CN211806103U

CN211806103U - Auxiliary marking device for machining aviation composite material wing body fairing

Info

Publication number: CN211806103U
Application number: CN201922391620.3U
Authority: CN
Inventors: 张体伟
Original assignee: Boeing Tianjin Composites Co Ltd
Current assignee: Boeing Tianjin Composites Co Ltd
Priority date: 2019-12-27
Filing date: 2019-12-27
Publication date: 2020-10-30
Anticipated expiration: 2029-12-27

Abstract

The utility model discloses an aviation composite material wing body fairing processing auxiliary marking device, which comprises a mounting plate, wherein a scale bar is horizontally and fixedly arranged at the top of the right side of the mounting plate, a horizontal bubble is fixedly arranged at the front side of the mounting plate, and a telescopic rod is horizontally arranged in the middle of the mounting plate in a penetrating way; the telescopic link right-hand member fixed mounting has the mark board, the slotted hole has been seted up perpendicularly in the middle part of the mark board, it has coloured marker pole to peg graft in the slotted hole, coloured marker pole top and the middle part fixed connection of pressing the lower surface of platen. The utility model discloses a cooperation according to clamp plate, compression spring and coloured mark pole is used, during the mark, presses down according to the clamp plate downwards, compresses compression spring according to the clamp plate downwards, and coloured mark pole wears out the slotted hole downwards and marks, and the mark is accomplished the back, loosens according to the clamp plate, and compression spring is owing to resume deformation and drive coloured mark pole and upwards reset, simple structure, convenient operation.

Description

Auxiliary marking device for machining aviation composite material wing body fairing

Technical Field

The utility model relates to a radome fairing processing technology field specifically is an aviation combined material wing body radome fairing processing auxiliary mark device.

Background

When the launch vehicle flies in the atmosphere, the satellite fairing is used for protecting the satellite and other effective loads so as to prevent the satellite from being influenced by harmful environments such as aerodynamic force, aerodynamic heating, sound vibration and the like. It is an important component of a launch vehicle. In the aspect of missiles, the missile is a necessary product of missile multi-warhead. During the manufacture of the fairing, it is often necessary to mark the fairing with a marking device.

However, the existing auxiliary marking device for machining the wing body fairing has the defects in the using process; 1. the conventional auxiliary marking device for machining the wing body fairing is complex in structure and inconvenient to use. 2. The existing auxiliary marking device for machining the wing body fairing often causes deviation in the machined fairing due to inaccurate marking during marking. Therefore, an auxiliary marking device for machining an aeronautical composite wing body fairing is provided.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an aviation combined material wing body radome fairing processing auxiliary mark device, through pressing the clamp plate, compression spring and coloured mark pole's cooperation is used, during the mark, press the clamp plate downwards, press the clamp plate to compress compression spring downwards, coloured mark pole is worn out the slotted hole downwards and is marked, mark completion back, loosen and press the clamp plate, compression spring is owing to resume deformation and drive coloured mark pole upwards and reset, moreover, the steam generator is simple in structure, and the operation is convenient, horizontal bubble through the mounting panel front side, whether the device is leveled convenient when the mark, avoid the crooked accuracy that influences the mark of mounting panel, and guide sliding sleeve and scale strip sliding connection through mark plate top, play the guide effect, avoid the mark plate crooked, the problem that provides in the background art has been solved.

In order to achieve the above object, the utility model provides a following technical scheme: an auxiliary marking device for machining of an aviation composite material wing body fairing comprises a mounting plate, wherein a scale bar is horizontally and fixedly mounted at the top of the right side of the mounting plate, a horizontal bubble is fixedly mounted at the front side of the mounting plate, and a telescopic rod horizontally penetrates through the middle of the mounting plate;

the telescopic link right-hand member fixed mounting has the mark board, the slotted hole has been seted up perpendicularly in the middle part of the mark board, it has coloured marker pole to peg graft in the slotted hole, coloured marker pole top and the middle part fixed connection of pressing the lower surface of platen.

As an optimized embodiment of the utility model, the telescopic link includes fixed loop bar and telescopic strut, fixed loop bar surface right side is provided with fastening screw.

As a preferred embodiment of the utility model, fixed loop bar right side is connected with telescopic strut, telescopic strut left end is pegged graft in fixed loop bar and telescopic strut right-hand member and mark board left side middle part fixed connection.

As an embodiment of the present invention, the top of the marking plate is fixedly connected with a guiding sliding sleeve, and the guiding sliding sleeve is slidably sleeved on the outside of the scale bar.

As a preferred embodiment of the utility model, press the equal fixedly connected with compression spring in the press plate lower surface left and right sides, it is two sets of compression spring bottom respectively with mark board upper surface left and right sides fixed connection.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the utility model discloses an aviation combined material wing body radome fairing processing auxiliary mark device uses through the cooperation of pressing down clamp plate, compression spring and coloured mark pole, during the mark, presses down the clamp plate, compresses compression spring according to the clamp plate downwards, and coloured mark pole wears out the slotted hole downwards and marks, and the back is accomplished in the mark, loosens and presses the clamp plate, and compression spring is owing to resume deformation and drive coloured mark pole and upwards reset, simple structure, convenient operation.

2. The utility model discloses an aviation combined material wing body radome fairing processing auxiliary mark device, through the horizontal bubble of mounting panel front side, whether the device is level is judged to the convenience when the mark, avoids the crooked accuracy that influences the mark of mounting panel, and through the direction sliding sleeve and the scale strip sliding connection at mark plate top, plays the guide effect, avoids the mark plate crooked.

Drawings

Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:

fig. 1 is a schematic overall structure diagram of the auxiliary marking device for machining the aeronautical composite material wing body fairing of the utility model;

fig. 2 is the utility model discloses aeronautical composite material wing body fairing processes auxiliary mark device's mark plate structure sketch map.

In the figure: 1 telescopic link, 2 fixed loop bars, 3 fastening screws, 4 mounting panels, 5 scale strips, 6 guide sliding sleeves, 7 marking plates, 8 telescopic supporting rods, 9 horizontal bubbles, 10 pressing plates, 11 compression springs, 12 slotted holes and 13 colored marking rods.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

In the description of the present invention, it should be noted that, unless explicitly stated or limited otherwise, the terms "mounted," "connected" and "disposed" are to be interpreted broadly, and may be, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed; the utility model discloses in provide only supply the reference with the model of electrical apparatus. For those skilled in the art, different types of electrical appliances with the same function can be replaced according to actual use conditions, and for those skilled in the art, the specific meaning of the above terms in the present invention can be understood in specific situations.

Referring to fig. 1-2, the present invention provides a technical solution: an auxiliary marking device for machining an aviation composite material wing body fairing comprises a mounting plate 4, wherein a scale bar 5 is horizontally and fixedly mounted at the top of the right side of the mounting plate 4, a horizontal bubble 9 is fixedly mounted at the front side of the mounting plate 4, and a telescopic rod 1 is horizontally arranged in the middle of the mounting plate 4 in a penetrating manner;

the right end of the telescopic rod 1 is fixedly provided with a marking plate 7, the middle of the marking plate 7 is vertically provided with a slotted hole 12, a colored marking rod 13 is inserted into the slotted hole 12, and the top of the colored marking rod 13 is fixedly connected with the middle of the lower surface of the pressing plate 10.

In this embodiment (refer to fig. 1), the telescopic rod 1 includes a fixed loop bar 2 and a telescopic supporting rod 8, and a fastening screw 3 is disposed on the right side of the surface of the fixed loop bar 2.

In this embodiment (please refer to fig. 1), the right side of the fixed loop bar 2 is connected with a telescopic strut 8, the left end of the telescopic strut 8 is inserted into the fixed loop bar 2, and the right end of the telescopic strut 8 is fixedly connected with the middle part of the left side of the marking plate 7.

In this embodiment (please refer to fig. 1), the top of the marking plate 7 is fixedly connected with a guide sliding sleeve 6, the guide sliding sleeve 6 is slidably sleeved outside the scale bar 5, and the guide sliding sleeve 6 can play a role in guiding and prevent the marking plate 7 from being inclined.

In this embodiment (see fig. 2), the left and right sides of the lower surface of the pressing plate 10 are fixedly connected with compression springs 11, the bottoms of the two sets of compression springs 11 are respectively and fixedly connected with the left and right sides of the upper surface of the marking plate 7, and the colored marking rods 13 can be conveniently reset through the compression springs 11.

It should be noted that the utility model relates to an aviation composite material wing body fairing processing auxiliary marking device, which comprises a telescopic rod 1, a fixed loop bar 2, a fastening screw 3, a mounting plate 4, a scale bar 5, a guide sliding sleeve 6, a marking plate 7, a telescopic support rod 8, a horizontal bubble 9, a pressing plate 10, a compression spring 11, a slotted hole 12, a colored marking rod 13, wherein the components are all universal standard components or components known by technicians in the field, the structure and principle of the marking device can be known by technical manuals or conventional test methods, when the aviation composite material wing body fairing processing auxiliary marking device is used, whether the device is horizontal or not is judged by observing whether the bubble in the horizontal bubble 9 is in the horizontal position, the telescopic support rod 8 is telescopic, the marking plate 7 is moved to the position to be marked by observing the scale bar 5, rotate fastening screw 3 and fix telescopic strut 8, press down again and press according to board 10, press board 10 and compress compression spring 11 downwards, coloured mark pole 13 is worn out slotted hole 12 downwards and is marked, and the back is accomplished in the mark, loosens and presses board 10, and compression spring 11 is owing to resume deformation and drive coloured mark pole 13 and upwards reset, simple structure, convenient operation, the result of use is comparatively ideal.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims

1. The utility model provides an aviation combined material wing body radome fairing processing auxiliary mark device, includes mounting panel (4), its characterized in that: a scale strip (5) is horizontally and fixedly installed at the top of the right side of the installation plate (4), a horizontal bubble (9) is fixedly installed at the front side of the installation plate (4), and a telescopic rod (1) is horizontally arranged in the middle of the installation plate (4) in a penetrating mode;

the telescopic rod is characterized in that a marking plate (7) is fixedly installed at the right end of the telescopic rod (1), a slotted hole (12) is vertically formed in the middle of the marking plate (7), a colored marking rod (13) is inserted into the slotted hole (12), and the top of the colored marking rod (13) is fixedly connected with the middle of the lower surface of the pressing plate (10).

2. The aeronautical composite material wing body fairing processing auxiliary marking device according to claim 1, characterized in that: the telescopic rod (1) comprises a fixed sleeve rod (2) and a telescopic supporting rod (8), and a fastening screw (3) is arranged on the right side of the surface of the fixed sleeve rod (2).

3. The aeronautical composite material wing body fairing processing auxiliary marking device of claim 2, wherein: the right side of the fixed loop bar (2) is connected with a telescopic supporting rod (8), the left end of the telescopic supporting rod (8) is inserted into the fixed loop bar (2), and the right end of the telescopic supporting rod (8) is fixedly connected with the middle part of the left side of the marking plate (7).

4. The aeronautical composite material wing body fairing processing auxiliary marking device according to claim 1, characterized in that: the top of the marking plate (7) is fixedly connected with a guide sliding sleeve (6), and the guide sliding sleeve (6) is slidably sleeved on the outer side of the scale bar (5).

5. The aeronautical composite material wing body fairing processing auxiliary marking device according to claim 1, characterized in that: the left side and the right side of the lower surface of the pressing plate (10) are fixedly connected with compression springs (11), and the bottoms of the two sets of compression springs (11) are fixedly connected with the left side and the right side of the upper surface of the marking plate (7) respectively.