CN106425926A - Pressing type guided missile warhead fixture - Google Patents
Pressing type guided missile warhead fixture Download PDFInfo
- Publication number
- CN106425926A CN106425926A CN201610914306.7A CN201610914306A CN106425926A CN 106425926 A CN106425926 A CN 106425926A CN 201610914306 A CN201610914306 A CN 201610914306A CN 106425926 A CN106425926 A CN 106425926A
- Authority
- CN
- China
- Prior art keywords
- sleeve
- guided missile
- bearing
- locating ring
- holder
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 description 7
- 238000009434 installation Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to the technical field of guided missile warhead fixture and particularly discloses a pressing type guided missile warhead fixture. The pressing type guided missile warhead fixture comprises a clamping seat, a positioning ring, connecting screws, a sleeve and a bearing, wherein one end of the positioning ring is mounted on the clamping seat; the other end of the positioning ring is assembled with the sleeve; the clamping seat is fixedly connected with the sleeve through the connecting screws; the bearing is mounted in the sleeve; the sleeve adopts a hollow cylindrical structure; an inlet is formed in one end of the sleeve; a bearing mounting groove is formed in the other end of the sleeve; and the inlet is isolated from the bearing mounting groove through a ring-shaped ridge which protrudes inwards. The pressing type guided missile warhead fixture is redesigned based on original techniques, maintains the advantages of the original techniques and has the characteristics of convenience in disassembly and assembly, high applicability and the like.
Description
Technical field
The present invention relates to the technical field of guided missile head frock clamp, particularly a kind of top-closed structure guided missile head frock clamp.
Background technology
Guided missile is a kind of carrying warhead, relies on the propulsion of self power device, guides control flight track by guidance system
Aircraft, current guided missile is even more the basic assurance of China's national security and strategic deterrence.For a long time, China attaches great importance to
The development of guided missile, the missile weapon system of annual China all being updated with certain speed and regenerate, the therefore year output of guided missile
Still than larger, the bullet for how clamping guided missile is an important technology content so as to facilitate guided missile production and the assembling of body,
The development of guided missile head frock clamp is directly restricted and affects guided missile production efficiency.Although some present guided missile head frock clamps
Species is relatively more, and type is also many, but perfect not enough, some guided missile head frock clamps use still not simple and practical enough,
Some guided missile head frock clamps are also had even to be only used on a certain guided missile, this undoubtedly considerably increases guided missile head frock clamp
Species, while also increasing production cost.
Content of the invention
It is an object of the invention to overcoming the shortcoming of prior art, a kind of disassembly and assembly is provided conveniently, convenient mounting and clamping
Guided missile head frock clamp.
The purpose of the present invention is achieved through the following technical solutions：A kind of top-closed structure guided missile head frock clamp, it includes folder
Seat, locating ring, attachment screw, sleeve and bearing, one end of locating ring on holder, the other end of locating ring and sleeve group
Close and install, holder is fixedly connected by attachment screw with sleeve, bearing is in sleeve, and described sleeve is tied for hollow circuit cylinder
Structure, one end of sleeve is provided with carry mouth, and the other end of sleeve is provided with bearing mounting groove, between carry mouth and bearing mounting groove
Separated by the annular rib of a convex.
Described locating ring is hollow structure, and the two ends of locating ring are provided with groove, and one end of locating ring can hold out against
Bearing in sleeve, the other end of locating ring on holder, locating ring by between groove restriction holder and sleeve away from
From.
Described bearing is at the bearing mounting groove in sleeve, and the inner ring of bearing can be entangled and hold out against guided missile head.
The present invention has advantages below：
1st, guided missile head frock clamp of the present invention has the convenient feature of disassembly and assembly, is easy to maintenance and renewal part.
2nd, the structure of the present invention is relatively easy, and the processing and manufacturing of each parts is simply easy, low cost of manufacture.
3rd, bearing arrangement specific to a kind of top-closed structure guided missile head frock clamp of the present invention can realize guided missile life
Rotation conversion surface during product, largely facilitates guided missile production process.
4th, guided missile head frock clamp of the present invention can be applied to the clamping of multiple guided missiles, by changing sleeve
For the clamping of other guided missile heads, thus strong applicability.
