CN106392726A - Missile head tool fixture - Google Patents
Missile head tool fixture Download PDFInfo
- Publication number
- CN106392726A CN106392726A CN201610914302.9A CN201610914302A CN106392726A CN 106392726 A CN106392726 A CN 106392726A CN 201610914302 A CN201610914302 A CN 201610914302A CN 106392726 A CN106392726 A CN 106392726A
- Authority
- CN
- China
- Prior art keywords
- guided missile
- missile head
- inner chamber
- adapter sleeve
- connecting rod
- 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
- 230000006978 adaptation Effects 0.000 claims 1
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 238000003754 machining Methods 0.000 abstract 1
- 239000007787 solid Substances 0.000 description 2
- 230000007717 exclusion Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 231100000225 lethality Toxicity 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 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 missile head tool fixture. The missile head tool fixture comprises a connection rod and a connection sleeve; a boss is arranged on the part, close to the head position, of one end of the connection rod in the circumferential direction of the connection rod; the connection rod is connected with a missile head; the missile head is internally provided with a first inner cavity; the head, close to the boss, of the connection rod stretches into the first inner cavity of the missile head and is fixedly connected with the missile head through a thread; the connection rod is externally provided with a connection sleeve; the connection sleeve is provided with a second inner cavity; the second inner cavity is divided into an inner cavity A, an inner cavity B and an inner cavity C; the inner cavity A is a conical cavity and is matched with the shape of the missile head; the inner cavity B is a cylindrical cavity and is matched with the boss; the inner cavity C is a cylinder cavity and is matched with the connection rod; and a plurality of screws A are arranged on the side wall, located in the inner cavity A, of the connection rod. The missile head tool fixture has the beneficial effects of being precise in positioning, tight and reliable in connection and capable of improving the missile head machining quality.
Description
Technical field
The present invention relates to the technical field of fixture, particularly a kind of guided missile head frock clamp.
Background technology
Guided missile is because lethality is strong, collateral damage is little, reflecting time is short, fighting efficiency is high, strike becomes the features such as accurate
The first-selected ammunition of precision strike is realized, guided missile head, as the warhead of guided missile, is the important component part of guided missile in modern war,
It is arranged on guided missile foremost, when guided missile head is processed or is installed with next stage, luggage is directly entered using scroll chuck
Folder, in clamping engineering, needs repeatedly to adjust guided missile head position and carries out centering, devote a tremendous amount of time, and adopt three-jaw card
Disk directly carries out clamping guided missile head, and guided missile head only sub-fraction is jammed, and it is not firm to connect, and positioning is not accurate, affects guided missile
The precision of processing, thus affect the precision strike of guided missile.
Content of the invention
It is an object of the invention to overcoming the shortcoming of prior art, a kind of accurate positioning being provided, connects fastening reliability, improve guided missile
The guided missile head frock clamp of head crudy.
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
Female connector, one end of described connecting rod is circumferentially with boss near tip position along it, and connecting rod is connected with guided missile head, guided missile head
In be provided with inner chamber I, stretch in the inner chamber I of guided missile head near the connecting rod termination of boss and pass through that screw thread is fixing with guided missile head to be connected
Connect, outside connecting rod, be provided with adapter sleeve, connect and be arranged with inner chamber II, inner chamber II is divided into inner chamber A, inner chamber B and inner chamber C, and inner chamber A is
Conical cavity and being adapted with guided missile head profile, inner chamber B is cylindrical cavity and is adapted with boss, inner chamber C be cylindrical cavity and with
Connecting rod is adapted, and is provided with multiple screw A on the side wall of the adapter sleeve of inner chamber location A.
It is provided with through hole on described inner chamber A corresponding adapter sleeve side wall, in through hole, is provided with spring, near 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 adapter sleeve by screw B.
Described screw A is along the side wall even circumferential setting of adapter sleeve.
The external diameter of described boss is identical with the external diameter of guided missile head connecting portion.
