CN201977813U - Guiding structure for body of X-ray machine for mammary glands - Google Patents
Guiding structure for body of X-ray machine for mammary glands Download PDFInfo
- Publication number
- CN201977813U CN201977813U CN2011200408012U CN201120040801U CN201977813U CN 201977813 U CN201977813 U CN 201977813U CN 2011200408012 U CN2011200408012 U CN 2011200408012U CN 201120040801 U CN201120040801 U CN 201120040801U CN 201977813 U CN201977813 U CN 201977813U
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- CN
- China
- Prior art keywords
- guide post
- fuselage
- frame
- guide
- ray machine
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Fee Related
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Abstract
The utility model relates to a guiding structure of a body of an X-ray machine for mammary glands, which comprises a main body structure frame, a guiding rod component and a guiding slide plate component. The guiding rod component is arranged on the main body structure frame, and the guiding slide plate component is disposed on the guiding rod component and can slide along the guiding rod component. In the structure, an electric push rod motor which is disposed on the lower portion of the guiding slide plate component pushes the guiding slide plate component to vertically reciprocate along a guiding rod, and accordingly the position of a C-shaped arm on the guiding slide plate component can be conveniently adjusted properly.
Description
Technical field
This utility model relates to the mechanism that uses on a kind of medical apparatus and instruments, is specifically related to the fuselage guide frame on a kind of breast X-ray machine.
Background technology
Medical apparatus and instruments is as indispensable instrument in the existing medical environment, extensively applying to the doctor carries out in the process of diagnosis and treatment to the patient, wherein, breast X-ray machine is as a kind of diagnostic instruments, extensively applied to clinicing aspect equally, have a mechanism to be called the fuselage guiding mechanism on breast X-ray machine, this mechanism is connected with C shape arm, is used for C shape arm is moved to the position of needs.
The utility model content
Technical purpose of the present utility model is for a kind of fuselage guide frame of breast X-ray machine being provided, being used for and will being attached thereto the position that the C shape arm that connects moves to needs.
To achieve these goals, this utility model provides a kind of breast X-ray machine fuselage guide frame, comprises the primary fuselage frame, guide post portion, the blade fin assembly, described guide post portion is located on the primary fuselage frame, and the blade fin assembly is located in the guide post portion and can be slided along guide post portion.
Further, described primary fuselage frame comprises airframe structure frame, fuselage leading truck, guiding pole socket, guide post fixing head, described fuselage leading truck is located at airframe structure frame inboard, and the guide post fixing head is located at airframe structure frame drift angle place, and the guiding pole socket is located at the bottom of guide post portion.
Further, described guide post portion comprises fuselage guide post and fuselage guide post positioning seat, and fuselage guide post upper end is fixedly arranged on the guide post fixing head by guide post gland and screw, and the lower end is fixedly arranged on the guiding pole socket by fuselage guide post positioning seat.
Further, described fuselage guide post top is fixed on the guide post fixing head by the fillister head screw that embeds in it, is provided with spring washer and flat shim between socket cap and guide post fixing head.
Further, described blade fin assembly comprises the fuselage installing plate, from the outside to the inboard, is provided with back-up ring, roller bearing gland, guide roller successively, and bearing is located in the guide roller, and the orienting roll wheel shaft passes bearing and roller bearing gland, and an end is fixed by back-up ring.
Useful technique effect of the present utility model: adopt this structure, be provided with electric pushrod motor promotion blade fin assembly in blade fin assembly bottom and pump, thereby the C shape arm of being convenient to be located on the blade fin molectron is adjusted to suitable position along guide post.
Below in conjunction with drawings and Examples, the technical solution of the utility model is described in further detail.
Description of drawings
Fig. 1 is the partial sectional view of main apparent direction of the present utility model;
Figure 1A is the partial enlarged drawing of Fig. 1;
Fig. 2 is the partial sectional view of left apparent direction of the present utility model;
Fig. 3 is that assembly of the present utility model cooperates sketch map.
The specific embodiment
Please refer to Fig. 1 to shown in Figure 2, specify below in conjunction with accompanying drawing, this utility model provides a kind of breast X-ray machine fuselage guide frame, comprise the primary fuselage frame, guide post portion, the blade fin assembly, described guide post portion is located on the primary fuselage frame, and the blade fin assembly is located in the guide post portion and can be slided along guide post portion.Wherein:
Described primary fuselage frame comprises airframe structure frame 1, fuselage leading truck 2, guiding pole socket 3, guide post fixing head 4, described fuselage leading truck 2 is located at airframe structure frame 1 inboard, guide post fixing head 4 is located at airframe structure frame 1 drift angle place, and guiding pole socket 3 is located at the bottom of guide post portion.
Described guide post portion comprises fuselage guide post 5 and fuselage guide post positioning seat 6, fuselage guide post 5 upper ends are fixedly arranged on the guide post fixing head 4 by guide post gland 7 and screw 8, the lower end is fixedly arranged on the guiding pole socket 3 by fuselage guide post positioning seat 6, wherein guide post gland 7 is fixed on the guide post fixing head 4 by screw 8, is provided with flat shim 9 and spring washer 10 between the head of screw of guide post gland 7 and screw 8.
Described fuselage guide post 5 tops are fixed on the guide post fixing head 4 by the fillister head screw 11 that embeds in it, are provided with spring washer 12 and flat shim 13 between socket cap and guide post fixing head 4.
