CN203427346U - Barrel installation structure of oil press - Google Patents

Barrel installation structure of oil press Download PDF

Info

Publication number
CN203427346U
CN203427346U CN201320515052.3U CN201320515052U CN203427346U CN 203427346 U CN203427346 U CN 203427346U CN 201320515052 U CN201320515052 U CN 201320515052U CN 203427346 U CN203427346 U CN 203427346U
Authority
CN
China
Prior art keywords
thorax
lock
button
fuselage
oil press
Prior art date
Application number
CN201320515052.3U
Other languages
Chinese (zh)
Inventor
赵明华
Original Assignee
赵明华
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 赵明华 filed Critical 赵明华
Priority to CN201320515052.3U priority Critical patent/CN203427346U/en
Application granted granted Critical
Publication of CN203427346U publication Critical patent/CN203427346U/en

Links

Abstract

The utility model relates to the technical field of oil presses, in particular to a barrel installation structure of the oil press. The barrel installation structure comprises a machine body, a barrel locking component, an unlocking control piece and a barrel, wherein the barrel locking component is connected with the machine body, a positioning piece is arranged at the rear end of the barrel and fixed to and matched with the barrel locking component, the machine body and the unlocking control piece, the unlocking control piece is a button, and a reset spring is arranged between the button and the machine body. The barrel of the oil press can be conveniently detached only by holding down the button, and labor is saved.