Described adapter sleeve is fixed on lathe by scroll chuck.
The present invention has advantages below：By arranging connecting rod and adapter sleeve, and boss is arranged on connecting rod, connecting
Setting inner chamber A, inner chamber B and inner chamber C in set, it is ensured that being fastenedly connected of connecting rod and guided missile head and adapter sleeve, realize connecting tightly
Gu reliability and accurate positioning；Clamping by adapter sleeve and scroll chuck, it is to avoid the damage of guided missile head profile, adapter sleeve is direct
In insertion lathe it is ensured that the axiality of trajectory head, thus improve guided missile head crudy it is ensured that guided missile head and next
Level guided missile position precisely connects.
Brief description
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the enlarged drawing of A-A in Fig. 1；
In figure, 1 connecting rod, 2 adapter sleeves, 3 boss, 4 guided missile heads, 5 screw A, 6 springs, 7 pressing plates, 8 is solid
Determine block, 9 screw B.
Specific embodiment
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 described below：
As shown in figure 1, a kind of guided missile head frock clamp, including connecting rod 1 and adapter sleeve 2, one end of connecting rod 1 is near termination position
Put and be circumferentially provided with boss 3 along it, connecting rod 1 is connected with guided missile head 4, is provided with inner chamber I in guided missile head 4, near the company of boss 3
The termination of extension bar 1 is stretched in the inner chamber I of guided missile head 4 and is fixedly connected with guided missile head 4 by screw thread, and guided missile head 4 also realized by boss 3
The axially effect of direction positioning, guided missile head 4 is divided into cylindrical connecting portion position and taper filling position, the termination of connecting rod 1
It is connected with the cylindrical connecting portion position of guided missile head 4, the external diameter of cylindrical connecting portion position of guided missile head 4 and the external diameter size of boss 3
Identical；It is provided with inner chamber II, inner chamber II is divided into inner chamber A, inner chamber B and inner chamber C, inner chamber A is conical cavity, interior in described adapter sleeve 2
Chamber B and inner chamber C is cylindrical cavity, and inner chamber B is bigger than inner chamber C, is placed on the inner chamber of adapter sleeve 2 after connecting rod 1 and guided missile head 4 connection
In II, the taper filling position of wherein guided missile head 4 is placed in inner chamber A, the taper of guided missile head 4 fill the profile at position with interior
Chamber A is adapted, and the cylindrical connecting portion position of boss 3 and guided missile head 4 is located in inner chamber B, and the cylinder of boss 3 and guided missile head 4
Connecting portion is adapted with inner chamber B, and boss 3 also acts as axially position in adapter sleeve 2 for the connecting rod 1, its remaining part of connecting rod 1
Position is located in inner chamber C, and remaining position of connecting rod 1 is adapted with inner chamber C, and in inner chamber B and the corresponding adapter sleeve of inner chamber C 2
Side wall on, be evenly arranged with multiple screw A5 along adapter sleeve 2 circumference, screw A5 plays the work of fixing guided missile head 4 and connecting rod 1
With；Adapter sleeve is fixed on lathe by scroll chuck.
As shown in Fig. 2 being provided with through hole on the corresponding adapter sleeve of inner chamber A 2 side wall, in through hole, it is provided with spring 6, near leading
Spring 6 end of bullet 4 is provided with pressing plate 7, and the other end of spring 6 is connected on fixed block 8, and it is solid that fixed block 8 passes through screw B9
It is scheduled on adapter sleeve 2, in frock, after guided missile head 4, connecting rod 1 and adapter sleeve 2 install, by spring 6, pressing plate is stretched into even
In the through hole of female connector 2 inner chamber A side wall, by fixed block 8, spring 6 is being compressed, locating piece 8 is fixed on adapter sleeve by screw B9
On 2 lateral wall, pressing plate 7 plays the effect compressing guided missile head 4 further, and pressing plate 7 also produces in guided missile head 4 axial direction
One power, plays the effect of tension guided missile head 4, further ensures and be fastenedly connected.
