CN208488012U - A kind of shock resistance hood for MISSILE LAUNCHING - Google Patents
A kind of shock resistance hood for MISSILE LAUNCHING Download PDFInfo
- Publication number
- CN208488012U CN208488012U CN201820996046.7U CN201820996046U CN208488012U CN 208488012 U CN208488012 U CN 208488012U CN 201820996046 U CN201820996046 U CN 201820996046U CN 208488012 U CN208488012 U CN 208488012U
- Authority
- CN
- China
- Prior art keywords
- shock resistance
- hood
- surge baffle
- layer
- surge
- 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 discloses a kind of shock resistance hood for MISSILE LAUNCHING, including a ball taper hood plate, and the edge of the hood plate is provided with annular mounting plate；It is provided on the annular mounting plate and is spaced evenly distributed mounting hole；And primary antibody impact cylinder is provided at the medial center position of the hood plate；The outside of the shock resistance cylinder is disposed with first layer anti-surge baffle, second layer anti-surge baffle and the third layer anti-surge baffle of annular.After the present apparatus is by setting, impact force can be fixed in each smaller shock zone by dispersion when shock resistance, will not because of under the reason of air-flow flows impact agglomerate to and a little considerably increase the impact resistance of hood, extend the service life of hood；And the present apparatus is provided with dismountable relief hole, can be properly done decompression function, and the anti-pressure ability that shock resistance push plate increases outer layer anti-surge baffle is arranged in outside；Increase the impact resistance of single unit system.
Description
Technical field
The utility model relates to a kind of guided missile launcher set field, specifically a kind of shock resistance for MISSILE LAUNCHING
Hood.
Background technique
Guided missile can generate very big recoil in transmitting under normal conditions, in the prior art usually MISSILE LAUNCHING
One piece of shock proof hood is arranged to eliminate the recoil in rear；And this shock proof hood structure usually compares in the prior art
Compared with it is simple, be generally arranged to the cover structure of ball taper, and made of high-intensitive sheet material, it is ensured that it is strong
Degree；But when actual use, after the impact force that when MISSILE LAUNCHING generates collides on hood, impact force sometimes can
Impact agglomerates on a bit, and very big pressure can be caused to hood, causes the destruction to hood, therefore tail in the prior art
Cover can not cope with the impact force of MISSILE LAUNCHING well；In addition its pressure can be from side in shock resistance for hood in the prior art
It discharges at edge, and people can be damaged if outer side stand has staff.
Utility model content
The purpose of this utility model is in view of the deficienciess of the prior art, providing a kind of shock resistance for MISSILE LAUNCHING
Hood.
A kind of technical solution: technical solution used by the utility model solves the problems, such as are as follows: anti-impact for MISSILE LAUNCHING
Hood, including a ball taper hood plate are hit, the edge of the hood plate is provided with annular mounting plate；The annular mounting plate
On be provided with and be spaced evenly distributed mounting hole；And primary antibody impact cylinder is provided at the medial center position of the hood plate；
The outside of the shock resistance cylinder is disposed with first layer anti-surge baffle, second layer anti-surge baffle and the third layer of annular
Anti-surge baffle；And longitudinal shock resistance of right-angled intersection is provided between the shock resistance cylinder and first layer anti-surge baffle
Partition；And the first layer anti-surge baffle and second layer anti-surge baffle and second layer anti-surge baffle and third layer are anti-
16 pieces of longitudinal anti-surge baffles are provided between impacting clapboard；And the anti-surge baffle between this two layers is linear company
Connect setting；And the shock resistance formed between first, second, and third layer of anti-surge baffle of annular and longitudinal anti-surge baffle
Energy-absorbing pad is also filled in region.
Preferably, the first layer anti-surge baffle, second layer anti-surge baffle and third layer anti-surge baffle
Setting height be sequentially increased.
Preferably, being additionally provided with dismountable pressure relief device on the hood plate, which includes relief hole
And it is mounted on removable decompression cover on relief hole.
Preferably, the pressure relief device is arranged between first layer anti-surge baffle and second layer anti-surge baffle.
Preferably, being also equipped with evenly spaced shock resistance push plate on the outside of the third layer anti-surge baffle；Institute
The shock resistance push plate stated is provided with eight pieces altogether.
The utility model has the advantages that the utility model has the following beneficial effects: by setting in its center inside hood in the present apparatus
Resistance to compression cylinder is set, the anti-surge baffle of shellring shape is arranged in outer layer, and longitudinal anti-surge baffle is accordingly arranged will be inside it
The region for the most serious that is hit is separated into the shock zone of several dispersions, and absorbable impact energy is arranged in shock zone
The energy-absorbing pad of amount, after being arranged in this way, impact force can be fixed in each smaller shock zone by dispersion when shock resistance, will not
Because impact agglomerates to the impact resistance for a little considerably increasing hood under the reason of air-flow flows, extend making for hood
Use the service life；And the present apparatus is provided with dismountable relief hole, can be properly done decompression function, and shock resistance push plate is arranged in outside
Increase the anti-pressure ability of outer layer anti-surge baffle；Increase the impact resistance of single unit system；And the impact force in the present apparatus is complete
Portion is absorbed by shock resistance region, therefore the energy being released is smaller, and the probability of very little causes harm to the human body.
Detailed description of the invention
Fig. 1 is the utility model structure chart.
Specific embodiment
In the following with reference to the drawings and specific embodiments, the utility model is furtherd elucidate, the present embodiment is with the utility model
Implemented under premised on technical solution, it should be understood that these embodiments are merely to illustrate the utility model rather than limit this reality
With novel range.
As shown in Figure 1, a kind of shock resistance hood for MISSILE LAUNCHING, including a ball taper hood plate 1, the hood plate 1
Edge be provided with annular mounting plate 2；It is provided on the annular mounting plate 2 and is spaced evenly distributed mounting hole 21；
And primary antibody impact cylinder 3 is provided at the medial center position of the hood plate 1；The outside of the shock resistance cylinder 3 is set gradually
There are first layer anti-surge baffle 4, second layer anti-surge baffle 5 and the third layer anti-surge baffle 6 of annular；And the anti-impact
It hits between cylinder 3 and first layer anti-surge baffle 4 and is provided with longitudinal anti-surge baffle 7 of right-angled intersection；And the first layer
Between anti-surge baffle 4 and second layer anti-surge baffle 5 and second layer anti-surge baffle 5 and third layer anti-surge baffle 6
It is provided with 16 pieces of longitudinal anti-surge baffles 7；And the anti-surge baffle 7 between this two layers is linear connection setting；And
It is also equal in the shock resistance region formed between first, second, and third layer of anti-surge baffle of annular and longitudinal anti-surge baffle 7
Filled with energy-absorbing pad 8.
The setting of the first layer anti-surge baffle 4, second layer anti-surge baffle 5 and third layer anti-surge baffle 6
Height is sequentially increased；Be additionally provided with dismountable pressure relief device on the hood plate 1, the pressure relief device include relief hole 9 with
And it is mounted on removable decompression cover 10 on relief hole 9.
The pressure relief device is arranged between first layer anti-surge baffle 4 and second layer anti-surge baffle 5；Described
The outside of three layers of anti-surge baffle 6 is also equipped with evenly spaced shock resistance push plate 11；The shock resistance push plate 11 is arranged altogether
There are eight pieces.
In the present apparatus inside hood by its center be arranged resistance to compression cylinder, outer layer be arranged shellring shape shock resistance every
Plate, and longitudinal anti-surge baffle is accordingly set, the region for the most serious that is hit inside it is separated into rushing for several dispersions
It hits in region, and the energy-absorbing pad of absorbable impact energy is set in shock zone, in this way after setting, impact force meeting when shock resistance
It is fixed in each smaller shock zone, will not be agglomerated to a bit because of being impacted under the reason of air-flow flows by dispersion,
The impact resistance for considerably increasing hood extends the service life of hood；And the present apparatus is provided with dismountable relief hole,
It can be properly done decompression function, the anti-pressure ability that shock resistance push plate increases outer layer anti-surge baffle is arranged in outside；Increase whole
The impact resistance of device.And the impact force in the present apparatus is all absorbed by shock resistance region, therefore the energy being released
Smaller, the probability of very little causes harm to the human body.
The above is only the preferred embodiment of the utility model, it is noted that for the common skill of the art
For art personnel, without departing from the principle of this utility model, several improvements and modifications can also be made, these improve and
Retouching also should be regarded as the protection scope of the utility model.
Claims (5)
1. a kind of shock resistance hood for MISSILE LAUNCHING, it is characterised in that: including a ball taper hood plate (1), the hood plate
(1) edge is provided with annular mounting plate (2)；It is provided on the annular mounting plate (2) and is spaced evenly distributed peace
It fills hole (21)；And primary antibody impact cylinder (3) is provided at the medial center position of the hood plate (1)；The shock resistance cylinder (3)
Outside be disposed with annular first layer anti-surge baffle (4), second layer anti-surge baffle (5) and third layer shock resistance
Partition (6)；And the longitudinal direction that right-angled intersection is provided between the shock resistance cylinder (3) and first layer anti-surge baffle (4) is anti-
Impacting clapboard (7)；And the first layer anti-surge baffle (4) and second layer anti-surge baffle (5) and second layer shock resistance
16 pieces of longitudinal anti-surge baffles (7) are provided between partition (5) and third layer anti-surge baffle (6)；And this two layers it
Between anti-surge baffle (7) be linear connection setting；And in first, second, and third layer of anti-surge baffle of annular and longitudinal direction
Also energy-absorbing pad (8) are filled in the shock resistance region formed between anti-surge baffle (7).
2. a kind of shock resistance hood for MISSILE LAUNCHING according to claim 1, it is characterised in that: the first layer
The setting height of anti-surge baffle (4), second layer anti-surge baffle (5) and third layer anti-surge baffle (6) is sequentially increased.
3. a kind of shock resistance hood for MISSILE LAUNCHING according to claim 1, it is characterised in that: the hood plate
(1) dismountable pressure relief device is additionally provided on, which includes relief hole (9) and be mounted on can on relief hole (9)
The decompression cover (10) of dismounting.
4. a kind of shock resistance hood for MISSILE LAUNCHING according to claim 3, it is characterised in that: the pressure release dress
It installs between first layer anti-surge baffle (4) and second layer anti-surge baffle (5).
5. a kind of shock resistance hood for MISSILE LAUNCHING according to claim 1, it is characterised in that: the third layer
Evenly spaced shock resistance push plate (11) is also equipped on the outside of anti-surge baffle (6)；The shock resistance push plate (11) is set altogether
It is equipped with eight pieces.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820996046.7U CN208488012U (en) | 2018-06-27 | 2018-06-27 | A kind of shock resistance hood for MISSILE LAUNCHING |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820996046.7U CN208488012U (en) | 2018-06-27 | 2018-06-27 | A kind of shock resistance hood for MISSILE LAUNCHING |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208488012U true CN208488012U (en) | 2019-02-12 |
Family
ID=65248706
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820996046.7U Expired - Fee Related CN208488012U (en) | 2018-06-27 | 2018-06-27 | A kind of shock resistance hood for MISSILE LAUNCHING |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208488012U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111238305A (en) * | 2020-03-16 | 2020-06-05 | 上海机电工程研究所 | Anti-impact tail cover suitable for missile launcher and missile launcher |
| CN112361895A (en) * | 2020-10-22 | 2021-02-12 | 湖北航天技术研究院总体设计所 | Retention type missile tail cover |
-
2018
- 2018-06-27 CN CN201820996046.7U patent/CN208488012U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111238305A (en) * | 2020-03-16 | 2020-06-05 | 上海机电工程研究所 | Anti-impact tail cover suitable for missile launcher and missile launcher |
| CN111238305B (en) * | 2020-03-16 | 2021-12-03 | 上海机电工程研究所 | Anti-impact tail cover suitable for missile launcher and missile launcher |
| CN112361895A (en) * | 2020-10-22 | 2021-02-12 | 湖北航天技术研究院总体设计所 | Retention type missile tail cover |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190212 Termination date: 20200627 |