CN101537628A - Razor device - Google Patents

Razor device Download PDF

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Publication number
CN101537628A
CN101537628A CN200910095933A CN200910095933A CN101537628A CN 101537628 A CN101537628 A CN 101537628A CN 200910095933 A CN200910095933 A CN 200910095933A CN 200910095933 A CN200910095933 A CN 200910095933A CN 101537628 A CN101537628 A CN 101537628A
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CN
China
Prior art keywords
razor
carriage
bracing frame
connecting rod
razor device
Prior art date
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Granted
Application number
CN200910095933A
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Chinese (zh)
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CN101537628B (en
Inventor
应平祥
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.)
Zhejiang Superman Polytron Technologies Inc
Original Assignee
CHAOREN GROUP CORP Ltd
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Application filed by CHAOREN GROUP CORP Ltd filed Critical CHAOREN GROUP CORP Ltd
Priority to CN2009100959332A priority Critical patent/CN101537628B/en
Publication of CN101537628A publication Critical patent/CN101537628A/en
Application granted granted Critical
Publication of CN101537628B publication Critical patent/CN101537628B/en
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Abstract

The invention discloses a razor device. A skin stand of the prior razor device only rotates in single direction, thereby extruding skin and being not applicable to faces with serious concave and convex shapes. The razor device comprises a machine body and a bracing rack which is arranged on the machine body, at least two groups of razor units are arranged on the bracing rack, each razor unit comprises an outer cutter and an inner cutter which can be driven to carry out the relative rotation by being close to the outer cutter, a bracket is sleeved at the periphery of each outer cutter, and each bracket can be arranged on the bracing rack by all-round floating relative to the outer cutter and the bracing rack through a connecting rod. As each bracket can carry out the all-round floating relative to the outer cutter and the bracing rack, the bracket is closer to the skin and can play the skin support function with the best state; the outer cutters are closer to the most concave position of the face, thereby leading the cutters to be easy to cut hair at the most concave position, being more applicable to various facial contours, reducing the pressure of the brackets on the face and reducing the pain caused by facial pressure.

Description

Razor device
Technical field
The present invention relates to a kind of razor device of protecting skin, its hair cut speed of bigger performance.
Background technology
Existing No. 95190642.9 patented technology schemes disclose a kind of razor device of skin support, and its technology has been explained its skin support and can be pivoted with respect to carriage with reaching with respect to corresponding outer cut.
The advantage of this technology: because the skin support can be with relatively rotating, the facial shape of can better fitting is brought into play the function that it supports skin.
The shortcoming of this technology:
(1) because this skin support is only made folk prescription to rotation, this pivot position just can not change, and causes pushing skin, and skin can not unfolded.
(2) because this skin support only is pivoted, the facial dark recess of outer cut contact is limited at the pivot position so relatively, can't be fit to the serious face of concaveconvex shape.
Summary of the invention
The technical assignment of the technical problem to be solved in the present invention and proposition is that the skin support that overcomes the prior art existence is only made folk prescription to rotation, cause the defective of pushing skin and can't be fit to the serious face of concaveconvex shape, a kind of new razor device is provided, so that reach the advantage that promptly keeps above-mentioned razor device, overcome the weak point of above-mentioned public technology again, in order to realize this purpose, technical scheme of the present invention is:
Razor device, comprise fuselage and the bracing frame that is installed on the fuselage, have two groups of razor groups on the described bracing frame at least, every group of razor group comprises outer cut and can be driven is pasting the counterrotating inner cutter of outer cut, be with carriage around each outer cut, it is characterized in that: described carriage can be done to be installed on the described bracing frame by connecting rod with respect to described outer cut and bracing frame omni-directionally-floatedly.
Advantage of the present invention is:
1, because the relative outer cut of carriage and bracing frame are done omni-directionally-floatedly, makes carriage more press close to skin, can bring into play its skin support function with the state of the best.
2, because carriage is omni-directionally-floated, make outer cut can more press close to the recess of face, make cutting knife can excise the hair of recess easily, adapt to various face contours more with this.
3, because carriage is omni-directionally-floated, alleviated the pressure of carriage, reduced facial pressure and the pain that produces face.
Description of drawings
Fig. 1: embodiment of the invention rotary shaver part cut-away view;
Fig. 2: rotating shaft distribution map of razor device of the present invention;
Fig. 3: the explosive view of razor device of the present invention;
Fig. 4: razor device connecting rod of the present invention and bracing frame network for location;
Fig. 5: razor device connecting rod of the present invention and bracket arrangement figure;
Fig. 6: the connecting rod boss structure figure of razor device connecting rod of the present invention;
Fig. 7: the layout drawing of razor device carriage interlock of the present invention;
Among the figure: 1-shaver fuselage; The 2-bracing frame; 3-razor group; The 4-carriage; The 5-connecting rod; The 6-inner cutter; The 7-outer cut; Locating slot on the 21-bracing frame; Locating hole on 41~46-carriage; The boss of 51~56-connecting rod; 57-connecting rod positioning boss; 58-elasticity position; The 8-spring; The 7-connecting rod; The boss of 71-connecting rod; A-a/a1-a1/a2-a2-carriage center and the determined axis of the bracing frame line of centres; The determined rotation of boss line of b-b/b1-b1/b2-b2-connecting rod; C-c-carriage moving direction; D-d-shaver fuselage rotation; The 4a/4b/4c-carriage; The 47-bracket boss; The 48-bracket boss; The 49-bracket boss.
The specific embodiment
Basic technical scheme of the present invention is: razor device, comprise fuselage and the bracing frame that is installed on the fuselage, have two groups of razor groups on the described bracing frame at least, every group of razor group comprises outer cut and can be driven is pasting the counterrotating inner cutter of outer cut, be with carriage around each outer cut, it is characterized in that: described carriage can be done to be installed on the described bracing frame by connecting rod with respect to described outer cut and bracing frame omni-directionally-floatedly.
As to further the improving and replenishing of technique scheme, the present invention also comprises the technical characterictic that following each section is additional, so that select for use when stating technical scheme on the implementation:
Carriage is can be installed on the bracing frame around the mode that two orthogonal axis relatively rotate and move up and down respectively.
Carriage with respectively can around two axis that are parallel to each other in relative rotation mode be installed on the bracing frame, these two axis normal that are parallel to each other are in the line of each razor group switching centre.
Carriage is installed on the bracing frame in the mode that moves up and down along the pivot of the razor group of correspondence respectively.
Connecting rod is an elastic component.
The interlaced pad of each carriage is pressed and is joined together to form relative interlock.
Below the present invention is described in detail: Fig. 1 represents an example of razor device of the present invention, this example is a rotary shaver, it comprises fuselage 1 and the bracing frame 2 that is installed on the fuselage 1, three groups of razor groups 3 are arranged on the bracing frame 2, every group of razor group 3 comprises outer cut 7 and can be driven is pasting outer cut 7 counterrotating inner cutters 6, is with carriage 4 around each outer cut 7; It is by fuselage 1 transferring power, make inner cutter 6 paste outer cut 7 rotations, thereby the hair that enters the hair mouth from outer cut is cut, and carriage 4 rotates and moves up and down and realize that the omni-directionally-floated of carriage is the content of most critical in present technique requires with respect to outer cut 7 and bracing frame 2 are relative.
Fig. 3 is explosive view of present embodiment, offer locating slot 21 that links to each other with three connecting rods 5 and three perforates of disposing on the bracing frame 2 with three carriages 4, so that three carriage 4 relative centers and (as shown in Figure 2) is set, each connecting rod all is provided with two boss 52,53,54,55,51,56, with adjacent two carriages 4 by the locating hole on the carriage 41,42,43,44,45,46 interconnect, and the formation Support Position, be to finish present technique to require interior rotation contact point, as shown in Figure 2: wherein the connecting rod boss 51,52 form the b1-b1 rotation, connecting rod boss 53,54 form the b2-b2 rotation, connecting rod boss 55-56 forms the b-b rotation, the connecting rod boss of each connecting rod 5 leaves the gap with the locating hole of the corresponding carriage that is connected 4, clearance control between 0.01mm-0.1mm so that rotation the time does not interfere.
Be provided with connecting rod positioning boss 57 in the middle of 5 liang of connecting rod boss of connecting rod and interconnect, can fix by tight fit mode or riveting or set position mode as Fig. 4 with locating slot 21 on the bracing frame.
The boss bottom of connecting rod 5 is provided with elasticity position 58, realizes moving up and down (as Fig. 5) along the c-c direction independently by the elasticity position 58 of connecting rod 5 to realize carriage 4; Because each boss of each connecting rod 5 can both independently move up and down, and realize that each carriage 4 rotates around carriage center and the determined axis a-a/a1-a1/a2-a2 of the bracing frame line of centres and moves, as shown in Figure 2: described connecting rod 5 suggestions have been adopted polymerization resin (POM, PA elastomeric material) and have been made, and described c-c axis is parallel to shaver fuselage 1 rotation d-d; As shown in Figure 6, the feasible boss by connecting rod of the spring function of each connecting rod 5 carries out resiliency supported to corresponding carriage also can be by directly installing a spring 8 on bracing frame 2, and in spring 8, wear the connecting rod 7 that a upper end of being supported by spring 8 has boss 71 and replace its function, this moment, boss 71 boss that is equivalent to connecting rod of connecting rod 7 cooperated with the corresponding site of carriage 4; Each carriage 4 one end is provided with a boss, the corresponding bracket boss 48 of carriage 4a, the corresponding bracket boss 49 of carriage 4b, the corresponding bracket boss 47 of carriage 4c, wherein carriage 4a pushes down the bracket boss 49 of carriage 4b, carriage 4b pushes down carriage 4c bracket boss 47, and carriage 4c pushes down carriage 4a bracket boss 48, thereby realizes that staggered pad pressure is joined together to form relative interlock (as shown in Figure 7).
Though in above-mentioned example, represented the embodiment of three cutting knife combinations of rotary shaver, razor device of the present invention also can be used at least two above shaver products of cutting knife combination of rotary shaver.
Although by the example of reference diagram the present invention is fully described, but be understood that, those skilled in the art can carry out various variations and remodeling, therefore every under situation about not breaking away from the scope of the invention, the various variations and the remodeling that are carried out all are interpreted as within the scope of the present invention.