Description

The squeezing thorax mounting structure of oil press
Technical field
The utility model relates to the squeezing thorax mounting structure of Domestic oil press technical field, particularly oil press.
Background technology
The squeezing thorax of existing Domestic oil press is generally fixed by the squeezing thorax locking component snapping with fuselage, and after squeezing thorax is fixing, the squeezing bar that is positioned at squeezing thorax also coordinates with the driving mechanism of fuselage simultaneously.Squeezing thorax locking component is provided with release and controls part, by controlling release, controls part, can realize the dismounting of squeezing thorax.But, because existing squeezing thorax locking component generally forms by being fixed on the deck in fuselage and rotating the cutting ferrule being arranged on outside deck, it is the driving lever being arranged on outside cutting ferrule that part is controlled in release, squeeze thorax the inner and be provided with chuck, chuck needs to pull driving lever after inserting, could realize and squeeze the fixing of thorax, operation is trouble comparatively; And driving lever takes up room many, affect product-forming, can not meet customer requirement.
Utility model content
The purpose of this utility model is to overcome the deficiency that above-mentioned prior art exists, and provides a kind of simple and reasonable for structure, is convenient to the squeezing thorax mounting structure that the oil press of thorax is squeezed in dismounting, to overcome the deficiencies in the prior art.
The purpose of this utility model is achieved in that
A kind of squeezing thorax mounting structure of oil press, comprise fuselage, squeeze thorax locking component, part is controlled in release and squeeze thorax, squeezing thorax locking component is connected with fuselage, squeezing thorax rear end is provided with keeper and squeezes thorax locking component, fuselage and release and control part secure fit, it is characterized in that: it is button that part is controlled in described release, between button and fuselage, is provided with back-moving spring.
The purpose of this utility model can also adopt following technical measures to solve:
As a kind of scheme more specifically, described squeezing thorax locking component comprises lock tube and lock pin, and lock pin interts on lock tube wall, and stretch out outside lock tube button one end, and the button other end and lock pin are in transmission connection; The keeper that squeezes thorax rear end is positioning sleeve, and the corresponding lock pin of positioning sleeve is provided with locating hole.
Between described lock pin bottom and fuselage, be also provided with back-moving spring.
Described lock pin top outer is provided with lead-in chamfered.
In described lock tube, be non-circular week, squeeze positioning sleeve and the interior all form fit of lock tube of thorax rear end.
As another kind of scheme more specifically, described squeezing thorax locking component comprises draw-in groove and lock dog, and draw-in groove is arranged on fuselage surface, and lock dog is slidably arranged in draw-in groove, and button is connected with lock dog through fuselage; The keeper that squeezes thorax rear end is positioning chuck, and positioning chuck inserts in draw-in groove and rotates snapping with draw-in groove.
Described lock dog and button are one-body molded.
The beneficial effects of the utility model are as follows:
(1) when the squeezing thorax of this kind of oil press is dismantled, only need to pin button can carry out disassembling section to squeezing thorax, extremely convenient, laborsaving.
Accompanying drawing explanation
Fig. 1 is the utility model one embodiment decomposition texture schematic diagram.
Fig. 2 is a cross-sectional view after Fig. 1 assembles.
Fig. 3 is A place structure for amplifying schematic diagram in Fig. 2.
Fig. 4 is the B-B sectional structure schematic diagram of Fig. 3.
Fig. 5 is another embodiment decomposition texture schematic diagram of the utility model.
Fig. 6 is local part decomposition texture schematic diagram in Fig. 5.
The specific embodiment
Below in conjunction with drawings and Examples, the utility model is further described.
Embodiment mono-, referring to shown in Fig. 1 to Fig. 4, a kind of squeezing thorax mounting structure of oil press, comprise fuselage 1, squeeze thorax locking component, part is controlled in release and squeeze thorax 6, squeezing thorax locking component is connected with fuselage 1, squeeze thorax 6 rear ends and be provided with keeper and squeeze thorax locking component, fuselage 1 and release and control part secure fit, it is button 4 that part is controlled in described release, between button 4 and fuselage 1, is provided with back-moving spring 8.
Described squeezing thorax locking component comprises lock tube 2 and lock pin 7, and lock pin 7 interts on lock tube 2 walls, and stretch out outside lock tube 2 button 4 one end, and button 4 other ends and lock pin 7 are in transmission connection; The keeper that squeezes thorax 6 rear ends is positioning sleeve 5, and the corresponding lock pin 7 of positioning sleeve 5 is provided with locating hole 51.
Between described lock pin 7 bottoms and fuselage 1, be also provided with back-moving spring 8.
Described lock pin 7 top outer are provided with lead-in chamfered 71.
The interior all ovalizes of described lock tube 2 (can be also the non-circular of other shape), squeeze the positioning sleeve 61 and the interior all form fit of lock tube 2 of thorax 6 rear ends.
It squeezes thorax 6 dismounting principles: take original state as shown in Fig. 1, squeezing thorax 6 does not install, by putting positive squeezing thorax 6 rear ends, insert in lock tube 2, squeezing the positioning sleeve 5 of thorax 6 rear ends and the lead-in chamfered 71 of lock pin 7 contacts, impel lock pin 7 to move and avoid positioning sleeve 5, simultaneously, back-moving spring 8 is compressed, button 4 is also being followed lock pin 7 and is being moved, when positioning sleeve 5 is inserted into appropriate location, the locating hole 51 of positioning sleeve 5 is aimed at lock pin 7, lock pin 7 resets under back-moving spring 8 effects, and insert in locating hole 51, positioning sleeve 5 is linked together by lock pin 7 with lock tube 2, cause squeezing thorax can not shift out outside fuselage 1, realize the installation of squeezing thorax, as shown in Figure 2.When needs are extracted squeezing thorax 6, press the button 4, button 4 leaves the locating hole 51 that squeezes thorax 6 rear end positioning sleeves 5 with pendulum lock pin 7, make not constraint between positioning sleeve 5 and lock tube 2, can in lock tube 2, extract squeezing thorax 6, and the dismounting of thorax is squeezed in realization.
Embodiment bis-, are, with the difference of embodiment mono-shown in Fig. 5 and Fig. 6, described squeezing thorax locking component comprises draw-in groove 11 and lock dog 41, draw-in groove 11 is arranged on fuselage 1 surface above, and lock dog 41 is slidably arranged in draw-in groove 11, and button 4 is connected with lock dog 41 through fuselage 1; The keeper that squeezes thorax 6 rear ends is positioning chuck 61, and positioning chuck 61 inserts in draw-in groove 11 and rotates snappings with draw-in groove 11.
Described lock dog 41 and draw-in groove 11 are one-body molded.
It squeezes thorax 6 dismounting principles: take original state as shown in Fig. 5, squeezing thorax 6 does not install, the positioning chuck 61 that squeezes thorax 6 rear ends is aimed to the draw-in groove 11 of fuselage 1, positioning chuck 61 inserts in draw-in groove 11, then pin button 4, lock dog 41 is moved toward fuselage 1 internal direction, thereby avoid positioning chuck 61, now back-moving spring 8 is in compressive state; Then, direction rotation squeezes thorax 6 in accordance with regulations, positioning chuck 61 is along with squeezing thorax 6 rotations and fastening with draw-in groove 11 gradually, after both fasten completely, release button 4, lock dog 41 and button move and are stopping positioning chuck 61 toward fuselage 1 outside direction under back-moving spring 8 effects, thereby avoid positioning chuck 61 upsets, make to squeeze thorax 6 and connect reliable.When needs are extracted squeezing thorax 6, press the button 4, button 4 drives lock dogs 41, and lock dog 41 no longer stops positioning chuck 61, now, can, squeezing thorax 6 counter-rotation, until positioning chuck 61 no longer fastens with draw-in groove 11, detachably squeeze thorax.

Claims (7)

1. the squeezing thorax mounting structure of an oil press, comprise fuselage, squeeze thorax locking component, part is controlled in release and squeeze thorax, squeezing thorax locking component is connected with fuselage, squeezing thorax rear end is provided with keeper and squeezes thorax locking component, fuselage and release and control part secure fit, it is characterized in that: it is button that part is controlled in described release, between button and fuselage, is provided with back-moving spring.
2. the squeezing thorax mounting structure of oil press according to claim 1, is characterized in that: described squeezing thorax locking component comprises lock tube and lock pin, and lock pin interts on lock tube wall, and stretch out outside lock tube button one end, and the button other end and lock pin are in transmission connection; The keeper that squeezes thorax rear end is positioning sleeve, and the corresponding lock pin of positioning sleeve is provided with locating hole.
3. the squeezing thorax mounting structure of oil press according to claim 2, is characterized in that: between described lock pin bottom and fuselage, be also provided with back-moving spring.
4. the squeezing thorax mounting structure of oil press according to claim 2, is characterized in that: described lock pin top outer is provided with lead-in chamfered.
5. the squeezing thorax mounting structure of oil press according to claim 2, is characterized in that: in described lock tube, is non-circular week, squeezes the positioning sleeve and the interior all form fit of lock tube of thorax rear end.
6. the squeezing thorax mounting structure of oil press according to claim 1, is characterized in that: described squeezing thorax locking component comprises draw-in groove and lock dog, and draw-in groove is arranged on fuselage surface, and lock dog is slidably arranged in draw-in groove, and button is connected with lock dog through fuselage; The keeper that squeezes thorax rear end is positioning chuck, and positioning chuck inserts in draw-in groove and rotates snapping with draw-in groove.
7. the squeezing thorax mounting structure of oil press according to claim 6, is characterized in that: described lock dog and button are one-body molded.
CN201320515052.3U 2013-08-22 2013-08-22 Barrel installation structure of oil press CN203427346U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320515052.3U CN203427346U (en) 2013-08-22 2013-08-22 Barrel installation structure of oil press

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320515052.3U CN203427346U (en) 2013-08-22 2013-08-22 Barrel installation structure of oil press

Publications (1)

Publication Number Publication Date
CN203427346U true CN203427346U (en) 2014-02-12

