CN106392726B - A kind of guided missile head frock clamp - Google Patents
A kind of guided missile head frock clamp Download PDFInfo
- Publication number
- CN106392726B CN106392726B CN201610914302.9A CN201610914302A CN106392726B CN 106392726 B CN106392726 B CN 106392726B CN 201610914302 A CN201610914302 A CN 201610914302A CN 106392726 B CN106392726 B CN 106392726B
- Authority
- CN
- China
- Prior art keywords
- inner cavity
- guided missile
- missile head
- connecting rod
- connector sleeve
- 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.)
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Links
- 230000006978 adaptation Effects 0.000 claims 1
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 1
- 231100000225 lethality Toxicity 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- 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
- B23Q3/12—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for securing to a spindle in general
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Clamps And Clips (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a kind of guided missile head frock clamps, including connecting rod and connector sleeve, one end of the connecting rod is circumferentially with boss close to tip position along it, connecting rod is connected with guided missile head, inner cavity I is provided in guided missile head, it is fixedly connected with guided missile head in the inner cavity I that guided missile head is stretched into the connecting rod end of boss and by screw thread, connector sleeve is equipped with outside connecting rod, connector sleeve is equipped with inner cavity II, inner cavity II is divided for inner cavity A, inner cavity B and inner cavity C, inner cavity A is conical cavity and is adapted with guided missile head shape, inner cavity B is cylindrical cavity and is adapted with boss, inner cavity C is cylindrical cavity and is adapted with connecting rod, multiple screw A are provided on the side wall of the connector sleeve of inner cavity location A.The beneficial effects of the invention are as follows：Accurate positioning, connection fastening is reliable, improves guided missile head processing quality.
Description
Technical field
The present invention relates to the technical field of fixture, especially a kind of guided missile head frock clamp.
Background technology
Guided missile becomes due to the features such as lethality is strong, collateral damage is small, reflecting time is short, fighting efficiency is high, strike is accurate
The preferred ammunition of precision strike is realized in modern war, warhead of the guided missile head as guided missile is the important component of guided missile,
Mounted on the front end of guided missile, using scroll chuck directly into luggage when guided missile head is processed or is installed with next stage
Folder is needed to adjust guided missile head position progress centering repeatedly, be devoted a tremendous amount of time, and use three-jaw card in clamping engineering
Disk directly carries out clamping guided missile head, and guided missile head only has sub-fraction to be jammed, and connection is not firm, and positioning is not accurate, influences guided missile
The precision of processing, to influence the precision strike of guided missile.
Invention content
It is an object of the invention to overcome the prior art, provide that a kind of accurate positioning, connection fastening is reliable, improves
The guided missile head frock clamp of guided missile head processing quality.
The purpose of the present invention is achieved through the following technical solutions：A kind of guided missile head frock clamp, including connecting rod and company
One end of female connector, the connecting rod is circumferentially with boss close to tip position along it, and connecting rod is connected with guided missile head, guided missile head
In be provided with inner cavity I, stretched into the inner cavity I of guided missile head close to the connecting rod end of boss and pass through screw thread and fixed with guided missile head and connect
It connects, connector sleeve is equipped with outside connecting rod, connector sleeve is equipped with inner cavity II, and inner cavity II is divided is for inner cavity A, inner cavity B and inner cavity C, inner cavity A
Conical cavity and be adapted with guided missile head shape, inner cavity B is cylindrical cavity and is adapted with boss, inner cavity C be cylindrical cavity and with
Connecting rod is adapted, and multiple screw A are provided on the side wall of the connector sleeve of inner cavity location A.
It is provided with through-hole on the corresponding connector sleeve side walls of the inner cavity A, spring is provided in through-hole, close to guided missile head
Spring end is provided with pressing plate, and the other end of spring is connected on fixed block, and fixed block is fixed on by screw B on connector sleeve.
The screw A is arranged along the side wall even circumferential of connector sleeve.
The outer diameter of the boss is identical as the outer diameter of guided missile head connecting portion.
The connector sleeve is fixed on by scroll chuck on lathe.
The present invention has the following advantages：By the way that connecting rod and connector sleeve is arranged, and boss is set in connecting rod, is being connected
Inner cavity A, inner cavity B and inner cavity C are set in set, ensure that being fastenedly connected for connecting rod and guided missile head and connector sleeve, realize connection tightly
Gu reliable and accurate positioning；By the clamping of connector sleeve and scroll chuck, the damage of guided missile head shape is avoided, connector sleeve is direct
Be inserted into lathe, ensure that the concentricity of trajectory head, to improve guided missile head processing quality, it is ensured that guided missile head with it is next
Grade guided missile position precisely connects.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention；
Fig. 2 is the enlarged drawing of A-A in Fig. 1；
In figure, 1-connecting rod, 2-connector sleeves, 3-boss, 4-guided missile heads, 5-screw A, 6-springs, 7-pressing plates,
8-fixed blocks, 9-screw B.
Specific implementation mode
The present invention will be further described below in conjunction with the accompanying drawings, and protection scope of the present invention is not limited to as described below：
As shown in Figure 1, proximal end is leaned in a kind of guided missile head frock clamp, including connecting rod 1 and connector sleeve 2, one end of connecting rod 1
Head position is circumferentially provided with boss 3 along it, and connecting rod 1 is connected with guided missile head 4, and inner cavity I is provided in guided missile head 4, close to boss 3
The end of connecting rod 1 stretch into the inner cavity I of guided missile head 4 and be fixedly connected with guided missile head 4 by screw thread, boss 3 is also realized and is led
The effect that axially direction positions of bullet 4, guided missile head 4 divides fills position for cylindrical connecting portion position and taper, connecting rod 1
End is connected with the cylindrical connecting portion position of guided missile head 4, the outer diameter of the outer diameter and boss 3 of the cylindrical connecting portion position of guided missile head 4
Size is identical；Inner cavity II is equipped in the connector sleeve 2, it is taper that inner cavity II, which is divided for inner cavity A, inner cavity B and inner cavity C, inner cavity A,
Chamber, inner cavity B and inner cavity C are cylindrical cavity, and inner cavity B is bigger than inner cavity C, and connector sleeve 2 is placed on after connecting rod 1 and the connection of guided missile head 4
Inner cavity II in, the taper filling position of wherein guided missile head 4 is placed in the A of inner cavity, the taper of guided missile head 4 filling position it is outer
Shape is adapted with inner cavity A, and the cylindrical connecting portion position of boss 3 and guided missile head 4 is located in the B of inner cavity, and boss 3 and guided missile head 4
Cylindrical connecting portion position is adapted with inner cavity B, and boss 3 also acts as axially position of the connecting rod 1 in connector sleeve 2, connecting rod 1
Remaining position is located in the C of inner cavity, and remaining position of connecting rod 1 is adapted with inner cavity C, and in inner cavity B and the corresponding companies of inner cavity C
On the side wall of female connector 2, multiple screw A5 circumferentially are evenly arranged with along connector sleeve 2, screw A5 plays fixed guided missile head 4 and connecting rod
1 effect；Connector sleeve is fixed on by scroll chuck on lathe.
As shown in Fig. 2, being provided with through-hole on corresponding 2 side walls of connector sleeve of inner cavity A, spring 6 is provided in through-hole, it is close to lead
6 end set of spring of bullet 4 has pressing plate 7, the other end of spring 6 to be connected on fixed block 8, and fixed block 8 is solid by screw B9
It is scheduled on connector sleeve 2, in tooling, after guided missile head 4, connecting rod 1 and connector sleeve 2 install, pressing plate is stretched by company by spring 6
In the through-hole of 2 inner cavity A side walls of female connector, spring 6 is being compressed by fixed block 8, locating piece 8 is fixed on connector sleeve by screw B9
On 2 lateral wall, pressing plate 7 plays the role of further compressing guided missile head 4, and pressing plate 7 is also generated in 4 axial direction of guided missile head
One power plays the role of tensing guided missile head 4, further ensures and be fastenedly connected.
When work, first 3 end of boss close in connecting rod 1 is screwed into the inner cavity I of guided missile head 4, connecting rod 1 and guided missile
First 4 are connected through a screw thread, then connecting rod 1 and guided missile head 4 are put into togerther in the inner cavity II of connector sleeve 2, wherein the cone of guided missile head 4
Shape position is located in the A of inner cavity and is completely embedded contact, the boss 3 of the connecting portion and connecting rod 1 of guided missile head 4 and connecting rod 1
It is fixed in the B of inner cavity and with screw A5 by guided missile head 4 and the connecting portion of connecting rod 1, is located at the connecting rod 1 of 3 other side of boss
Position is located in the C of inner cavity and is fixed with screw A5 by connecting rod, then pressing plate 7 is inserted into the through-hole on 2 side wall of connector sleeve by spring 6
In, spring 6 is compressed by fixed block 8, fixed block 8 is fixed on the lateral wall of connector sleeve 2 with screw B9, to realize
The precise positioning of guided missile head 4；The one end of connector sleeve 2 far from guided missile head 4 is fixed on by scroll chuck on lathe again, passes through machine
Bed drives connector sleeve 2, drives guided missile head 4 to rotate by connector sleeve 2.
