CN209681240U - Radome fairing drilling jig tool on F10K missile launcher - Google Patents
Radome fairing drilling jig tool on F10K missile launcher Download PDFInfo
- Publication number
- CN209681240U CN209681240U CN201920516644.4U CN201920516644U CN209681240U CN 209681240 U CN209681240 U CN 209681240U CN 201920516644 U CN201920516644 U CN 201920516644U CN 209681240 U CN209681240 U CN 209681240U
- Authority
- CN
- China
- Prior art keywords
- radome fairing
- imitative type
- liner
- upper radome
- drill jig
- 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
Radome fairing drilling jig tool on F10K missile launcher, it includes the imitative type drill jig (1) for each boring sites in curing cooperation of multiple and upper radome fairing being successively arranged along upper radome fairing front-rear direction, the connecting plate (2) and liner (3) of multiple each drill jigs of connection, one group of guide hole corresponding with upper radome fairing mounting hole is had on each imitative type drill jig (1), imitative type drill jig (1) positioned at front end is equipped with one and encloses upper radome fairing front end positive stop lug boss (4), the positioning chuck (5) being used cooperatively with upper radome fairing front end limiting slot is respectively equipped in the two side walls of liner (3) front end.The utility model advantage is: quickly can carry out positioning and clamping to upper radome fairing, by imitative type drill jig positioning, can quickly drill to each position of upper radome fairing.
Description
Technical field
The utility model relates to clamp arts, and in particular to radome fairing drilling jig tool on F10K missile launcher.
Background technique
Currently, radome fairing is U-shaped cover on F10K missile launcher, U-shaped cover front end face is vertical plane, and U-shaped cover rear end face is
Inclined surface, the bottom surface of U-shaped cover front end extreme direction backward by arc towards horizontal plane successively gradual change, positioned at two of U-shaped cover front end
Front end limiting slot is had on side plate, multiple groups mounting hole is had on the bottom surface of U-shaped cover and two side plates, for being fixed on
On launcher, due to being in shaped face upper opening, and the quantity in hole is more, how to carry out positioning to workpiece and fast and accurately exist
It is current urgent problem that drilling is carried out on each face.
Utility model content
The purpose of this utility model is aiming at currently, radome fairing is U-shaped cover, U-shaped cover front end on F10K missile launcher
Face is vertical plane, and U-shaped cover rear end face is inclined surface, U-shaped cover front end backward extreme direction bottom surface by arc towards horizontal plane successively
Gradual change has front end limiting slot on two side plates of U-shaped cover front end, distinguishes on the bottom surface of U-shaped cover and two side plates
It is provided with multiple groups mounting hole, for being fixed on launcher, due to being in shaped face upper opening, and the quantity in hole is more, how to work
Part carries out positioning and fast and accurately carrying out on each face drilling being current urgent problem, and provides F10K guided missile
Radome fairing drilling jig tool on launcher.
The utility model includes that the multiple and each boring sites in curing of upper radome fairing being successively arranged along upper radome fairing front-rear direction is matched
The connecting plate and liner of the imitative type drill jig, each drill jig of multiple connections that close have one group and upper radome fairing on each imitative type drill jig
The corresponding guide hole of mounting hole, the imitative type drill jig positioned at front end are equipped with one and enclose upper radome fairing front end positive stop lug boss, be located at interior
It serves as a contrast and is respectively equipped with the positioning chuck being used cooperatively with upper radome fairing front end limiting slot in the two side walls of front end.
Liner front end is provided with the slot being used cooperatively with upper radome fairing front end positive stop lug boss.
Two imitative type drill jigs positioned at upper radome fairing tail end are welded part.
The height of liner is less than the height of upper radome fairing side plate, is arcwall face at the top of liner.
The height for positioning chuck is not more than the thickness of upper radome fairing side plate.
It is connected between imitative type drill jig and connecting plate by screw rod.
The utility model advantage is: positioning and clamping quickly can be carried out to upper radome fairing, be positioned by imitative type drill jig,
It can quickly drill to each position of upper radome fairing.
Detailed description of the invention
Fig. 1 is the utility model structure diagram.
Fig. 2 is the utility model decomposing state structural schematic diagram.
Fig. 3 is Fig. 2 partial enlargement structural representation.
Specific embodiment
As shown in the picture, radome fairing is U-shaped cover on the utility model, and U-shaped cover front end face is vertical plane, U-shaped cover rear end face
For inclined surface, the bottom surface of U-shaped cover front end extreme direction backward by arc towards horizontal plane successively gradual change, positioned at the two of U-shaped cover front end
Front end limiting slot is had on a side plate, has multiple groups mounting hole on the bottom surface of U-shaped cover and two side plates；Drilling jig tool
It is the imitative type drill jig 1 of each boring sites in curing cooperation of multiple and upper radome fairing including being successively arranged along upper radome fairing front-rear direction, multiple
The connecting plate 2 and liner 3 of each drill jig are connected, one group is had on each imitative type drill jig 1 and corresponding with upper radome fairing mounting hole is drawn
Guide hole, the imitative type drill jig 1 positioned at front end is equipped with one and encloses upper radome fairing front end positive stop lug boss 4, positioned at two of 3 front end of liner
The positioning chuck 5 being used cooperatively with upper radome fairing front end limiting slot is respectively equipped on side wall.
3 front end of liner is provided with the slot being used cooperatively with upper radome fairing front end positive stop lug boss 4.
Two imitative type drill jigs 1 positioned at upper radome fairing tail end are welded part.
The height of liner 3 is less than the height of upper radome fairing side plate, is arcwall face at the top of liner 3.
The height for positioning chuck 5 is not more than the thickness of upper radome fairing side plate.
It is connected between imitative type drill jig 1 and connecting plate 2 by screw rod.
Working method and principle: having guide hole corresponding with upper radome fairing on each imitative type drill jig 1, liner 3 is fixed
On the table, multiple imitative type drill jigs 1 are in turn connected into an entirety by connecting plate 2, and upper radome fairing covers on liner 3,
Upper radome fairing front end limiting slot carries out position with the positioning cooperation of chuck 5 and fixes, and then the imitative type drill jig 1 connected is covered on upper whole
On stream cover, the imitative type drill jig 1 of front end is cooperated by upper radome fairing front end positive stop lug boss 4 and liner 3, makes imitative type drill jig 1 and upper
Radome fairing alignment, successively drills to each position of upper radome fairing by electronic hand drill, and drilling when only needs drill bit to stretch
Enter into the guide hole of each imitative type drill jig 1, guide hole plays positioning action.It is arcwall face at the top of liner 3, is rectified in convenience
Cover is quickly inserted on liner 3.
Claims (6)
- Radome fairing drilling jig tool on 1.F10K missile launcher, it is characterised in that it includes successively setting along upper radome fairing front-rear direction The imitative type drill jig (1) of each boring sites in curing cooperation of the multiple and upper radome fairing having, multiple connecting plates (2) and liner for connecting each drill jig (3), one group of guide hole corresponding with upper radome fairing mounting hole, the imitative type positioned at front end are had on each imitative type drill jig (1) Drill jig (1) is equipped with one and encloses upper radome fairing front end positive stop lug boss (4), is located in the two side walls of liner (3) front end and is respectively equipped with The positioning chuck (5) being used cooperatively with upper radome fairing front end limiting slot.
- 2. radome fairing drilling jig tool on F10K missile launcher according to claim 1, it is characterised in that liner (3) front end It is provided with the slot being used cooperatively with upper radome fairing front end positive stop lug boss (4).
- 3. radome fairing drilling jig tool on F10K missile launcher according to claim 1, it is characterised in that be located at upper rectification The imitative type drill jig (1) of two of cover tail end is welded part.
- 4. radome fairing drilling jig tool on F10K missile launcher according to claim 1, it is characterised in that the height of liner (3) Degree is less than the height of upper radome fairing side plate, is arcwall face at the top of liner (3).
- 5. radome fairing drilling jig tool on F10K missile launcher according to claim 1, it is characterised in that positioning chuck (5) Height be not more than upper radome fairing side plate thickness.
- 6. radome fairing drilling jig tool on F10K missile launcher according to claim 1, it is characterised in that imitative type drill jig (1) It is connected between connecting plate (2) by screw rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920516644.4U CN209681240U (en) | 2019-04-17 | 2019-04-17 | Radome fairing drilling jig tool on F10K missile launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920516644.4U CN209681240U (en) | 2019-04-17 | 2019-04-17 | Radome fairing drilling jig tool on F10K missile launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209681240U true CN209681240U (en) | 2019-11-26 |
Family
ID=68607884
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920516644.4U Expired - Fee Related CN209681240U (en) | 2019-04-17 | 2019-04-17 | Radome fairing drilling jig tool on F10K missile launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209681240U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115164654A (en) * | 2022-06-06 | 2022-10-11 | 西北工业大学 | Experimental auxiliary device that water was gone into in area angle of attack of navigation ware |
-
2019
- 2019-04-17 CN CN201920516644.4U patent/CN209681240U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115164654A (en) * | 2022-06-06 | 2022-10-11 | 西北工业大学 | Experimental auxiliary device that water was gone into in area angle of attack of navigation ware |
| CN115164654B (en) * | 2022-06-06 | 2023-10-13 | 西北工业大学 | Auxiliary device for water inlet test of aircraft with attack angle |
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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: 20191126 |