Family

ID=50056405

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320515052.3U CN203427346U (en) 2013-08-22 2013-08-22 Barrel installation structure of oil press

Country Status (1)

Country Link
CN (1) CN203427346U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104260398A (en) * 2014-07-24 2015-01-07 寇建华 Household oil press
CN104401026A (en) * 2014-11-30 2015-03-11 李军安 Press barrel mounting structure for oil press
CN108340615A (en) * 2017-12-15 2018-07-31 深圳建溢宝电子有限公司 A kind of oil press of quick despatch press chamber press chamber

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104260398A (en) * 2014-07-24 2015-01-07 寇建华 Household oil press
CN104401026A (en) * 2014-11-30 2015-03-11 李军安 Press barrel mounting structure for oil press
CN108340615A (en) * 2017-12-15 2018-07-31 深圳建溢宝电子有限公司 A kind of oil press of quick despatch press chamber press chamber
CN108340615B (en) * 2017-12-15 2019-12-10 深圳建溢宝电子有限公司 Oil press capable of quickly assembling and disassembling barrel and pressing rod

Similar Documents

Publication Publication Date Title
CN204271392U (en) Connector modules fixed frame
CN104209404A (en) Rotary extrusion secondary forming die for novel pipe fitting for decoration and forming method thereof
CN202402425U (en) Spring type locking device
CN107244486B (en) A kind of open air logistics storage bin equipment
CN203092475U (en) Fast-disassembling and fast-assembling tool for internal combustion engine cylinder sleeve
CN202972274U (en) Pipeline clamp
CN202498771U (en) Mould locking mechanism
CN202697961U (en) Self-locking type zipper puller
CN204184184U (en) Battery box catch gear and Battery case and battery box
CN202100564U (en) Fastener for furniture
CN201546444U (en) Scaffold fastening and connecting hook
CN103835348B (en) Drain plug interlock apparatus
JP2007290107A (en) Extracting device for positioning pin
CN102667032A (en) Multi-point lock with translating bolt
CN205544077U (en) Novel electric hidden box
CN208519037U (en) A kind of force arm type dual spring lock pin
CN103626114A (en) Semiautomatic device for sleeving quilt core into quilt cover
CN202251312U (en) Pin shaft end fixing device
CN102989909A (en) Riveting die of upper cover
CN203495537U (en) Extraction tool for hole punching male die or hole punching female die
WO2018036159A1 (en) Tool for mounting tappet body
CN104533913A (en) Telescopic locking device
CN201394807Y (en) Socket wrench
CN203114861U (en) Transmission shaft for forced feeder of tablet press
CN203241263U (en) Soil sampler

Legal Events

Date Code Title Description
GR01 Patent grant
C14 Grant of patent or utility model
ASS Succession or assignment of patent right

Owner name: ANHUI BEILING ANTELOPE ELECTRIC CO., LTD.

Free format text: FORMER OWNER: ZHAO MINGHUA

Effective date: 20140929

TR01 Transfer of patent right

Effective date of registration: 20140929

Address after: 242100 Langxi Economic Development Zone, Xuancheng, Anhui

Patentee after: Anhui North antelope Electric Appliance Co., Ltd.

Address before: 266100 No. 1 Haier Road, Laoshan District, Shandong, Qingdao

Patentee before: Zhao Minghua

C41 Transfer of patent application or patent right or utility model
COR Change of bibliographic data

Free format text: CORRECT: ADDRESS; FROM: 266100 QINGDAO, SHANDONG PROVINCE TO: 242100 XUANCHENG, ANHUI PROVINCE

RINS Preservation of patent right or utility model and its discharge
PP01 Preservation of patent right

Effective date of registration: 20150608

Granted publication date: 20140212

RINS Preservation of patent right or utility model and its discharge
PD01 Discharge of preservation of patent

Date of cancellation: 20151208

Granted publication date: 20140212

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140212

Termination date: 20150822

EXPY Termination of patent right or utility model