CN220410898U - Auxiliary positioning tool for angle sensor for outer flap rocker arm of airplane - Google Patents
Auxiliary positioning tool for angle sensor for outer flap rocker arm of airplane Download PDFInfo
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- CN220410898U CN220410898U CN202321841503.2U CN202321841503U CN220410898U CN 220410898 U CN220410898 U CN 220410898U CN 202321841503 U CN202321841503 U CN 202321841503U CN 220410898 U CN220410898 U CN 220410898U
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- outer flap
- rocker arm
- mounting plate
- angle sensor
- mounting
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- 238000009434 installation Methods 0.000 abstract description 15
- 238000005259 measurement Methods 0.000 abstract description 5
- 238000013461 design Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
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Abstract
The utility model discloses an angle sensor auxiliary positioning tool for an outer flap rocker arm of an airplane, which is characterized in that a first mounting assembly can rotationally connect a mounting plate to the outer flap rocker arm so that a first positioning piece can be abutted against the side wall of the outer flap rocker arm, and the first mounting assembly can lock or unlock the relative positions of the mounting plate and the outer flap rocker arm; the second installation component can rotationally connect the connecting joint to the installation plate so that the connecting joint can abut against the second positioning piece, and the second installation component can lock or unlock the relative positions of the installation plate and the connecting joint; when the first positioning piece is propped against the side wall of the outer flap rocker arm, the connecting joint is propped against the second positioning piece, the first connecting part and the second connecting part are aligned, and the first connecting part is used for being connected with the second connecting part. The assembly position of the connecting joint can be accurately and efficiently determined, the positioning and assembly efficiency of the angle sensor is improved, and the measurement accuracy of the angle sensor is improved.
Description
Technical Field
The utility model relates to the technical field of aircraft assembly, in particular to an auxiliary positioning tool for an angle sensor for an aircraft outer flap rocker arm.
Background
The angle sensor is a measuring instrument for measuring the inclination angle of an object, outputs corresponding electric signals by detecting the inclination degree of the object, and has the advantages of high detection precision, wide application range, long service life, easy maintenance and the like. In the prior art, an angle sensor on an outer flap rocker arm is usually connected to the outer flap rocker arm through a connecting joint, so that the positioning and mounting accuracy of the connecting joint directly influences the accuracy of measured data of the angle sensor, and particularly, the warning of the measured data of the angle sensor of an aircraft in a route operation stage is mostly derived from larger positioning errors of the connecting joint. Therefore, in order to ensure the measurement accuracy of the angle sensor on the outer flap rocker arm of the aircraft, the false alarm caused by large data error measured by the angle sensor is avoided when the aircraft flies, and the improvement of the positioning accuracy of the angle sensor in the assembly process is very important.
At present, a manual scribing mode is generally adopted to position the installation position of the connecting joint of the angle sensor in the prior art, and the positioning mode has large positioning error and low positioning efficiency, so that the assembly efficiency of the angle sensor is low, and the measurement accuracy of the angle sensor is low.
Disclosure of Invention
The utility model aims to provide an auxiliary positioning tool for an angle sensor for an outer flap rocker arm of an aircraft, which is used for solving the problems of high positioning error, low positioning efficiency, low assembly efficiency of the angle sensor and low measurement accuracy of the angle sensor in the prior art by positioning the installation position of a connecting joint of the angle sensor in a manual scribing mode.
To achieve the purpose, the utility model adopts the following technical scheme:
the utility model provides an angle sensor auxiliary positioning frock for outer flap rocking arm of aircraft for assemble angle sensor in outer flap rocking arm, angle sensor includes angle sensor body, attach fitting and connecting rod, angle sensor body detachable connect in attach fitting, connecting rod fixed connection in outer flap rocking arm, it includes:
the mounting plate, the first mounting assembly and the first positioning piece are arranged on the mounting plate, the first mounting assembly can rotationally connect the mounting plate to the outer flap rocker arm so that the first positioning piece can be abutted against the side wall of the outer flap rocker arm, and the first mounting assembly can lock or unlock the relative positions of the mounting plate and the outer flap rocker arm;
the second installation component can rotationally connect the connecting joint to the installation plate so that the connecting joint can be abutted against the second positioning piece, and the second installation component can lock or unlock the relative positions of the installation plate and the connecting joint;
when the first positioning piece is propped against the side wall of the outer flap rocker arm, the connecting joint is propped against the second positioning piece, a first connecting part of the connecting joint is aligned with a second connecting part of the connecting rod, and the first connecting part is used for being connected with the second connecting part.
