping direction along the direction that described axle moves axially near support member.
Further, described clamping element around described axle pivot the far-end that makes eccentric part axle axially on be clamping direction towards the direction of support member.
Further, described reciprocating-type saw is a sweep-saw.
Further, the end tooth face of described clamping element is positioned on the end face of eccentric part of described ring-type.
Compared with prior art, the beneficial effects of the utility model are: the operator only need regulate clamping and the release that independent spanner portion can realize support member, convenient to operation, the clamping degree high conformity of Shi Yonging repeatedly, the wearing and tearing because of clamping element do not cause clamping not tight.
Description of drawings
Fig. 1 is the overall structure front view of first embodiment of the present utility model.
Fig. 2 is the angular adjustment schematic diagram of first embodiment of the present utility model.
Fig. 3 is the three-dimensional exploded view of first embodiment of the present utility model.
Fig. 4 is the three-dimensional exploded view of second embodiment of the present utility model.
Fig. 5 is the stereogram of the regulating part of second embodiment of the present utility model.
Fig. 6 is the support member governor motion schematic diagram of second embodiment of the present utility model.
1 reciprocating-type saw, 6 quiet cams, 501 holes
2 saw blades, 7 clamping elements, 503 flat quadrate parts
3 support members, 72 second clutch parts, 505 ends
31 through holes, 73 moving cams, 590 bearing pins
33 arch portions, 77 grooves, 70 clamping elements
4 fuselages, 8 regulating parts, 720 end tooth faces
41 underframe, 81 adjusting portions, 80 regulating parts
43 arch portions, 83 spanner portions, 810 adjusting portions
45 through holes, 85 first clutch parts, 820 end tooth faces
59 stage clip 830 spanner portions
51 pads, 10 packing rings, 90 springs
53 main parts, 11 card Figure 100 packing rings
50 110 collars in 55 ends
The specific embodiment
Fig. 1 is the overall schematic of first embodiment of the present utility model.As shown in Figure 1, reciprocating-type saw 1 is a kind of hand held electric tool, is specially a kind of sweep-saw, yet it can be reciprocating saw or other similar reciprocating-type saws equally.Reciprocating-type saw 1 comprises fuselage 4 and saw blade 2, be provided with a motor (figure does not show) in the fuselage 4, motor rotatablely moves to a transmission mechanism (figure does not show) output, this transmission mechanism will rotatablely move and be converted into reciprocating motion, to drive saw blade 2 straight reciprocating motions or to move back and forth, carry out cutting function along track.And reciprocating-type saw 1 is during cutting operation, normally is placed on to use on the workpiece.Reciprocating-type saw 1 also comprises an adjustable support member 3, this support member 3 is connected in the underframe of fuselage 4, so that along bearing-surface (as a workpiece or a relevant guide member) guiding reciprocating-type saw 1, and, during carrying out cutting operation, support member 3 is used to support reciprocating-type saw 1.Support member 3 can pivot with respect to fuselage 4 around himself longitudinal axis.In order to regulate support members 3 with respect to fuselage 4, support member 3 can be clamped and be unclamped.As shown in Figure 2, this adjusting allows the user to select the desired angle of saw blade 2 with respect to the surface of the work (not shown) of 3 joints of support member during cutting operation.
Fig. 3 is the three-dimensional exploded view of support member governor motion of the present utility model.As shown in Figure 3, fuselage 4 has one and is used for the underframe 41 that engages with support member 3, and underframe 41 has to the projecting inward arch portion 43 of fuselage 4, and this arch portion 43 has a through hole 45.Accordingly, support member 3 has an arch portion 33 that protrudes to fuselage 4 directions, and this arch portion 33 has a long and narrow through hole 31 of arranging along the bending direction of arch.The degree of crook of arch portion 33 and arch portion 43 is roughly suitable, shape matches, and can fitting tightly, and the extension angle of arch portion 33 is greater than the extension angle of arch portion 43, can allowing support member 3 to pivot, and fit tightly all the time with fuselage 4 around the relative fuselage 4 of self longitudinal axis.