Described blade fin assembly comprises fuselage installing plate 14, from the outside to the inboard, be provided with back-up ring 15, roller bearing gland 16, guide roller 17 successively, bearing 18 is located in the guide roller 17, orienting roll wheel shaft 19 passes bearing 18 and roller bearing gland 16, one ends are fixing by back-up ring 15.
Adopt this structure, be provided with electric pushrod motor promotion blade fin assembly in blade fin assembly bottom and pump, thereby the C shape arm of being convenient to be located on the blade fin molectron is adjusted to suitable position along guide post 5.
Please refer to shown in Figure 3, guide post 5 pass with fuselage leading truck 2 to bonded blade fin assembly, between the fuselage leading truck 2 of both sides, be provided with spindle bearing holder 20.
The above; it only is the preferable specific embodiment of this utility model; but protection domain of the present utility model is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that this utility model discloses; the variation that can expect easily or replacement all should be encompassed within the protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with the protection domain of claim.
Claims (5)
1. breast X-ray machine fuselage guide frame is characterized in that, comprises the primary fuselage frame, guide post portion, and the blade fin assembly, described guide post portion is located on the primary fuselage frame, and the blade fin assembly is located in the guide post portion and can be slided along guide post portion.
2. breast X-ray machine fuselage guide frame as claimed in claim 1, it is characterized in that, described primary fuselage frame comprises airframe structure frame, fuselage leading truck, guiding pole socket, guide post fixing head, described fuselage leading truck is located at airframe structure frame inboard, the guide post fixing head is located at airframe structure frame drift angle place, and the guiding pole socket is located at the bottom of guide post portion.
3. breast X-ray machine fuselage guide frame as claimed in claim 1 or 2, it is characterized in that, described guide post portion comprises fuselage guide post and fuselage guide post positioning seat, fuselage guide post upper end is fixedly arranged on the guide post fixing head by guide post gland and screw, and the lower end is fixedly arranged on the guiding pole socket by fuselage guide post positioning seat.
4. breast X-ray machine fuselage guide frame as claimed in claim 3, it is characterized in that, described fuselage guide post top is fixed on the guide post fixing head by the fillister head screw that embeds in it, is provided with spring washer and flat shim between socket cap and guide post fixing head.
5. breast X-ray machine fuselage guide frame as claimed in claim 1, it is characterized in that, described blade fin assembly comprises the fuselage installing plate, from the outside to the inboard, be provided with back-up ring, roller bearing gland, guide roller successively, bearing is located in the guide roller, and the orienting roll wheel shaft passes bearing and roller bearing gland, and an end is fixed by back-up ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200408012U CN201977813U (en) | 2011-02-17 | 2011-02-17 | Guiding structure for body of X-ray machine for mammary glands |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200408012U CN201977813U (en) | 2011-02-17 | 2011-02-17 | Guiding structure for body of X-ray machine for mammary glands |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201977813U true CN201977813U (en) | 2011-09-21 |
Family
ID=44605285
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011200408012U Expired - Fee Related CN201977813U (en) | 2011-02-17 | 2011-02-17 | Guiding structure for body of X-ray machine for mammary glands |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201977813U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103126715A (en) * | 2013-03-05 | 2013-06-05 | 华润万东医疗装备股份有限公司 | Compression device of digital flat mammography |
| CN107963458A (en) * | 2017-12-22 | 2018-04-27 | 无锡市创恒机械有限公司 | A kind of linear guide |
-
2011
- 2011-02-17 CN CN2011200408012U patent/CN201977813U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103126715A (en) * | 2013-03-05 | 2013-06-05 | 华润万东医疗装备股份有限公司 | Compression device of digital flat mammography |
| CN103126715B (en) * | 2013-03-05 | 2015-06-10 | 华润万东医疗装备股份有限公司 | Compression device of digital flat mammography |
| CN107963458A (en) * | 2017-12-22 | 2018-04-27 | 无锡市创恒机械有限公司 | A kind of linear guide |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Free format text: FORMER OWNER: TAN BAOHUA Effective date: 20121114 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| C53 | Correction of patent for invention or patent application | ||
| CB03 | Change of inventor or designer information |
Inventor after: Yao Weimin Inventor before: Yao Weimin Inventor before: Tan Baohua |
|
| COR | Change of bibliographic data |
Free format text: CORRECT: INVENTOR; FROM: YAO WEIMIN TAN BAOHUA TO: YAO WEIMIN Free format text: CORRECT: ADDRESS; FROM: 272100 JINING, SHANDONG PROVINCE TO: 518108 SHENZHEN, GUANGDONG PROVINCE |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20121114 Address after: 518108, 3 floor, Fu Xin Fa Industrial Park, Shiyan fourth industrial area, Shiyan City, Guangdong, Shenzhen, Baoan District Patentee after: Yao Weimin Address before: 272100, room 1, building 9, building No. 402, North Ring Road, No. 258, Jining, Shandong, Yanzhou Patentee before: Yao Weimin Patentee before: Tan Baohua |
|
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Shenzhen macroo Electronics Co., Ltd. Assignor: Yao Weimin Contract record no.: 2014440020115 Denomination of utility model: Guiding structure for body of X-ray machine for mammary glands Granted publication date: 20110921 License type: Exclusive License Record date: 20140414 |
|
| LICC | Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110921 Termination date: 20160217 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |