CN201457739U - Rectification protector for gunship guidance device - Google Patents
Rectification protector for gunship guidance device Download PDFInfo
- Publication number
- CN201457739U CN201457739U CN2009200030529U CN200920003052U CN201457739U CN 201457739 U CN201457739 U CN 201457739U CN 2009200030529 U CN2009200030529 U CN 2009200030529U CN 200920003052 U CN200920003052 U CN 200920003052U CN 201457739 U CN201457739 U CN 201457739U
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- China
- Prior art keywords
- cylindrical drum
- liner
- rectification
- utility
- gunship
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Abstract
The utility model discloses a rectification protector for a gunship guidance device, belonging to the field of national defense. The rectification protector consists of a cylinder (1), a lining cylinder (2), a module wall (3) and a top enclosure (4). As being produced by adopting high-technology material and reasonable design, the rectification protector can play a role of rectifying protection for the guidance device arranged on the gunship, and is also applicable to protecting a pilot day and night forward-looking system sensor arranged on the gunship.
Description
Technical field
The utility model relates to a kind of guide apparatus rectification protector of using in the national defence field, be made up of cylindrical drum, overhead guard, module wall, liner cylindrical drum.
Background technology
The rectification protector that the guide apparatus of being installed on the various now armed helicopters is installed all is to be made by synthetic polyester plastics, homogeneous armor steel; and it is simple in structure; very easily ruined and injure guide apparatus, thereby make helicopter lose tracking to target, lock function and be out of action by aviation cannon, cumulative attack.The rectification protector of being installed on the guide apparatus as Russia's manufacturing is exactly to make with common homogeneous armor; its structure is exactly cylindrical drum of mono-, and protective value is poor, is just repeatedly ruined by the kinetic energy attack in Chechen War; injure guide apparatus, make the helicopter of Russian army lose the advantage of operation.
Summary of the invention
The utility model provides a kind of rectification protector of using on a kind of guide apparatus of installing on to armed helicopter in the national defence field.In order to achieve the above object, the utility model serves as a contrast cylindrical drum within the walls by cylindrical drum, overhead guard, module and forms.Stamp out one along the position at liner cylinder nozzle and be 90 ° flange with stack shell, on flange, be drilled with eight and be used for installing screw hole of the present utility model, be drilled with rivet hole equably at the following stack shell of liner cylindrical drum spherical top position, with rivet the module wall is installed on the liner cylindrical drum stack shell, and the module wall is closely arranged each other, again overhead guard is covered on tightly the enlightened top portion of liner cylindrical drum ball, the liner cylindrical drum that module wall and overhead guard will be installed with cylindrical drum covers afterwards, and with the cylinder nozzle along position and liner cylindrical drum flange position firm welding, become as a whole.
Because cylindrical drum of the present utility model, the liner cylindrical drum is made by compound armour and overhead guard, module wall are made by the aluminium chloride pottery; very strong armor facing ability is all arranged; can stand the strike of aviation cannon, cumulative bullet, sniping gun effectively; configuration design is reasonable in addition, can play good rectification protective effect to guide apparatus.The utility model adopts the high-tech material manufacture, does not influence emission and the reception of guide apparatus to signal.The utility model also be applicable to chaufeur that helicopter is installed above round the clock the forward sight system sensor play a protective role.
Description of drawings
Fig. 1 is the cutaway view of the utility model specific embodiment.
Fig. 2 is the front elevation of the utility model liner cylindrical drum.
Fig. 3 be in the utility model specific implementation process on the liner cylindrical drum front elevation when installed module wall and overhead guard.
Fig. 4 is the birds-eye view of the utility model specific embodiment.
Fig. 5 is the cross sectional drawing of the utility model module wall.
Fig. 6 is the back view of the utility model module wall.
Fig. 7 is the front elevation of the utility model module wall.
Fig. 8 is the front elevation of the utility model cylindrical drum.
Fig. 9 is the front elevational view of the utility model overhead guard.
Figure 10 is the upward view of the utility model overhead guard.
Concrete enforcement
The utility model is described in further detail below in conjunction with specification drawings and specific embodiments.
Armed helicopter guide apparatus rectification protector shown in Figure 1 is made up of cylindrical drum 1, liner cylindrical drum 2, module wall 3, overhead guard 4.
2 mouthfuls of liner cylindrical drum shown in Figure 2 stamp out one and are 90 ° flange 5 with stack shell along the position, be drilled with eight and be used for installing rivet hole 6 of the present utility model on flange 5, are processed with rivet hole 7 equably at the following stack shell of liner cylindrical drum 2 spherical top position.
Shown in Figure 3ly with rivet module wall 3 is fixed on massively by rivet hole 7 on the stack shell of liner cylindrical drum 2, then overhead guard 4 is covered on the spherical top of liner cylindrical drum 2 at the following stack shell of liner cylindrical drum 2 spherical top position.
After module wall 3 on liner cylindrical drum 2 shown in Figure 1 installs with overhead guard 4, again with on cylindrical drum 1 cover, and with 1 mouthful of cylindrical drum along position and liner cylindrical drum 2 flanges 5 position firm welding, become as a whole.
When using, the utility model requires the whole good compactness that has, increase anti-strike capability, so install on the liner cylindrical drum 2 after module wall 3 and the overhead guard 4, when being inserted in the cylindrical drum 1 again will with cylindrical drum 1 tight connecting, so when manufacturing and designing, must make the semicircle orphan degree of overhead guard 4 consistent with the semicircle orphan degree at cylindrical drum 1 top, because system fastened close coincideing with semicircle position, liner cylindrical drum 2 top when overhead guard 4 covered on the liner cylindrical drum 2, the semicircle orphan degree of overhead guard 4 also is consistent with the semicircle orphan degree at liner cylindrical drum 2 tops so, nature, cylindrical drum 1 is consistent with the arc degree at the semicircle position at liner cylindrical drum 2 tops.
Owing to emphasize compactness, the spherical top of liner cylinder 2 places overhead guard 4 and the stack shell position must be smooth with the outer wall that forms after the good module wall 3 of rivet riveting, and when being inserted in the cylindrical drum 1 will with cylindrical drum 1 tight connecting, module wall 3 is consistent with the Thickness Design one-tenth of overhead guard 4 so.
After the utility model manufacturing finishes; owing to adopted high-tech material and rational exterior design; can stand the strike of aviation cannon, cumulative bullet, sniping gun effectively, guide apparatus is played good rectification protective effect, and not influence emission and the reception of guide apparatus signal.The utility model also be applicable to chaufeur that helicopter, tank are installed above round the clock the forward sight system sensor play a protective role.
Claims (3)
1. armed helicopter guide apparatus rectification protector of forming by cylindrical drum (1), liner cylindrical drum (2), module wall (3), overhead guard (4); it is characterized in that: the spherical top of liner cylindrical drum (2) is laid protective case (4); the stack shell position is equipped with module wall (3) with rivet; again with on cylindrical drum (1) cover, and mouthful be welded into as a whole cylindrical drum (1) along position and liner cylindrical drum (2) flange (5) position.
2. armed helicopter guide apparatus rectification protector according to claim 1 is characterized in that: cylindrical drum (1) is the semisphere with radian with the top of liner cylindrical drum (2).
3. according to claim 1 or the described armed helicopter guide apparatus of claim 3 rectification protector, it is characterized in that: the consistency of thickness of module wall (3) and overhead guard (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200030529U CN201457739U (en) | 2009-03-26 | 2009-03-26 | Rectification protector for gunship guidance device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200030529U CN201457739U (en) | 2009-03-26 | 2009-03-26 | Rectification protector for gunship guidance device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201457739U true CN201457739U (en) | 2010-05-12 |
Family
ID=42385093
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009200030529U Expired - Fee Related CN201457739U (en) | 2009-03-26 | 2009-03-26 | Rectification protector for gunship guidance device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201457739U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102556356A (en) * | 2010-12-06 | 2012-07-11 | 空中客车运营公司 | Protecting device for an aircraft exterior probe |
-
2009
- 2009-03-26 CN CN2009200030529U patent/CN201457739U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102556356A (en) * | 2010-12-06 | 2012-07-11 | 空中客车运营公司 | Protecting device for an aircraft exterior probe |
| CN102556356B (en) * | 2010-12-06 | 2016-07-06 | 空中客车运营公司 | For being arranged on the protection device of the radar of aircraft exterior |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100512 Termination date: 20110326 |