Preferably, the mounting plate is provided with a first mounting surface and a second mounting surface, the first mounting assembly and the first positioning piece are distributed on the first mounting surface at intervals, the second mounting assembly and the second positioning piece are distributed on the second mounting surface at intervals, and the first mounting surface and the second mounting surface are parallel and distributed along the thickness direction of the mounting plate at intervals.
Preferably, the first mounting assembly includes a first connector passing through the mounting plate and the outer flap rocker arm and in threaded connection with a first nut.
Preferably, the first mounting assembly further comprises a first bushing and a first adjusting gasket, the first bushing is inserted into the mounting plate, and the first connecting piece sequentially penetrates through the first bushing, the mounting plate, the outer flap rocker arm and the first adjusting gasket and is in threaded connection with the first nut.
Preferably, the first connector and/or the first nut is provided with a first handle.
Preferably, the second mounting assembly includes a second connector and a second nut, and the second connector passes through the mounting plate and the connection joint and is in threaded connection with the second nut.
Preferably, the second connector and/or the second nut is provided with a second handle.
Preferably, a third adjusting washer is provided between the first connecting portion of the connecting joint and the second connecting portion of the connecting rod.
Preferably, the mounting plate is provided with a first slot and a second slot, the first positioning piece is inserted into the first slot, and the second positioning piece is inserted into the second slot.
Preferably, the mounting plate is provided with a lightening hole.
The utility model has the beneficial effects that:
the utility model aims to provide an auxiliary positioning tool for an angle sensor for an outer flap rocker arm of an airplane, which comprises a mounting plate, a first mounting assembly, a second mounting assembly, a first positioning piece and a second positioning piece. The angle sensor auxiliary positioning tool for the aircraft outer flap rocker arm comprises the steps of firstly, rotationally connecting a mounting plate to the outer flap rocker arm through a first mounting assembly, then, rotationally connecting the mounting plate around the central axis of the first mounting assembly until a first positioning piece arranged on the mounting plate abuts against the side wall of the outer flap rocker arm, locking the mounting plate and the outer flap rocker arm through the first mounting assembly, namely, locking the relative positions of the mounting plate and the outer flap rocker arm, rotationally connecting a connecting joint to the mounting plate through a second mounting assembly, rotationally connecting the connecting joint around the central axis of the second mounting assembly until the connecting joint abuts against a second positioning piece on the mounting plate, locking the connecting joint and the mounting plate through the second mounting assembly, namely, locking the relative positions of the connecting joint and the mounting plate, and fixedly connecting a connecting rod to the outer flap rocker arm, so that the relative positions of the connecting joint and the connecting rod are fixed, aligning a first connecting part of the connecting joint with a second connecting part of the connecting rod, and connecting the first connecting part to the second connecting part, and accurately and efficiently determining the assembly position of the connecting joint; after being connected well with attach fitting and connecting rod, with second installation component, mounting panel and first installation component dismantlement, with angle sensor body coupling in attach fitting, for prior art, effectively promoted angle sensor's location and assembly efficiency, and promoted angle sensor's measurement accuracy.
Drawings
FIG. 1 is a schematic view of an auxiliary positioning tool for an angle sensor for an outer flap rocker arm of an aircraft along a first view angle according to an embodiment of the present utility model;
FIG. 2 is a schematic structural view of an auxiliary positioning tool for an angle sensor for an outer flap rocker arm of an aircraft along a second view angle according to an embodiment of the present utility model;
FIG. 3 is a schematic view of a part of an auxiliary positioning tool for an angle sensor for an outer flap rocker arm of an aircraft, according to an embodiment of the present utility model;
FIG. 4 is a schematic structural view of a first mounting assembly of an auxiliary positioning tool for an angle sensor for an outer flap rocker arm of an aircraft, provided by an embodiment of the utility model;
FIG. 5 is a cross-sectional view of a first mounting assembly of an angle sensor assisted positioning tooling for an outer flap rocker arm of an aircraft provided in accordance with an embodiment of the present utility model;
FIG. 6 is a schematic structural view of a second mounting assembly of an auxiliary positioning tooling for an angle sensor for an outer flap rocker arm of an aircraft, provided by an embodiment of the present utility model;
FIG. 7 is a cross-sectional view of a second mounting assembly of an angle sensor assisted positioning tooling for an outer flap rocker arm of an aircraft, provided in accordance with an embodiment of the present utility model.
