CN209153299U - A kind of agitator for food-making fuselage postposition push type new line interlocking structure - Google Patents

Abstract

The utility model relates to agitator for food-making technical fields, refer in particular to a kind of agitator for food-making fuselage postposition push type new line interlocking structure, agitator for food-making includes the fuselage and pedestal that rear side is rotatably coupled by shaft, there is locking piece in fuselage, fuselage is stretched out in side behind the slave of locking piece one end, the locking piece other end is equipped with hook portion, is rotatably installed in fuselage on locking piece by the first pin shaft；Pedestal forward position is equipped with lock hole, and hook portion passes through lock hole and is hooked on pedestal；There is supporting element in fuselage, supporting element one end is rotatably installed in fuselage by the second pin shaft, and the supporting element other end is connected with driving spring, and driving spring provides supporting element the elastic force for making the other end of supporting element to rotation on front side of fuselage.The postposition push type new line interlocking structure of the utility model, by release button design on rear side of fuselage, user only needs the singlehanded operation of lifting that can carry out fuselage, more convenient to use, while interlocking structure is simple and reliable, and cost is lower.

Description

A kind of agitator for food-making fuselage postposition push type new line interlocking structure

Technical field

The utility model relates to agitator for food-making technical fields, refer in particular to a kind of agitator for food-making fuselage postposition push type lift Head interlocking structure.

Background technique

Currently, commonly the foods such as veterinary antibiotics, beans are stirred with the food processor packet of processing in people's life Base and fuselage are included, the fuselage is connect with base back end activity, in use process, is needed to open on fuselage and is lifted and could will stir It mixes container and is taken in and out base, fuselage is whether located at lifting position, or positioned at the position cooperated with base, fuselage and machine It is required to be located at lock state between seat, is able to satisfy fuselage just using safety requirements from unintentional rotation.Such as Chinese patent public affairs A kind of food processor that the number of opening is mentioned for CN201658271U, including base and fuselage, the fuselage and base back end activity Connection, base one side corresponding with fuselage is respectively equipped with pneumatically or hydraulically spring, have telescopic rod be movably connected in this two Between a pneumatically or hydraulically spring, it is equipped with button positioned at the another side of base, which connects flexible self-locking card Button, the fuselage are equipped with self-locking buckle corresponding with the self-locking buckle of elasticity；Program middle fuselage and base in mated condition, Fuselage is locked on base by elasticity self-locking buckle between them, when fuselage is located at lifting status, fuselage and base it Between connection locking realized by pneumatically or hydraulically spring, while the release button of the self-locking buckle of elasticity is being located at the front of pedestal just Face in use, can only be by the hand steered shape fuselage of another when a hand operates release button, and operating process is not convenient enough, And using the connection type of pneumatically or hydraulically spring, lead to the higher cost of product, it is necessary to be further improved.

Utility model content

The purpose of this utility model is to propose a kind of agitator for food-making fuselage postposition push type new line interlocking structure, will be discharged For push-button design on rear side of fuselage, user only needs the singlehanded operation of lifting that can carry out fuselage, more convenient to use, together When interlocking structure it is simple and reliable, cost is lower.

In order to achieve the above object, the technical solution adopted in the utility model is as follows: a kind of agitator for food-making fuselage postposition Push type new line interlocking structure, the agitator for food-making include fuselage and pedestal, and the rear side of the fuselage and the rear side of pedestal are logical It crosses shaft to be rotatably coupled, which is characterized in that be equipped with locking piece, side behind one end slave of the locking piece in the fuselage The fuselage is stretched out, the other end of the locking piece is equipped with hook portion, and the position between the locking piece both ends passes through the first pin shaft It is rotatably installed in fuselage；Position on the pedestal in front of it is equipped with lock hole, and the hook portion passes through the lock Determine hole and hook on the base；Supporting element is additionally provided in the fuselage, one end of the supporting element can turn by the second pin shaft It is installed in fuselage dynamicly, the other end of the supporting element is connected with driving spring, and the driving spring makes supporting element offer Elastic force of the other end of supporting element to rotation on front side of fuselage.The postposition push type new line interlocking structure of the utility model, will discharge For push-button design on rear side of fuselage, user only needs the singlehanded operation of lifting that can carry out fuselage, more convenient to use, together When interlocking structure it is simple and reliable, cost is lower.