Description of the drawings
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the structural representation of Fig. 1 middle sleeve 4；
Fig. 3 is the structural representation of locating ring 2 in Fig. 1；
In figure：1- holder, 2- locating ring, 3- attachment screw, 4- sleeve, 5- bearing, 6- carry mouth, 7- bearing mounting groove, 8- is recessed
Groove.
Specific embodiment
The present invention will be further described below in conjunction with the accompanying drawings, but protection scope of the present invention is not limited to following institute
State.
As shown in Figure 1, Figure 2 and Figure 3, a kind of top-closed structure guided missile head frock clamp, it includes holder 1, locating ring 2, connection
Screw 3, sleeve 4 and bearing 5, one end of locating ring 2 is on holder 1, and the other end of locating ring 2 combines installation with sleeve 4,
Holder 1 is fixedly connected by attachment screw 3 with sleeve 4, and bearing 5 is in sleeve 4, and described sleeve 4 is tied for hollow circuit cylinder
Structure, one end of sleeve 4 is provided with carry mouth 6, and the other end of sleeve 4 is provided with bearing mounting groove 7, and carry mouth 6 is installed with bearing
Separated by the annular rib of a convex between groove 7.
Described locating ring 2 is hollow structure, and the two ends of locating ring 2 are provided with groove 8, and one end of locating ring 2 can
The bearing 5 in sleeve 4 is held out against, the other end of locating ring 2 is on holder 1, and locating ring 2 limits holder 1 with set by groove 8
The distance between cylinder 4；Described bearing 5 is at the bearing mounting groove 7 in sleeve 4, and the inner ring of bearing 5 can be entangled and be pushed up
Tight guided missile head.
The installation process of the present invention and using process as follows：By one end of locating ring 2 on holder, bearing 5 is pacified
It is mounted at the bearing mounting groove 7 in sleeve 4, then sleeve 4 is combined installation with the other end of locating ring 2, attachment screw 3 screws in folder
On seat 1, sleeve 4 and holder 1, top-closed structure guided missile head frock clamp installation is fixedly connected.Horizontal for guided missile being placed on is taken up
Put, with the point of top-closed structure guided missile head frock clamp clamping guided missile head, now guided missile head is by clamping and positioning.Due to entangling
The part of guided missile head can be rotated and be changed face by bearing 5 for the inner ring of bearing 5, therefore guided missile head, and this just effectively facilitates
The production process of guided missile.
The above is only the preferred embodiment of the present invention, it should be understood that the present invention is not limited to described herein
Form, is not to be taken as the exclusion to other embodiment, and can be used for various other combinations, modification and environment, and can be at this
In the text contemplated scope, it is modified by the technology or knowledge of above-mentioned teaching or association area.And those skilled in the art are entered
The change of row and change, then all should be in the protection domains of claims of the present invention without departing from the spirit and scope of the present invention
Interior.
Claims (3)
1. a kind of top-closed structure guided missile head frock clamp, it is characterised in that：It includes holder（1）, locating ring（2）, attachment screw
（3）, sleeve（4）And bearing（5）, locating ring（2）One end be arranged on holder（1）On, locating ring（2）The other end and sleeve
（4）Combination is installed, holder（1）And sleeve（4）By attachment screw（3）It is fixedly connected, bearing（5）Installed in sleeve（4）Interior, institute
The sleeve that states（4）For hollow cylindrical structure, sleeve（4）One end be provided with carry mouth（6）, sleeve（4）The other end be provided with
Bearing mounting groove（7）, carry mouth（6）With bearing mounting groove（7）Between separated by the annular rib of a convex.
2. a kind of top-closed structure guided missile head frock clamp according to claim 1, it is characterised in that：Described locating ring（2）
For hollow structure, locating ring（2）Two ends be provided with groove（8）, locating ring（2）One end can hold out against sleeve（4）Interior
Bearing（5）, locating ring（2）The other end be arranged on holder（1）On, locating ring（2）By groove（8）Limit holder（1）With set
Cylinder（4）The distance between.
3. a kind of top-closed structure guided missile head frock clamp according to claim 1, it is characterised in that：Described bearing（5）Peace
It is mounted in sleeve（4）Interior bearing mounting groove（7）Place, bearing（5）Inner ring can entangle and hold out against guided missile head.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610914306.7A CN106425926B (en) | 2016-10-20 | 2016-10-20 | A kind of top-closed structure guided missile head frock clamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610914306.7A CN106425926B (en) | 2016-10-20 | 2016-10-20 | A kind of top-closed structure guided missile head frock clamp |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106425926A true CN106425926A (en) | 2017-02-22 |
| CN106425926B CN106425926B (en) | 2018-07-24 |
Family
ID=58175959
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610914306.7A Active CN106425926B (en) | 2016-10-20 | 2016-10-20 | A kind of top-closed structure guided missile head frock clamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106425926B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110879022A (en) * | 2019-11-25 | 2020-03-13 | 中国航天空气动力技术研究院 | Small-size guided missile detects strutting arrangement |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995030382A1 (en) * | 1994-05-05 | 1995-11-16 | Joseph Hintersehr | Method and device for manufacturing a dental prosthesis |
| US5487537A (en) * | 1994-06-09 | 1996-01-30 | Rye; Robert A. | Transfer case stand |
| CN1443287A (en) * | 2000-08-04 | 2003-09-17 | 本田技研工业株式会社 | Elastic bush and method of press-fitting elastic bush |
| CN204308235U (en) * | 2014-12-09 | 2015-05-06 | 株洲中航动科南方燃气轮机成套制造安装有限公司 | Part fixture for processing |
| CN204819366U (en) * | 2015-07-17 | 2015-12-02 | 中国人民解放军军械工程学院 | Terminal -guided shell control cabinet is connected volution and is unloaded instrument soon |
| CN205290796U (en) * | 2015-12-16 | 2016-06-08 | 沈阳航天新星机电有限责任公司 | Guided missile airvane launches component Assembly frock |
-
2016
- 2016-10-20 CN CN201610914306.7A patent/CN106425926B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995030382A1 (en) * | 1994-05-05 | 1995-11-16 | Joseph Hintersehr | Method and device for manufacturing a dental prosthesis |
| US5487537A (en) * | 1994-06-09 | 1996-01-30 | Rye; Robert A. | Transfer case stand |
| CN1443287A (en) * | 2000-08-04 | 2003-09-17 | 本田技研工业株式会社 | Elastic bush and method of press-fitting elastic bush |
| CN204308235U (en) * | 2014-12-09 | 2015-05-06 | 株洲中航动科南方燃气轮机成套制造安装有限公司 | Part fixture for processing |
| CN204819366U (en) * | 2015-07-17 | 2015-12-02 | 中国人民解放军军械工程学院 | Terminal -guided shell control cabinet is connected volution and is unloaded instrument soon |
| CN205290796U (en) * | 2015-12-16 | 2016-06-08 | 沈阳航天新星机电有限责任公司 | Guided missile airvane launches component Assembly frock |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110879022A (en) * | 2019-11-25 | 2020-03-13 | 中国航天空气动力技术研究院 | Small-size guided missile detects strutting arrangement |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106425926B (en) | 2018-07-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Pressing type guided missile warhead fixture Effective date of registration: 20200720 Granted publication date: 20180724 Pledgee: Agricultural Bank of China Limited Chengdu Economic and Technological Development Zone sub branch Pledgor: CHENGDU JIUXIN TIMES TECHNOLOGY Co.,Ltd. Registration number: Y2020510000075 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Granted publication date: 20180724 Pledgee: Agricultural Bank of China Limited Chengdu Economic and Technological Development Zone sub branch Pledgor: CHENGDU JIUXIN TIMES TECHNOLOGY CO.,LTD. Registration number: Y2020510000075 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: A Top Tight Missile Head Fixture Granted publication date: 20180724 Pledgee: Agricultural Bank of China Limited Chengdu Economic and Technological Development Zone sub branch Pledgor: CHENGDU JIUXIN TIMES TECHNOLOGY CO.,LTD. Registration number: Y2024510000035 |