Claims (9)

1, razor device, comprise fuselage (1) and be installed in bracing frame (2) on the fuselage (1), have two groups of razor groups (3) on the described bracing frame (2) at least, every group of razor group (3) comprises outer cut (7) and can be driven is pasting the counterrotating inner cutter of outer cut (7) (6), be with carriage (4) around each outer cut (7), it is characterized in that: described carriage (4) can be done to be installed on the described bracing frame (2) by connecting rod (5) with respect to described outer cut (7) and bracing frame (2) omni-directionally-floatedly.
2, razor device according to claim 1 is characterized in that described carriage (4) is can be installed in around the mode that two orthogonal axis relatively rotate and move up and down on the described bracing frame (2) respectively.
3, razor device according to claim 1, it is characterized in that described carriage (4) with respectively can around two axis that are parallel to each other in relative rotation mode be installed on the described bracing frame (2), these two axis normal that are parallel to each other are in the line at described each razor group (3) center.
4, razor device according to claim 1 is characterized in that described carriage (4) is installed on the described bracing frame (2) in the mode that moves up and down along the pivot of the razor group of correspondence respectively.
5, razor device according to claim 1 is characterized in that described connecting rod is an elastic component.
6, razor device according to claim 1 is characterized in that the interlaced pad pressure of each carriage is joined together to form relative interlock.
7, razor device according to claim 1 is characterized in that offering on the bracing frame bracing frame locating slot that links to each other with connecting rod and three perforates of disposing with carriage; The locating hole that each connecting rod all is provided with on two boss and adjacent two carriages interconnects.
8, razor device according to claim 7 is characterized in that leaving between described connecting rod boss and the positioning hole corresponding gap of 0.01mm~0.1mm.
9, razor device according to claim 7 is characterized in that the bottom of described connecting rod boss is provided with the elastic construction of Support bracket.
CN2009100959332A 2009-02-20 2009-02-20 Razor device Active CN101537628B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009100959332A CN101537628B (en) 2009-02-20 2009-02-20 Razor device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009100959332A CN101537628B (en) 2009-02-20 2009-02-20 Razor device

Publications (2)

Publication Number Publication Date
CN101537628A true CN101537628A (en) 2009-09-23
CN101537628B CN101537628B (en) 2012-03-07

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009100959332A Active CN101537628B (en) 2009-02-20 2009-02-20 Razor device

Country Status (1)

Country Link
CN (1) CN101537628B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102669923A (en) * 2012-05-10 2012-09-19 超人集团有限公司 Skin wrinkle curing stretcher
CN103009408A (en) * 2012-12-03 2013-04-03 超人集团有限公司 Floating shaver
CN109877883A (en) * 2019-04-17 2019-06-14 天津须眉科技有限公司 Cutter head floating structure
CN114209423A (en) * 2022-02-21 2022-03-22 吉麦思科技(深圳)有限公司 Skin tendering instrument with laser depilation function

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102669923A (en) * 2012-05-10 2012-09-19 超人集团有限公司 Skin wrinkle curing stretcher
CN102669923B (en) * 2012-05-10 2015-01-21 超人集团有限公司 Skin wrinkle curing stretcher
CN103009408A (en) * 2012-12-03 2013-04-03 超人集团有限公司 Floating shaver
CN109877883A (en) * 2019-04-17 2019-06-14 天津须眉科技有限公司 Cutter head floating structure
CN114209423A (en) * 2022-02-21 2022-03-22 吉麦思科技(深圳)有限公司 Skin tendering instrument with laser depilation function
CN114209423B (en) * 2022-02-21 2022-05-13 吉麦思科技(深圳)有限公司 Skin tendering instrument with laser depilation function

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CN101537628B (en) 2012-03-07

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Effective date of registration: 20160810

Address after: 321300 No. 116 Beihu Road, Yongkang Economic Development Zone, Zhejiang, Jinhua, China

Patentee after: Zhejiang Superman Polytron Technologies Inc

Address before: 321300 hardware science and Technology Industrial Zone, Yongkang, Zhejiang

Patentee before: Chaoren Group Corp., Ltd.