According to above scheme, Lock spring is connected on the locking piece, one end of the Lock spring is connected to locking Close to the position of its hook portion on part, the other end of the Lock spring is connected on fuselage, and the Lock spring applies locking piece Add elastic force so that the hook portion is maintained at the position for hooking the pedestal.Elastic force is provided to locking piece by Lock spring, makes to lock Determine part and can have to remain at the position for hooking pedestal, when fuselage and base engagement, locking piece can be more reliably Positioned at lock state, make to be able to maintain in the engagement condition between fuselage and pedestal in locked state, it will not accidental separation.

According to above scheme, the locking piece has the lock arm of pair of parellel setting, and one end of lock arm, which has, to be stretched out Button release in fuselage rear, the other end of lock arm all have hook portion, pass through one first pin between the both ends of lock arm Axis is rotatably installed in fuselage；Lock hole of the position equipped with pair of parellel setting on the pedestal in front of it, two A hook portion is each passed through two lock holes and hook on the base.Button release is designed on locking piece, and family operation can be used It is more convenient when locking piece, while using a pair of locking arm and a pair of of hook portion, makes locking structure between locking piece and pedestal more Reliably, locking dynamics is bigger, prevents from surprisingly flicking between fuselage and pedestal.

According to above scheme, torsional spring is arranged in the shaft, the torsional spring is sandwiched between pedestal and fuselage, so as to turn round Spring provides around the shaft relative to the elastic force of base rotation fuselage.Elastic force is provided to fuselage by torsional spring, when locking piece and pedestal Between cooperation when being unlocked, fuselage can be lifted up automatically under the effect of the elastic force of torsional spring, not need user's manual overturning Fuselage, it is more convenient when carrying out lifting operation.

According to above scheme, the guide surface of arc, the other end of the supporting element and the guidance are equipped in the pedestal Face is in contact and can slide in guide surface.By the guide surface of arc, limit and guidance can be realized to supporting element, work as fuselage When being in mated condition with pedestal, the other end of supporting element is guided face limit；During fuselage and pedestal are in and lift, branch The other end of support member can be slided along guide surface；When fuselage and pedestal are in platform state, the other end of supporting element skids off guidance It except face, while being stretched out under the effect of the elastic force of driving spring to the front side of fuselage, supporting element is made to be shelved on the upper surface of pedestal On, realize the effect that supporting element is supported by pedestal.The fit structure of guide surface and supporting element makes to prop up in fuselage rotation process Support member can be slided along guide surface more like clockwork, finally realize its support function.

According to above scheme, there is driving plate close to the position of its hook portion on the locking piece, have in the driving plate Sliding groove；One end of the supporting element has slide head, and the slide head is located in sliding groove；The sliding groove is in front-rear direction On size be greater than the size of the slide head in the longitudinal direction, and when the other end of supporting element is to turning on front side of fuselage When position, it is in contact on rear side of the rear side and sliding groove of the slide head.Using the fit structure of slide head and sliding groove, make to lock Part can link with supporting element, it is only necessary to operate locking piece, supporting element can move synchronously, and further simplify the operation of user Process, using just plus convenient.

The postposition push type new line interlocking structure of the utility model, in fuselage and base engagement position, using locking piece This structure of fuselage is hooked to realize locking, locking piece is the multisection type hook formation of special designing, in this way can be by locking piece Release part be designed into the rear side of fuselage, user is when pressure-locking part while can help fuselage, makes user in operation lock One hand can complete operating procedure when determining part；When fuselage and pedestal are in lifting position, supporting element can be in driving spring Drive it is lower stretched out to the front side of fuselage, and be shelved on the upper surface of pedestal, make to be propped up between the front side between fuselage and pedestal Member supports limit, and the rear side between fuselage and pedestal, and the lower end surface on rear side of fuselage can withstand on the upper end surface side on rear side of pedestal Side.Above structure can be realized under lifting status, be locked between fuselage and pedestal, and therefore, the utility model will discharge For push-button design on rear side of fuselage, user only needs the singlehanded operation of lifting that can carry out fuselage, more convenient to use, together When interlocking structure it is simple and reliable, cost is lower.

Detailed description of the invention

Fig. 1 is the locking piece fit structure schematic diagram of the utility model；

Fig. 2 is the supporting element fit structure schematic diagram of the utility model；

Fig. 3 is the lifting status structural schematic diagram of the utility model；

Fig. 4 is the locking piece of the utility model and supporting element is linked structural schematic diagram.

In figure: 1, fuselage；2, pedestal；3, shaft；4, locking piece；5, hook portion；6, the first pin shaft；7, lock hole；8, it supports Part；9, the second pin shaft；10, driving spring；11, Lock spring；12, lock arm；13, button release；14, torsional spring；15, guide surface； 16, driving plate；17, sliding groove；18, slide head.

Specific embodiment

The technical solution of the utility model is illustrated with embodiment with reference to the accompanying drawing.

As depicted in figs. 1 and 2,1 postposition push type of a kind of agitator for food-making fuselage described in the utility model, which comes back, interlocks Structure, the agitator for food-making include fuselage 1 and pedestal 2, and the rear side of the fuselage 1 can be turned with the rear side of pedestal 2 by shaft 3 It connects dynamicly, is equipped with locking piece 4 in the fuselage 1, the fuselage 1, institute are stretched out in one end of the locking piece 4 on rear side of fuselage 1 The other end for stating locking piece 4 is equipped with hook portion 5, and the position between 4 both ends of locking piece is rotatably mounted by the first pin shaft 6 In in fuselage 1；Position on the pedestal 2 in front of it is equipped with lock hole 7, and the hook portion 5 passes through the lock hole 7 and hook On the pedestal 2；Supporting element 8 is additionally provided in the fuselage 1, one end of the supporting element 8 passes through the second pin shaft 9 rotationally It is installed in fuselage 1, the other end of the supporting element 8 is connected with driving spring 10, and the driving spring 10 mentions supporting element 8 For making the other end of supporting element 8 to the elastic force rotated on front side of fuselage 1.The postposition push type new line interlocking structure of the utility model, In fuselage 1 and 2 cooperation position of pedestal, this structure of fuselage 1 is hooked using locking piece 4 to realize locking, locking piece 4 is special The release part of locking piece 4, can be designed into the rear side of fuselage 1 by the multisection type hook formation of design in this way, and user is pressing Fuselage 1 can be helped simultaneously when locking piece 4, makes user's one hand when operating locking piece 4 that can complete operating procedure；In fuselage 1 when be in lifting position with pedestal 2, and supporting element 8 and can be shelved under the driving of driving spring 10 to the stretching of the front side of fuselage 1 On the upper surface of pedestal 2, make to be supported 8 support limit of part between the front side between fuselage 1 and pedestal 2, and fuselage 1 and pedestal The lower end surface of rear side between 2,1 rear side of fuselage can withstand on the upper surface side of 2 rear side of pedestal.Above structure can be realized It under lifting status, is locked between fuselage 1 and pedestal 2, therefore, the utility model designs release button in 1 rear side of fuselage, uses Family only needs the singlehanded operation of lifting that can carry out fuselage 1, more convenient to use, while interlocking structure is simple and reliable, Cost is lower.

As shown in Figure 1, being connected with Lock spring 11 on the locking piece 4, one end of the Lock spring 11 is connected to lock Determine the position on part 4 close to its hook portion 5, the other end of the Lock spring 11 is connected on fuselage 1, the Lock spring 11 Elastic force is applied to locking piece 4 so that the hook portion 5 is maintained at the position for hooking the pedestal 2.It is locked by 11 Duis of Lock spring Part 4 provides elastic force, and locking piece 4 is allow to have the position for remaining at and hooking pedestal 2, when fuselage 1 and the cooperation of pedestal 2, Locking piece 4 can more reliably be located at lock state, make to be able to maintain in the engagement condition between fuselage 1 and pedestal 2 and locked Fixed state, will not accidental separation.

As shown in figure 4, the locking piece 4 has the lock arm 12 of pair of parellel setting, one end of lock arm 12, which has, stretches For the button release 13 at 1 rear of fuselage, the other end of lock arm 12 all has hook portion 5, passes through between the both ends of lock arm 12 One the first pin shaft 6 is rotatably installed in fuselage 1；Position on the pedestal 2 in front of it is set equipped with pair of parellel The lock hole 7 set, two hook portions 5 are each passed through two lock holes 7 and are hooked on the pedestal 2.Release is designed on locking piece 4 Button 13 is more convenient when family operation locking piece 4 can be used, while using a pair of locking arm 12 and a pair of of hook portion 5, making locking piece 4 Locking structure between pedestal 2 is relatively reliable, and locking dynamics is bigger, prevents from surprisingly flicking between fuselage 1 and pedestal 2.

As shown in Fig. 2, being arranged with torsional spring 14 in the shaft 3, the torsional spring 14 is sandwiched between pedestal 2 and fuselage 1, with Torsional spring 14 is set to provide 3 elastic force rotated relative to pedestal 2 around the shaft to fuselage 1.Elastic force is provided to fuselage 1 by torsional spring 14, when When cooperation between locking piece 4 and pedestal 2 is unlocked, fuselage 1 can be lifted up automatically under the effect of the elastic force of torsional spring 14, no The manual tipper body 1 of user is needed, it is more convenient when carrying out lifting operation.

As shown in Fig. 2, being equipped with the guide surface 15 of arc, the other end of the supporting element 8 and the guidance in the pedestal 2 Face 15 is in contact and can slide in guide surface 15.By the guide surface 15 of arc, limit can be realized to supporting element 8 and is drawn It leads, when fuselage 1 is in mated condition with pedestal 2, the other end of supporting element 8 is guided the limit of face 15；When fuselage 1 and pedestal 2 During lifting, the other end of supporting element 8 can be slided along guide surface 15；When fuselage 1 and pedestal 2 are in platform state, The other end of supporting element 8 skids off except guide surface 15, while stretching under the effect of the elastic force of driving spring 10 to the front side of fuselage 1 Out, it is shelved on supporting element 8 on the upper surface of pedestal 2, realizes the effect that supporting element 8 is supported by pedestal 2.Guide surface 15 and support The fit structure of part 8 slides supporting element 8 along guide surface 15 more like clockwork, most in 1 rotation process of fuselage Its support function is realized eventually.

As shown in Figure 1, Figure 2, Figure 3 and Figure 4, there is driving plate 16, institute close to the position of its hook portion 5 on the locking piece 4 Stating has sliding groove 17 in driving plate 16；One end of the supporting element 8 has slide head 18, and the slide head 18 is located at sliding groove In 17；The size of the sliding groove 17 in the longitudinal direction is greater than the size of the slide head 18 in the longitudinal direction, and works as To when rotateing in place on front side of fuselage 1, the rear side of the slide head 18 connects the other end of supporting element 8 with the rear side of sliding groove 17 Touching.Using the fit structure of slide head 18 and sliding groove 17, locking piece 4 and supporting element 8 is set to link, it is only necessary to operate locking piece 4, supporting element 8 can move synchronously, and further simplify the operating process of user, using just plus convenient.

When fuselage 1 and pedestal 2 are in assembled state, as shown in Figure 1, the hook portion 5 of locking piece 4 is by the locking on pedestal 2 Hole 7 is extend into pedestal 2, is hooked in the hook portion 5 of locking piece 4 on pedestal 2, and the front side of fuselage 1 and the front side of pedestal 2 are locked and connected It connects, and the rear side of fuselage 1 is connect with the rear side of pedestal 2 by shaft 3, can realize that fuselage 1 is being assembled with pedestal 2 in this way It is locked under state, is not in the case where fuselage 1 rotates automatically；Meanwhile as shown in Fig. 2, supporting element 8 is located in fuselage 1, though Right driving spring 10 provides elastic force to the other end of supporting element 8, but under the limitation of guide surface 15, and the other end of supporting element 8 is only It can be resisted against in guide surface 15.

When needing to lift on fuselage 1, user only needs one hand to help fuselage 1 and downwards by button release 13, such as Fig. 2 institute Show, at this moment locking piece 4 can be rotated clockwise around the first lock shaft, and hook portion 5 on locking piece 4 can be in lock hole 7 to before fuselage 1 Side is mobile, and hook portion 5 will exit from pedestal 2, no longer hook pedestal 2, will unlock between fuselage 1 and pedestal 2；Fuselage 1 is being turned round Under the elastic force effect of spring 14, deasil can slowly it be lifted relative to the rotation of pedestal 2 around shaft 3 automatically, when the hook of locking piece 4 When portion 5 is exited from lock hole 7, button release 13 can be unclamped.During slowly turntable rises fuselage 1, supporting element 8 The other end is along 15 upward sliding of guide surface；When fuselage 1 is completely in lifting status, as shown in figure 3, under 1 rear side of fuselage End face can be pressed on the upper surface side of 2 rear side of pedestal, prevent fuselage 1 from rotating along clockwise direction relative to pedestal 2 again；This When supporting element 8 the other end just skid off guide surface 15, driving spring 10 pops up the other end of supporting element 8 to front side, makes to prop up The other end bottom surface of support member 8 is shelved on the upper surface of 2 front side of pedestal, fuselage 1 is supported, such fuselage 1 can not be along inverse Clockwise is rotated relative to pedestal 2；When the other end of supporting element 8 is supported on pedestal 2, the upper slide head of supporting element 8 18 are just in contact on rear side of the sliding groove 17 in the driving plate 16 on locking piece 4.Knot is compressed in 2 rear side of fuselage 1 and pedestal Under the 8 dual limitation of support limit structure of supporting element of 1 front side of structure and fuselage, fuselage 1 and pedestal 2 are locked in lifting status.