The above is only a 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 excluding other embodiments, and can be used for other combinations, modifications, and environments, and can be at this
In the text contemplated scope, modifications can be made through the above teachings or related fields of technology or knowledge.And those skilled in the art institute into
Capable modifications and changes do not depart from the spirit and scope of the present invention, then all should be in the protection domain of appended claims of the present invention
It is interior.
Claims (5)
1. a kind of guided missile head frock clamp, it is characterised in that：Including connecting rod（1）And connector sleeve（2）, the connecting rod（1）
One end be circumferentially with boss along it close to tip position（3）, connecting rod（1）With guided missile head（4）It is connected, guided missile head（4）In set
It is equipped with inner cavity I, close to boss（3）Connecting rod（1）Guided missile head is stretched into end（4）Inner cavity I in and pass through screw thread and guided missile head
（4）It is fixedly connected, connecting rod（1）Outside is equipped with connector sleeve（2）, connector sleeve（2）Equipped with inner cavity II, inner cavity II is divided for inner cavity A, interior
Chamber B and inner cavity C, inner cavity A are conical cavity and and guided missile head（4）Shape is adapted, and inner cavity B is cylindrical cavity and and boss（3）Phase
Adaptation, inner cavity C are cylindrical cavity and and connecting rod（1）It is upper to remove boss（3）And it stretches into and is fixed in guided missile head（4）In inner cavity I
Rest part outside end is adapted；B and the corresponding connector sleeves of inner cavity C in inner cavity（2）Side wall on, along connector sleeve（2）It is circumferential
It is evenly arranged with multiple screw A（5）.
2. a kind of guided missile head frock clamp according to claim 1, it is characterised in that：The corresponding connections of inner cavity A
Set（2）It is provided with through-hole on side wall, spring is provided in through-hole（6）, close to guided missile head（4）Spring（6）End set has pressure
Plate（7）, spring（6）The other end be connected to fixed block（8）On, fixed block（8）Pass through screw B（9）It is fixed on connector sleeve（2）
On.
3. a kind of guided missile head frock clamp according to claim 1, it is characterised in that：The screw A（5）Along connector sleeve
（2）Side wall even circumferential setting.
4. a kind of guided missile head frock clamp according to claim 1, it is characterised in that：The boss（3）Outer diameter with
Guided missile head（4）The outer diameter of connecting portion is identical.
5. a kind of guided missile head frock clamp according to claim 1 or 3, it is characterised in that：The connector sleeve（2）Pass through
Scroll chuck is fixed on lathe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610914302.9A CN106392726B (en) | 2016-10-20 | 2016-10-20 | A kind of guided missile head frock clamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610914302.9A CN106392726B (en) | 2016-10-20 | 2016-10-20 | A kind of guided missile head frock clamp |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106392726A CN106392726A (en) | 2017-02-15 |
| CN106392726B true CN106392726B (en) | 2018-08-28 |
Family
ID=58013176
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610914302.9A Active CN106392726B (en) | 2016-10-20 | 2016-10-20 | A kind of guided missile head frock clamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106392726B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100216B (en) * | 2018-09-17 | 2021-05-18 | 江西洪都航空工业集团有限责任公司 | Guided missile slider hanging and loading tool structure |
-
2016
- 2016-10-20 CN CN201610914302.9A patent/CN106392726B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN106392726A (en) | 2017-02-15 |
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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: Missile head tool fixture Effective date of registration: 20200720 Granted publication date: 20180828 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: 20180828 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 missile head fixture Granted publication date: 20180828 Pledgee: Agricultural Bank of China Limited Chengdu Economic and Technological Development Zone sub branch Pledgor: CHENGDU JIUXIN TIMES TECHNOLOGY CO.,LTD. Registration number: Y2024510000035 |