A connector is specially an axle 5 with screw thread, passes the through hole 31 of aforesaid arch portion 33 and the through hole 45 of arch portion 43 successively, extends to the inside of fuselage 4.The form of connector can have multiple, as, have the axle of teeth groove, perhaps and support member 3 be combined as a whole etc.Axle 5 has less shaft-like main part 53 of diameter and the bigger end 55 of diameter.Also has a pad 51 between the arch portion 33 of end 55 and support member 3.A clamping element 7 is specially nut, and the inside and the axle that are positioned at fuselage 45 match, and the underframe 41 and the support member 3 of fuselage 4 is clamped between the end 55 of clamping element 7 and axle 5, and its clamping degree of tightness can be regulated.When clamping was loose, support member 3 can pivot with adjusting angle; When clamping was tight, support member 3 was fixed on a specific angle, and aforesaid long and narrow through hole 41 allows support member 3 can pivot in certain angular range when axle 5 passes.
The support member governor motion of first embodiment of the present utility model has the coarse adjustment of clamping tightness and two kinds of adjustment structures of fine tuning.Coarse adjustment structure and fine tuning structure are to operate by an independent regulating part, move simultaneously to reach a kind of quick and easy, the operating experience that settles at one go.The convenience of be describing, below the fine tuning structure of the clamping tightness of support member is described earlier.
As Fig. 3, a regulating part 8 is provided with in abutting connection with described clamping element 7, and regulating part 8 comprises an adjusting portion 81 and a spanner portion 83, and adjusting portion 81 is set on the nut 7, spanner portion 83 extends to fuselage 4 outsides, for the clamping tightness of operator's operation with the adjusting support member.Be provided with a cover clutch between regulating part 8 and the nut 7.Concrete, clutch comprises first clutch part 85 and second clutch part 72, first clutch part 85 is fixedly connected on the adjusting portion 81 of regulating part 8, first clutch part 85 has the axial end flank of tooth of annular, has end to end a plurality of end tooth on the end tooth face, each end tooth shape unanimity, have respectively two that the angle of inclination do not wait domatic, and each end tooth arbitrary domatic adjacent to the angle of inclination of adjacent end tooth do not wait domatic.Second clutch part 72 is fixedly connected on the clamping element 7, the annular section that formation is outwards extended along diametric(al) from the bottom of the main part of clamping element 7, this annular section has the axial end flank of tooth, relative and the shape of the longitudinal end flank of tooth of the longitudinal end flank of tooth of second clutch part 72 and first clutch part 85 matches, fitting tightly each other.The opposite side relative with annular section is provided with the groove 77 of a ring-type on the clamping element 7, and a collar 11 is installed on the groove 77, is equipped with packing ring 10 between collar 11 and the ring part successively, elastic component 9, the adjusting portion 81 of regulating part 8.Like this, elastic component 9 is specially a stage clip, oppresses first clutch part 85 and second clutch part 72 closely against each other.
The fine tuning structure that is provided with as above-mentioned mode has reached meticulous adjusting clamping element 7, and the effect of the clamping tightness of volitional check maximum.When operator's rotary spanner portion 83, the adjusting portion 81 and first clutch part 85 are followed rotation, by thereon the end tooth and the end tooth interlock of second clutch part 72, and then drive second clutch 72 and clamping element 7 is followed rotation.Because two longitudinal end flank of tooth are fit together by elastic component 9 compressings, keep the critical torque of fitting so have, the size of critical torque is by the inclined degree and the coefficient of friction acting in conjunction decision of the coefficient of elasticity of elastic component 9 and stressed end tooth.When the moment of torsion that bears during greater than critical torque, first clutch part 85 will go round and begin again along the inclined plane of end tooth with respect to 72 rotations of second clutch part and overcome and move on the pressure of elastic component 9 and then pressurized falls, promptly begin to climb repeatedly.Again because the inclination angle, inclined plane that end tooth rises along clockwise direction is not equal to the inclination angle that descends along clockwise direction, so degree of tightness regulating part 8 right handed critical torques are not equal to the critical torque of rotation counterclockwise.Definition degree of tightness regulating part 8 clockwise rotating to be are rotated in the forward, and it is close to each other to be rotated in the forward the end 55 that drives clamping element 7 and axle 5; Definition regulating part 8 is anticlockwise to rotate to be reverse rotation, and the end 55 that reverse rotation drives clamping element 7 and axle 5 away from each other.In the present embodiment, the critical torque that setting is rotated in the forward is less than the critical torque of reverse rotation, and, the critical torque that is rotated in the forward is the default critical torque of clutch of the present utility model, the default critical torque of this clutch set corresponding to corresponding to default support member clamping tightness, promptly, when the elasticity of support member 3 and underframe 4 during less than a default support member clamping tightness, the operator can operate spanner portion 83 and be rotated in the forward, clamping element 7 is near the bottom 55 of axle 5, the clamping tightness is increased, up to reaching default support member clamping tightness, after this order about the required moment of torsion of clamping element 7 rotations once more greater than the critical torque that is rotated in the forward, the foregoing climbing of first clutch part, 85 beginnings no longer drives clamping element 7 rotations.Because the critical torque of reverse rotation is greater than the critical torque that is rotated in the forward, after reaching the maximum grip tightness, the operator can drive 83 reverse rotations of spanner portion, unclamps support member 3.In the present embodiment, clamping element 7 is motion on the clamping direction in the motion on the axial direction of axle 5, and it causes support member clamped.