During work, first close boss 3 termination in connecting rod 1 is screwed in the inner chamber I of guided missile head 4, connecting rod 1 and guided missile
4 are threaded connection, then connecting rod 1 are put into together with guided missile head 4 in the inner chamber II of adapter sleeve 2, the wherein cone of guided missile head 4
Shape position is located in inner chamber A and is completely embedded contact, the boss 3 of the connecting portion of guided missile head 4 and connecting rod 1 and connecting rod 1
In inner chamber B and with screw A5, the connecting portion of guided missile head 4 and connecting rod 1 is fixed, positioned at the connecting rod 1 of boss 3 opposite side
Position is located in inner chamber C and is fixed connecting rod with screw A5, then pressing plate 7 inserts the through hole on adapter sleeve 2 side wall by spring 6
In, by fixed block 8, spring 6 is compressed, with screw B9, fixed block 8 is fixed on the lateral wall of adapter sleeve 2, it is achieved thereby that
The precise positioning of guided missile head 4；Again adapter sleeve 2 is fixed on lathe by scroll chuck away from one end of guided missile head 4, by machine
Bed drives adapter sleeve 2, drives guided missile head 4 to rotate by adapter sleeve 2.
The above be only the preferred embodiment of the present invention it should be understood that the present invention be 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 described contemplated scope of literary composition, 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 (5)
1. a kind of guided missile head frock clamp it is characterised in that：Including connecting rod（1）And adapter sleeve（2）, described connecting rod（1）
One end be circumferentially with boss near tip position along it（3）, connecting rod（1）With guided missile head（4）It is connected, guided missile head（4）In set
It is equipped with inner chamber I, near boss（3）Connecting rod（1）Guided missile head is stretched in termination（4）Inner chamber I in and pass through screw thread and guided missile head
（4）It is fixedly connected, connecting rod（1）Outside is provided with adapter sleeve（2）, adapter sleeve（2）It is provided with inner chamber II, inner chamber II is divided into inner chamber A, interior
Chamber B and inner chamber C, inner chamber A are conical cavity and and guided missile head（4）Profile is adapted, and inner chamber B is cylindrical cavity and and boss（3）Phase
Adaptation, inner chamber C is cylindrical cavity and and connecting rod（1）It is adapted, positioned at the adapter sleeve of inner chamber location A（2）Side wall on arrange
There are multiple screw A（5）.
2. a kind of guided missile head frock clamp according to claim 1 it is characterised in that：The described corresponding connection of inner chamber A
Set（2）Through hole is provided with the wall of side, in through hole, is provided with spring（6）, near guided missile head（4）Spring（6）End is provided with pressure
Plate（7）, spring（6）The other end be connected to fixed block（8）On, fixed block（8）By screw B（9）It is fixed on adapter sleeve（2）
On.
3. a kind of guided missile head frock clamp according to claim 1 it is characterised in that：Described screw A（5）Along adapter sleeve
（2）The setting of side wall even circumferential.
4. a kind of guided missile head frock clamp according to claim 1 it is characterised in that：Described boss（3）External diameter with
Guided missile head（4）The external 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：Described adapter 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 true CN106392726A (en) | 2017-02-15 |
| CN106392726B 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) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100216A (en) * | 2018-09-17 | 2018-12-28 | 江西洪都航空工业集团有限责任公司 | A kind of missile block hanging load tool structure |
-
2016
- 2016-10-20 CN CN201610914302.9A patent/CN106392726B/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100216A (en) * | 2018-09-17 | 2018-12-28 | 江西洪都航空工业集团有限责任公司 | A kind of missile block hanging load tool structure |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106392726B (en) | 2018-08-28 |
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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 |
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 |
|
| PE01 | Entry into force 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 |
|
| PC01 | Cancellation 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 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |