CN218317389U - Novel left horizontal tail type frame frock - Google Patents
Novel left horizontal tail type frame frock Download PDFInfo
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- CN218317389U CN218317389U CN202222499822.1U CN202222499822U CN218317389U CN 218317389 U CN218317389 U CN 218317389U CN 202222499822 U CN202222499822 U CN 202222499822U CN 218317389 U CN218317389 U CN 218317389U
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- clamping piece
- type frame
- horizontal tail
- left horizontal
- tail type
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Abstract
A novel left horizontal tail type frame tool comprises a first clamping piece, a second clamping piece, a fastener, a clamping plate assembly, a positioning device and a horizontal dotter; one end of the fastener is connected to the first clamping piece, and the other end of the fastener is connected to the second clamping piece; a fused accommodating space for accommodating the left horizontal tail type frame is formed between the first clamping piece and the second clamping piece; the clamping plate assembly is connected to the first clamping plate; the positioning device is connected to the first clamping sheet; the positioning device comprises a positioning plate assembly, a first lifting rudder shaft positioner, a back beam metal joint positioner, a second lifting rudder shaft positioner and a skin limiter; locating plate subassembly, lift steering shaft's locator, back beam metal joint locator, lift steering shaft locator and covering stopper all connect on first splint, and left horizontal tail type frame frock uses cardboard subassembly, a plurality of locator and stopper to fix a position it, and the locating position is nimble changeable, and the location is more accurate, makes things convenient for the workman to assemble left horizontal tail type frame.
Description
Technical Field
The utility model belongs to the technical field of left horizontal tail anchor clamps, especially, relate to a novel left horizontal tail type frame frock.
Background
The horizontal tail is a short term for a horizontal tail, is one of the main large parts of an airplane, and is generally horizontally installed on the tail. The front half part of the airplane is immovable and is a horizontal stabilizing surface for pitching stabilization, and the rear half part is an elevator for controlling the airplane to ascend and descend and is connected with the airplane by a hinge.
However, in the process of aircraft assembly, the positioning device used on the left horizontal tail type frame tool is inaccurate, so that a large number of left horizontal tail positions can be debugged by workers in the assembly process, the assembly efficiency is low, the cost is increased, and the development of company careers is not facilitated.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model aims at providing a novel left horizontal tail type frame frock to solve and exist among the prior art, in aircraft assembling process, the positioner who uses above the horizontal tail type frame frock of a left side is inaccurate, leads to the workman to debug the position of horizontal tail in a large number in assembling process, and assembly efficiency is lower, and the cost is improved, is unfavorable for the technical problem of company's career development.
In order to achieve the above purpose, the technical scheme of the utility model is realized like this:
a novel left horizontal tail type frame tool comprises a first clamping piece, a second clamping piece, a fastener, a clamping plate assembly, a positioning device and a horizontal dotter;
one end of the fastener is connected to the first clamping piece, and the other end of the fastener is connected to the second clamping piece;
a melting accommodating space for accommodating the left horizontal tail type frame is formed between the first clamping piece and the second clamping piece;
the clamping plate assembly is connected to the first clamping plate;
the positioning device is connected to the first clamping sheet;
the positioning device comprises a positioning plate assembly, a first elevator rudder shaft positioner, a back beam metal joint positioner, a second elevator rudder shaft positioner and a skin limiter;
the positioning plate assembly, the lifting rudder shaft positioner, the back beam metal joint positioner, the lifting rudder shaft positioner and the skin limiter are all connected to the first clamping piece;
the horizontal dotting devices are connected to the periphery of the first clamping piece, and the number of the horizontal dotting devices is multiple.
Furthermore, the clamping plate assembly comprises a profile clamping plate, a beam web positioner and a bent handle plug pin;
one end of the bent handle bolt passes through the outline clamping plate and is connected to the first clamping piece.
Further, the locating plate assembly further comprises a first rib locating plate, a second rib locating plate and a third rib locating plate.
Furthermore, a first hoisting piece is arranged on the first clamping piece, and a second hoisting piece is arranged on the second clamping piece.
Compared with the prior art, the utility model discloses a novel left horizontal tail type frame frock has following advantage:
(1) The utility model discloses a left horizontal tail type frame frock uses cardboard subassembly, a plurality of locator and stopper to fix a position it, and the locating position is nimble changeable, fixes a position more accurately, makes things convenient for the workman to assemble left horizontal tail type frame.
(2) The clamping plate component of the utility model can strengthen the positioning of the left horizontal tail type frame on the tooling, and the lower end of the curved handle bolt passes through the outline clamping plate and is fixed on the first clamping plate, so as to prevent the outline clamping plate from shaking; still be equipped with the web locator on the plate body of appearance profile cardboard, detect whether the position of web is accurate, guarantee that the position of left horizontal tail type frame on the frock is accurate, improve the efficiency of assembly.
(3) The utility model discloses a locating plate subassembly includes three locating plate, and left horizontal tail type frame position about the frock can be adjusted to first rib locating plate and third rib locating plate, fixes a position left horizontal tail type frame, and is same, and left horizontal tail type frame position around in the frock can be adjusted to second rib locating plate, fixes a position left horizontal tail type frame for left horizontal tail type frame is more accurate in the position on first clamping piece, is convenient for assemble.
(4) The utility model discloses a all be equipped with rings on two clips, perhaps lifting hook all is equipped with a plurality of pieces that lift on every clip, makes things convenient for workman's transportation clamping piece, can also lift by crane convenient and fast when two clamping piece centre gripping aircraft tails.
Drawings
The accompanying drawings, which form a part of the present disclosure, are included to provide a further understanding of the present disclosure, and are incorporated in and constitute a part of this specification, illustrate embodiments of the present disclosure and together with the description serve to explain the present disclosure. In the drawings:
fig. 1 is a schematic structural view of a novel left horizontal tail type frame fixture according to an embodiment of the present invention;
fig. 2 is a schematic structural diagram of a first clamping piece according to an embodiment of the present invention.
Description of the reference numerals:
100-a first clip; 101-a first lifting member;
200-a second clip; 201-a second lifting element;
300-a fastener; 400-a card board assembly;
401-outline cardboard; 402-web locator;
403-bent handle bolt; 500-a positioning device;
501-positioning plate assembly; 502-a first elevator rudder shaft positioner;
503-back beam metal joint locator; 504-a second elevator rudder shaft positioner;
505-skin stops; 506-a first rib positioning plate;
507-a second rib positioning plate; 508-third rib positioning plate.
600-horizontal dotter.
Detailed Description
It should be noted that, in the present invention, the embodiments and features of the embodiments may be combined with each other without conflict.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "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 used merely for convenience of description and for 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. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected" and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
The present invention will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
As shown in fig. 1-2, the utility model provides a novel left horizontal tail type frame tool, which comprises a first clamping piece 100, a second clamping piece 200, a fastener 300, a clamping plate assembly 400, a positioning device 500 and a horizontal dotter 600;
one end of the fastener 300 is connected to the first jaw 100, and the other end of the fastener 300 is connected to the second jaw 200;
a melting accommodating space for accommodating the left horizontal tail type frame is formed between the first clamping piece 100 and the second clamping piece 200;
the card assembly 400 is attached to the first clip 100;
the positioning device 500 is connected to the first clip 100;
the positioning device 500 comprises a positioning plate assembly 501, a first elevator rudder shaft positioner 502, a back beam metal joint positioner 503, a second elevator rudder shaft positioner 504 and a skin limiter 505;
the positioning plate assembly 501, the positioner 502 of the elevator rudder shaft, the metal joint positioner 503 of the back beam, the positioner 504 of the elevator rudder shaft and the skin limiter 505 are all connected to the first clip 100;
the horizontal dotter 600 is attached to the periphery of the first jaw 100, and the number of the horizontal dotters 600 is plural.
In an embodiment of the present invention, as shown in fig. 1 and fig. 2, the first clamping piece 100 and the second clamping piece 200 are fixed by a plurality of fasteners, and a melted accommodating space for accommodating the left horizontal tail frame is formed between the two clamping pieces, so that the left horizontal tail frame can be conveniently placed for assembly.
Locating plate subassembly 501 on positioner 500, the locator 502 of lift rudder axle, back beam metal joint locator 503, lift rudder axle locator 504 and covering stopper 505 are all installed on first clamping piece 100, contain a plurality of locating plates in the locating plate subassembly 501 and fix a position left horizontal tail type frame, and lift rudder axle's locator 502, locators such as back beam metal joint locator 503 and lift rudder axle locator 504 carry out accurate location to left horizontal tail type frame, guarantee that left horizontal tail type frame assembles quick accuracy, covering stopper 505 can restrict left horizontal tail type frame and take place the displacement at two clamping pieces, it is quick convenient to install, improve assembly efficiency.
A plurality of horizontal dotters 600 are installed on the periphery of the first jaw 100 to facilitate marking on the left horizontal tail type frame.
More preferably, the card assembly 400 includes a contoured card 401, a web locator 402, and a cranked latch 403;
one end of a bent handle latch 403 is connected to the first clip 100 through the contoured clip 401.
In an embodiment of the present invention, as shown in fig. 1 and fig. 2, the clamping plate assembly 400 can enhance the positioning of the left horizontal tail frame on the tooling, and the lower end of the curved handle bolt 403 passes through the outline clamping plate 401 and is fixed on the first clamping plate 100, so as to prevent the outline clamping plate 401 from shaking; and a beam web positioner 402 is further arranged on the plate body of the contour clamping plate 401, so that whether the position of a beam web is accurate or not is detected, the position of the left horizontal tail type frame on the tool is accurate, and the assembly efficiency is improved.
More preferably, the positioning plate assembly 501 further includes a first rib positioning plate 506, a second rib positioning plate 507 and a third rib positioning plate 508.
The utility model discloses an embodiment, as shown in fig. 1, fig. 2, locating plate subassembly 501 includes three locating plate, left horizontal tail type frame left and right sides position on the frock can be adjusted to first rib locating plate 506 and third rib locating plate 508, fix a position left horizontal tail type frame, and is same, second rib locating plate 507 can adjust left horizontal tail type frame front and back position on the frock, fixes a position left horizontal tail type frame for left horizontal tail type frame is more accurate in the position on first clamping piece 100, the assembly of being convenient for.
More preferably, the first jaw 100 is provided with a first lifting member 101, and the second jaw 200 is provided with a second lifting member 201.
The utility model discloses an in the embodiment, as shown in fig. 1, fig. 2, all be equipped with rings on two clips, perhaps play the lifting hook, all be equipped with a plurality of pieces that lift on every clip, make things convenient for workman's transportation clamping piece, can also lift by crane convenient and fast when two clamping piece centre gripping aircraft tails.
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (4)
1. The utility model provides a novel left horizontal tail type frame frock which characterized in that: comprises a first clamping piece (100), a second clamping piece (200), a fastener (300), a clamping plate component (400), a positioning device (500) and a horizontal dotter (600);
one end of the fastener (300) is connected to the first jaw (100), and the other end of the fastener (300) is connected to the second jaw (200);
a melting accommodating space for accommodating the left horizontal tail type frame is formed between the first clamping piece (100) and the second clamping piece (200);
the card assembly (400) is connected to the first clip (100);
the positioning device (500) is connected to the first clip (100);
the positioning device (500) comprises a positioning plate assembly (501), a first elevator steering shaft positioner (502), a back beam metal joint positioner (503), a second elevator steering shaft positioner (504) and a skin limiter (505);
the positioning plate assembly (501), the elevator shaft positioner (502), the back beam metal joint positioner (503), the elevator shaft positioner (504) and the skin limiter (505) are all connected to the first clamping piece (100);
the horizontal dotting devices (600) are connected to the periphery of the first clamping piece (100), and the number of the horizontal dotting devices (600) is multiple.
2. The novel left horizontal tail type frame tool according to claim 1, characterized in that: the clamping plate assembly (400) comprises a contour clamping plate (401), a beam web positioner (402) and a bent handle plug pin (403);
one end of the bent handle bolt (403) penetrates through the outline clamping plate (401) to be connected to the first clamping piece (100).
3. The novel left horizontal tail type frame tool according to claim 2, characterized in that: the locating plate assembly (501) further comprises a first rib locating plate (506), a second rib locating plate (507), and a third rib locating plate (508).
4. The novel left horizontal tail type frame tool according to claim 3, characterized in that: the first clamping piece (100) is provided with a first hoisting piece (101), and the second clamping piece (200) is provided with a second hoisting piece (201).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222499822.1U CN218317389U (en) | 2022-09-21 | 2022-09-21 | Novel left horizontal tail type frame frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222499822.1U CN218317389U (en) | 2022-09-21 | 2022-09-21 | Novel left horizontal tail type frame frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218317389U true CN218317389U (en) | 2023-01-17 |
Family
ID=84819389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222499822.1U Active CN218317389U (en) | 2022-09-21 | 2022-09-21 | Novel left horizontal tail type frame frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218317389U (en) |
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2022
- 2022-09-21 CN CN202222499822.1U patent/CN218317389U/en active Active
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