The key point that it may be noted that the support member clamping tightness of realizing that restriction is default is a clutch is set between degree of tightness regulating part 8 and clamping element 7, and that the specific embodiment of clutch can have is multiple.As, this programme is provided with axial end tooth, however it also is attainable on the side face that axle 5 and clamping element 7 cooperate end tooth being set radially.For another example, the clutch of this programme cooperates by the end tooth face to be realized, yet the clutch that steel ball cooperates with chute also is attainable.The average personnel in this area design easily and are different from the clutch of scheme as previously mentioned.
The coarse adjustment structure of the clamping tightness of support member 6 is described below.
As Fig. 3, the coarse adjustment structure comprises one with respect to the movable moving cam 73 of fuselage, also comprises a quiet cam 6 static with respect to fuselage.Moving cam 73 is fixedly connected on the clamping element 7, rotates along with the rotation of clamping element 7.High plane and low plane on moving cam 73 has axially.Quiet cam 6 is arranged in the groove in the fuselage 4, high plane and low plane on having axially, and the high plane of shape and moving cam 73 and low plane match so that each contented high-order face during in the face of the other side's low plane mutual gapless against.When clamping element 7 drives moving cams 73 rotations, the high plane of moving cam 73 is during in the face of the high plane of quiet cam 6, the clamping degree fast rise of support member 3.When clamping element 7 drives moving cams 73 rotations, the high plane of moving cam 73 is during in the face of the low plane of quiet cam 6, and the clamping degree of support member 3 descends fast.This be because the movable length variations between clamping element 7 and axle 5 the bottom 55 one section particular length, this segment length equals the high plane of moving cam 73 haply and the distance of low plane adds the high plane of quiet cam 6 and the distance of low plane, because the variable in distance that this moment, axle 5 rotations caused is less relatively.
Foregoing, the fine tuning structure and the coarse adjustment structure of support member 3 tightness are combinations.Loose at support member 3, the low plane separately of quiet cam 6 and moving cam 73 is in the face of the other side's high plane, when needing to clamp, the operator operates spanner portion 83 and is rotated in the forward, adjusting portion 81 at first drives nut 7 rotations by clutch, make the high plane of quiet cam 6 and moving cam 73 abut against each other, this moment, support member 3 was clamped fast, yet may also not reach default support member clamping tightness, the operator can operate spanner portion 83 and continued to be rotated in the forward this moment, up to reaching default support member clamping tightness, clutch begins climbing.Support member 3 clamps, and in the time of need unclamping, process is opposite with the process of clamping, the operator operates 83 reverse rotations of spanner portion, and nut 5 unclamps a segment distance, and the high plane of quiet then cam 6 and moving cam 73 is separated from each other, low plane separately is in the face of the other side's high plane, and support member 3 is released.
In the process that clamps repeatedly and unclamp of support member 3, the high plane of moving cam 73 and quiet cam 6 can produce wearing and tearing, the clamping effect that reaches by camming will reduce like this, yet much more slightly this can be rotated in the forward the wear extent that a segment distance compensates camming by spanner portion 83.This has prolonged the service life of support member regulating system.
Below in conjunction with Fig. 4, Fig. 5, Fig. 6 second embodiment of the present utility model is described.
Fig. 4 is the three-dimensional exploded view of second embodiment of the present utility model.As Fig. 4, second embodiment has same fuselage 4 and support member 3.Also have connector, be specially axle 50, pass the through hole on fuselage 4 and the support member 3, extend to support member 3 the bottom a and pass pad 51.After axle 50 assembles, be positioned at pad 51 times, the part in a of support member 3 bottoms is provided with the hole 501 perpendicular to the axial direction of axle 50, and bearing pin 590 passes hole 501, perpendicular to axle 50.Be socketed with regulating part 80 of the present utility model on the bearing pin 590, clamping element 70 and clutch therebetween.Be regulating part, clamping element and clutch therebetween all are contained in a of support member 3 bottoms.
