CN208149641U - A kind of device being easily installed aircraft side siding sash assembly - Google Patents
A kind of device being easily installed aircraft side siding sash assembly Download PDFInfo
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- CN208149641U CN208149641U CN201820481017.7U CN201820481017U CN208149641U CN 208149641 U CN208149641 U CN 208149641U CN 201820481017 U CN201820481017 U CN 201820481017U CN 208149641 U CN208149641 U CN 208149641U
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Abstract
The utility model relates to a kind of devices for being easily installed aircraft side siding sash assembly, the shape of described device is cross, the horizontal direction of the cross is longer than vertical direction, both horizontally and vertically, at equidistant 4 points at cross center, it is provided with contact (3), the contact (3) is at a distance from cross center and the radius of the circle viewing glass (2) of aircraft side walls is almost the same, indicates equidistant groove on the cross of the contact (3) nearby.The utility model utilizes the cross rack device location window frame component with contact, wherein the position of contact and the circumferential size of viewing glass are almost the same, the device is placed on round viewing glass, the center of circle can be found according to cross center is accurate by being had good positioning using contact, and then determine whether the placement of sash assembly surrounding is uniform, to go on smoothly installation.
Description
Technical field
The utility model relates to technique for aircraft composite inner trim panels to manufacture installing area, more particularly to installation aircraft side siding
A kind of device positioned when sash assembly.
Background technique
It requires to use composite material inner trim panels in aircraft cabin, and fuselage side wall has round viewing glass, for the ease of seeing
It examines and combines beauty, the place that Circular glass is installed on sidewall paneling is mounted with sash assembly.But due to Circular glass and window frame
Component has a circle, and justifying viewing glass is to be mounted in advance on aircraft side walls skeleton, not when installing sash assembly
Confirm the center of circle well, cause sash assembly often to position inaccurate, the circle of sash assembly can not be completely right with the circle of circle viewing glass
It answers, in-site installation positioning relies solely on people's naked eyes and positions, and deviation inevitably occurs, therefore seek the device that can be positioned, and guarantees window
It is not in relatively large deviation in frame component mounting process.
It is most initially to be positioned by human eye, a people holds sash assembly and is placed on sidewall paneling circle viewing glass, separately
In aircraft cabin, sight adjusts height of sighting line, finds circle center and positioned perpendicular to sidewall paneling at outer people station.Due to every
Personal view is different, and such method installation sash assembly is inaccurate.Later it is envisioned that being positioned using infrared laser, purchase
One can project the infrared laser device of cross.Device bad fixation is found when on-the-spot test uses, and is relied solely on hand and is taken
Not in one plane, the cross laser positioning easy deviation of light is found for easy shaking, next circle viewing glass and sash assembly
The center of circle be still not allowed, even if finding the center of circle, it is also desirable to visually left and right up and down several sides it is whether uniform, be positioned such that or have partially
Difference, and the manpower needed is also more, is not easy to operate.
Utility model content
In order to solve the problems, such as to encounter in above-mentioned production process, the utility model one kind is easily installed aircraft side siding window frame
The device of component accurate can find the center of circle using the device of the utility model, and sash assembly is accurately positioned, smoothly into
Row installation.
The above-mentioned purpose of the utility model is achieved through the following technical solutions:
A kind of device being easily installed aircraft side siding sash assembly, the shape of described device are cross, the cross
The horizontal direction of frame is longer than vertical direction, both horizontally and vertically, equidistant 4 points with cross center
Place, is respectively arranged with contact, and the contact is at a distance from cross center and the radius base of the circle viewing glass of aircraft side walls
This is consistent, and equidistant groove is indicated on the cross of the near contacts.
In addition, the position of the contact is adjustable, so as to adjust the contact at a distance from cross center, with suitable
Answer different size of round viewing glass.
In addition, being additionally provided with the square slider that can be slided in the horizontal direction in one end of cross horizontal direction.It moves left and right
Sliding block guarantees to block one side of sidewall paneling, can guarantee that whole device with the edge of sidewall paneling is vertical in this way.
Described device is made of light material, preferably aluminum material.
Compared with prior art, the utility model utilizes the cross rack device location window frame component of the contact with there are four,
In four contacts position and viewing glass circumferential size it is almost the same, which is placed on round viewing glass, benefit
The center of circle can be found according to cross center is accurate by being had good positioning with four contacts, and then determine that sash assembly surrounding is placed
Whether uniformly, to go on smoothly installation.
Detailed description of the invention
Fig. 1 is window frame for aircraft component scheme of installation;
Fig. 2 is the schematic diagram according to the device for being easily installed aircraft side siding sash assembly of the utility model.
Specific embodiment
Below with reference to the accompanying drawings, in conjunction with specific embodiments, aircraft side siding sash assembly is easily installed to the utility model
Device be described in further detail.
Fig. 1 is window frame for aircraft component scheme of installation.As shown, sash assembly is mounted on the sidewall paneling of fuselage, it is right
It should be in the circle viewing glass installed on side wall.
Fig. 2 schematically illustrates the device for being easily installed aircraft side siding sash assembly according to the utility model.As schemed
Show, the shape of described device is cross, and the horizontal direction of the cross is longer than vertical direction, in the horizontal direction and Vertical Square
To, at equidistant 4 points at cross center, be respectively arranged with contact 3, the contact 3 and cross center away from
Radius from the circle viewing glass 2 with aircraft side walls is almost the same, indicates on the cross near the contact 3 at equal intervals
Groove.In addition, the position of the contact 3 is adjustable, so as to adjust the contact at a distance from cross center, to adapt to
Different size of round viewing glass 2.
In addition, being additionally provided with the square slider 4 that can be slided in the horizontal direction in one end of cross horizontal direction.Left and right is moved
Movable slider 4 guarantees to block one side of sidewall paneling, can guarantee that whole device with the edge of sidewall paneling is vertical in this way.
Described device is made of light material, preferably aluminum material.
When using the device, sash assembly 1 is put into sidewall paneling window frame, then there are four the cross of contact is rack-mounted by band
It puts into round 2 surface of viewing glass, so that contact 3 is contacted circle 2 surface of viewing glass, positioned using the device, observe contact 3
The circumferential size of the scale of surrounding, the position and viewing glass that make contact 3 is almost the same, guarantees that cross center and circle are observed
2 center of glass pane is overlapped, to make contact 3 to good round observation window 2.Sliding block 4 is moved left and right to the one side for guaranteeing to block sidewall paneling,
Can guarantee in this way whole device with the edge of sidewall paneling be it is vertical, adjust the position of sash assembly 1, guarantee cross or more
The distance of left and right is uniform, ensures that sash assembly installation is uniform in this way.
Claims (4)
1. a kind of device for being easily installed aircraft side siding sash assembly, the shape of described device is cross, the cross
Horizontal direction it is longer than vertical direction, both horizontally and vertically, at a distance from cross center at identical 4 points,
It is respectively arranged with contact (3), the contact (3) is at a distance from cross center and the circle viewing glass (2) of aircraft side walls
Radius is almost the same, indicates equidistant groove on the cross of the contact (3) nearby.
2. device described in accordance with the claim 1, wherein the position of the contact (3) is adjustable.
3. device described in accordance with the claim 1, wherein be additionally provided with to slide in the horizontal direction in one end of cross horizontal direction
Dynamic square slider (4).
4. device described in accordance with the claim 1, wherein described device is made of aluminum material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201820481017.7U CN208149641U (en) | 2018-04-04 | 2018-04-04 | A kind of device being easily installed aircraft side siding sash assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201820481017.7U CN208149641U (en) | 2018-04-04 | 2018-04-04 | A kind of device being easily installed aircraft side siding sash assembly |
Publications (1)
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CN208149641U true CN208149641U (en) | 2018-11-27 |
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CN201820481017.7U Active CN208149641U (en) | 2018-04-04 | 2018-04-04 | A kind of device being easily installed aircraft side siding sash assembly |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109949245A (en) * | 2019-03-25 | 2019-06-28 | 长沙智能驾驶研究院有限公司 | Cross laser detects localization method, device, storage medium and computer equipment |
CN110239738A (en) * | 2019-05-29 | 2019-09-17 | 陕西飞机工业(集团)有限公司 | A kind of Aircraft inner decoration plate window frame benchmark alignment device and method |
-
2018
- 2018-04-04 CN CN201820481017.7U patent/CN208149641U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109949245A (en) * | 2019-03-25 | 2019-06-28 | 长沙智能驾驶研究院有限公司 | Cross laser detects localization method, device, storage medium and computer equipment |
CN109949245B (en) * | 2019-03-25 | 2021-04-16 | 长沙智能驾驶研究院有限公司 | Cross laser detection positioning method and device, storage medium and computer equipment |
CN110239738A (en) * | 2019-05-29 | 2019-09-17 | 陕西飞机工业(集团)有限公司 | A kind of Aircraft inner decoration plate window frame benchmark alignment device and method |
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GR01 | Patent grant | ||
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CP03 | Change of name, title or address |
Address after: 723213 Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province Patentee after: Shaanxi Aircraft Industry Co.,Ltd. Address before: 723213 cuijiashan Town, Hanzhong City, Shaanxi Province Patentee before: Shaanxi Aircraft INDUSTRY(GROUP) Co.,Ltd. |