When needing that fuselage 1 and pedestal 2 are adjusted to assembled state again, user equally can be with one-handed performance downwards by releasing The elastic force turned round to overcome locking elastic is put, locking piece 4 is rotated clockwise, the driving plate 16 on locking piece 4 can be to 1 front side of fuselage It is mobile, since the rear of the sliding groove 17 in driving plate 16 at this time is in contact with the slide head 18 on supporting element 8, driving To when moving on front side of fuselage 1, slide head 18 can be pushed plate 16 by the sliding groove 17 of driving plate 16, and such supporting element 8 can be around the Two pin shafts 9 rotate in the counterclockwise direction, make the other end of supporting element 8 to moving on rear side of fuselage 1, supporting element 8 will be from pedestal 2 Upper surface is backed out, at the same be moved to guide surface 15 cooperate position, between such fuselage 1 and pedestal 2 under lifting status quilt It unlocks；Button release 13 can be unclamped at this time, and fuselage 1 is pushed and pressed to front side in the rear side of fuselage 1, makes 1 gram of fuselage The elastic force for taking torsional spring 14 rotates in the counterclockwise direction around shaft 3, the other end of supporting element 8 slide downward in guide surface 15, When fuselage 1, which is turned to, is in rigging position with pedestal 2, the hook portion 5 of locking piece 4 passes through lock hole 7, as shown in Figure 1, locking piece 4 in the case where the elastic force of Lock spring 11 is pullled, and hook portion 5 is hooked on pedestal 2 to moving after fuselage 1, makes fuselage 1 and pedestal 2 Between be locked in rigging position.

The above description is only a preferred embodiment of the present invention, therefore all according to described in the utility model patent application range The equivalent change or modification done of structure, feature and principle, be included in the scope of the utility model patent application.

Claims (6)

1. a kind of agitator for food-making fuselage postposition push type new line interlocking structure, the agitator for food-making includes fuselage and pedestal, The rear side of the fuselage and the rear side of pedestal are rotatably coupled by shaft, which is characterized in that

Locking piece is equipped in the fuselage, the fuselage is stretched out in side behind one end slave of the locking piece, the locking piece The other end is equipped with hook portion, and the position between the locking piece both ends is rotatably installed in fuselage by the first pin shaft；

Position on the pedestal in front of it is equipped with lock hole, and the hook portion passes through the lock hole and is hooked in the pedestal On；Supporting element is additionally provided in the fuselage, one end of the supporting element is rotatably installed in fuselage by the second pin shaft, institute The other end for stating supporting element is connected with driving spring, and the driving spring makes the other end of supporting element to fuselage supporting element offer The elastic force of front side rotation.

2. agitator for food-making fuselage postposition push type new line interlocking structure according to claim 1, which is characterized in that described Lock spring is connected on locking piece, one end of the Lock spring is connected to the position on locking piece close to its hook portion, described The other end of Lock spring is connected on fuselage, and the Lock spring applies elastic force so that the hook portion is maintained at hook to locking piece State the position of pedestal in residence.

3. agitator for food-making fuselage postposition push type new line interlocking structure according to claim 2, which is characterized in that described Locking piece has the lock arm of pair of parellel setting, and one end of lock arm has the button release for stretching out in fuselage rear, lock arm The other end all have hook portion, be rotatably installed in fuselage by first pin shaft between the both ends of lock arm；Institute The lock hole that the position on pedestal in front of it is equipped with pair of parellel setting is stated, two hook portions are each passed through two lock holes simultaneously Hook is on the base.

4. agitator for food-making fuselage postposition push type new line interlocking structure according to claim 1, which is characterized in that described Torsional spring is arranged in shaft, the torsional spring is sandwiched between pedestal and fuselage so that torsional spring to fuselage provide around the shaft relative to The elastic force of base rotation.

5. agitator for food-making fuselage postposition push type new line interlocking structure according to claim 1, which is characterized in that described The guide surface of arc is equipped in pedestal, the other end of the supporting element is in contact with the guide surface and can slide in guide surface It is dynamic.

6. agitator for food-making fuselage postposition push type new line interlocking structure according to claim 1, which is characterized in that described There is driving plate close to the position of its hook portion on locking piece, there is sliding groove in the driving plate；One end of the supporting element has There is slide head, the slide head is located in sliding groove；The size of the sliding groove in the longitudinal direction is greater than the slide head and exists Size on front-rear direction, and when the other end of supporting element is to when rotateing in place on front side of fuselage, the rear side of the slide head with It is in contact on rear side of sliding groove.