Specifically describe the support member governor motion of second embodiment in conjunction with Fig. 4, Fig. 5, Fig. 6, a flat quadrate part 503 is formed at the bottom of axle 50, the end of bearing pin 590 is greater than the diameter in hole 501, be positioned at the right side of flat quadrate part 503, the axial region of bearing pin 590 passes the opposite side that hole 501 extends across flat quadrate part, its end is provided with draw-in groove and the collar 110 that matches, and with aforesaid regulating part 80, clamping element 70 and clutch therebetween are arranged at the left side of flat quadrate part 503.Be provided with packing ring 100 successively, spring 90, regulating part 80, clamping element 70 between the flat quadrate part 503 of collar 110 and axle 50.As figure, the same with the regulating part 8 of first embodiment, regulating part 80 comprises an adjusting portion 810 and a spanner portion 830.Adjusting portion 810 is suitable for the person's of being operated operation to regulate clamping element 70.Clamping element 70 is specially an eccentric wheel, and it has apart from its axis of rotation far-end far away and nearer near-end, and from the near-end to the far-end, eccentric radius gradually changes.Like this, during clamping element 70 rotation, if its far-end butt pad 51, then oppress support member 3 and fuselage 4 is close to each other with clamp supports, if its near-end butt pad 51 then unclamps support member 3 and fuselage 4, to unclamp support member 3.Similar first embodiment, be provided with clutch between clamping element 70 and the regulating part 80, be specially: adjusting portion 810 and clamping element 70 end face of butt joint mutually are the end tooth face 820 and the end tooth face 720 of interworking, and they have continuous fluctuating and the end to end a plurality of end teeth of ring-type separately.Spring 90 1 ends are resisted against on the packing ring 100, and an end is resisted against on the adjusting portion 810, and the pressure side flank of tooth 820 and end tooth face 720 are close to each other.Same, the clamp mechanism among second embodiment has default critical torque.
The mechanism of the support member governor motion of second embodiment as described below.When needs are regulated the angle of support member 3, spanner portion 830 is pulled around bearing pin 590 pivots from default clamped position, at this moment, because the end tooth face 820 of the spring 90 compressing adjusting portions 810 in the clutch and the end tooth face 720 of clamping element 70 are close to each other, regulating part 80 drives clamping element 70 and pivots around bearing pin 590, the far-end of clamping element 70 leaves pad 51 gradually, unclamps support member 3.After the angle that regulates support member 3, oppositely pull spanner portion 830, by the clutch effect, drive clamping element 70 and pivot, make its far-end near pad 51, clamp supports 3.Clamping degree at support member 3 reaches preset value, make the clutch effect, after driving the required default critical torque of moment of torsion of clamping element 70 further clampings greater than clutch, the moment of torsion that clutch no longer transmits regulating part 80 is to the clamping section 70, the climbing that the end tooth face 720 of the end tooth face 820 of the adjusting portion 810 that matches and clamping element 70 of being specially begins to go round and begin again, adjusting portion 810 overcomes the compressing of spring 90, clamping element 70 leaves in axial direction court along bearing pin 590, end tooth face 820 and 720 disengagings of end tooth face are meshing with each other, after crossing a lattice end tooth, end tooth face 820 and end tooth face 720 are engaged with each other under spring 90 compressings once more, so go round and begin again.Return to default clamped position up to spanner portion 830.In the present embodiment, the far-end that causes eccentric part of clamping element 70 is a clamping direction against the pivotal orientation of pad 51, and it causes support member 3 clamped.
As previously mentioned, in a second embodiment, the near-end of clamping element 70 gradually changes and rises to far-end, under initial state, clamping element 70 does not need the far-end of its radius maximum against pad 51, and certain position that only needs certain radius in the far-end promptly can reach clamping against pad 51, and then regulating part 80 and spanner portion 830 thereof reach default clamped position by the climbing action of clutch.Longer when service time, clamping element 70 wearing and tearing, after the position radius of original certain radius reduced in the far-end, regulating part 80 still drives clamping element 70 to be continued to rotate up to the new position with this certain radius against pad 51.Like this, the radius that has reached distal-most end up to the degree of wear of clamping element 70 is reduced to the degree of this certain radius, the support member governor motion still is operable, this has prolonged the service life of support member governor motion greatly, and, it is that clamping is reliable and stable through the optimal value of calculating and test draws (being the clamping degree of the predetermined torque correspondence of clutch) all the time that the support member of support member governor motion clamps degree.
In the utility model, in the process that clamps repeatedly and unclamp of support member 3, the operator only need operate independent spanner portion, just can reach support member 3 clampings that settle at one go and the effect of unclamping, simple and fast.

Claims (10)

1. a reciprocating-type saw comprises: fuselage (4); Be installed on the motor in the fuselage; Driven with respect to the reciprocating saw blade of fuselage (2) by motor; Be resisted against the support member (3) of bearing-surface; The connector that connects described support member and fuselage; Connect described connector, exercisable motion is with the clamping element with respect to the fuselage clamp supports; Driving clamping element moves on the clamping direction of clamping element with the regulating part of clamp supports, it is characterized in that: be provided with clutch between described regulating part and the clamping element, clutch has default critical torque, when clamping element motion required torque on clamping direction reaches described critical torque, regulating part can not drive clamping element and move on clamping direction.
2. reciprocating-type saw according to claim 1, it is characterized in that: described connector is for vertically being arranged in the axle of the coupling part of fuselage and support member, described clamping element is connected on the described axle, has eccentric part, and the motion of clamping element pivot drive eccentric part is with clamping or unclamp support member.
3. reciprocating-type saw according to claim 2, it is characterized in that: the bottom of described support member is recessed to form arch portion to the fuselage direction, described axle passes supporting member and extends in the arrival arch portion, the part that axle is arranged in arch portion vertically is equipped with bearing pin, and aforesaid regulating part and clamping element are socketed on the bearing pin and adjustablely pivot around bearing pin.
4. reciprocating-type saw according to claim 1, it is characterized in that: described connector is for vertically wearing the axle of the coupling part of sub-body and support member, described clamping element is socketed on the axle, sway threadably and axle axially on move, to clamp or to unclamp support member.
5. reciprocating-type saw according to claim 4 is characterized in that: comprise the movable moving cam of relative fuselage (73), described moving cam connects described axle, have axle axially on high plane and low plane.
6. reciprocating-type saw according to claim 5, it is characterized in that: comprise the quiet cam (6) that relative fuselage is static, described quiet cam is between the bottom of connector and clamping element and in abutting connection with described moving cam, have the high plane and the low plane that match with described moving cam, described moving cam be positioned at be fixedly connected on clamping element the bottom to move with clamping element.
7. reciprocating-type saw according to claim 1, it is characterized in that: described clutch comprises first clutch part (85) of fixedlying connected with described regulating part and second clutch part (72) of fixedlying connected with described clamping element, and oppress first clutch part and second clutch part elastic component (9) close to each other, described first clutch part and second clutch part have relative static with the moment of torsion that transmits regulating part to first state of clamping element and relative activity with the moment of torsion of cut-out regulating part second state to clamping element.
8. reciprocating-type saw according to claim 8, it is characterized in that: the end face that connects mutually of described first clutch part and second clutch part is the end tooth face, have a plurality of end teeth on it respectively, with the applying each other that matches, described each end tooth week upwards joins end to end and the shape unanimity, have two that the angle of inclination do not wait domatic, each end tooth arbitrary domatic adjacent to the angle of inclination of adjacent end tooth do not wait domatic.
9. reciprocating-type saw according to claim 1 is characterized in that: described regulating part one end is connected with described clamping element, and the other end is positioned at fuselage appearance. spanner portion (83).
10. reciprocating-type saw according to claim 1 is characterized in that: the exercisable relative fuselage of described support member is around himself longitudinal axis pivot.
CN2009201774324U 2009-08-31 2009-08-31 reciprocating saw Expired - Fee Related CN201483083U (en)

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CN2009201774324U CN201483083U (en) 2009-08-31 2009-08-31 reciprocating saw

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CN2009201774324U Expired - Fee Related CN201483083U (en) 2009-08-31 2009-08-31 reciprocating saw

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102000879B (en) * 2009-08-31 2012-10-03 苏州宝时得电动工具有限公司 Reciprocating saw

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102000879B (en) * 2009-08-31 2012-10-03 苏州宝时得电动工具有限公司 Reciprocating saw

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