In the figure:
100. an outer flap rocker arm; 210. a connection joint; 211. a first connection portion; 220. a connecting rod; 221. a second connecting portion;
1. a mounting plate; 11. a first mounting surface; 12. a second mounting surface; 13. a lightening hole;
2. a first mounting assembly; 21. a first connector; 22. a first nut; 23. a first bushing; 24. a first adjustment shim; 25. a first handle;
3. a first positioning member;
4. a second mounting assembly; 41. a second connector; 42. a second nut; 43. a second bushing; 44. a second adjustment shim; 45. a second handle;
5. and a second positioning piece.
Detailed Description
In order to make the technical problems solved by the present utility model, the technical solutions adopted and the technical effects achieved more clear, the technical solutions of the embodiments of the present utility model will be described in further detail below with reference to the accompanying drawings, and it is obvious that the described embodiments are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In the description of the present utility model, unless explicitly stated and limited otherwise, the terms "connected," "connected," and "fixed" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
In the present utility model, unless expressly stated or limited otherwise, a first feature "above" or "below" a second feature may include both the first and second features being in direct contact, as well as the first and second features not being in direct contact but being in contact with each other through additional features therebetween. Moreover, a first feature being "above," "over" and "on" a second feature includes the first feature being directly above and obliquely above the second feature, or simply indicating that the first feature is higher in level than the second feature. The first feature being "under", "below" and "beneath" the second feature includes the first feature being directly under and obliquely below the second feature, or simply means that the first feature is less level than the second feature.
The utility model provides an auxiliary positioning tool for an angle sensor for an aircraft outer flap rocker arm, which is used for assembling the angle sensor on the outer flap rocker arm 100, as shown in fig. 1-3, wherein the angle sensor comprises an angle sensor body, a connecting joint 210 and a connecting rod 220, the angle sensor body is detachably connected with the connecting joint 210, the connecting rod 220 is fixedly connected with the outer flap rocker arm 100, the auxiliary positioning tool for the aircraft outer flap rocker arm comprises a mounting plate 1, a first mounting assembly 2, a second mounting assembly 4, a first positioning piece 3 and a second positioning piece 5, the first positioning piece 3 is arranged on the mounting plate 1, the first mounting assembly 2 can rotationally connect the mounting plate 1 with the outer flap rocker arm 100 so that the first positioning piece 3 can abut against the side wall of the outer flap rocker arm 100, and the first mounting assembly 2 can lock or unlock the relative positions of the mounting plate 1 and the outer flap rocker arm 100; the second positioning piece 5 is arranged on the mounting plate 1, the second mounting assembly 4 can rotationally connect the connecting joint 210 to the mounting plate 1, so that the connecting joint 210 can abut against the second positioning piece 5, and the second mounting assembly 4 can lock or unlock the relative positions of the mounting plate 1 and the connecting joint 210; when the first positioning member 3 abuts against the side wall of the outer flap rocker arm 100 and the connecting joint 210 abuts against the second positioning member 5, the first connecting portion 211 of the connecting joint 210 and the second connecting portion 221 of the connecting rod 220 are aligned, and the first connecting portion 211 is used for connecting with the second connecting portion 221.
As shown in fig. 1-3, the auxiliary positioning tool for an angle sensor for an outer flap rocker of an aircraft firstly rotates the mounting plate 1 to be connected with the outer flap rocker 100 through the first mounting component 2, then rotates the mounting plate 1 around the central axis of the first mounting component 2 until the first positioning piece 3 arranged on the mounting plate 1 is abutted against the side wall of the outer flap rocker 100, then locks the mounting plate 1 and the outer flap rocker 100 through the first mounting component 2, namely the relative positions of the mounting plate 1 and the outer flap rocker 100 are locked, then rotates the connecting joint 210 to be connected with the mounting plate 1 through the second mounting component 4, rotates the connecting joint 210 around the central axis of the second mounting component 4 until the connecting joint 210 is abutted against the second positioning piece 5 on the mounting plate 1, then locks the connecting joint 210 and the mounting plate 1 through the second mounting component 4, namely the relative positions of the connecting joint 210 and the mounting plate 1 are locked, and the connecting rod 220 is fixedly connected with the outer flap rocker 100, thus, the relative positions of the connecting joint 210 and the first connecting part 211 of the connecting rod 220 are aligned, and the second connecting part 221 of the connecting joint 210 and the connecting rod 220 are accurately assembled, and the accurate connecting joint 211 is realized; after the connection joint 210 is connected with the connecting rod 220, the second installation component 4, the installation plate 1 and the first installation component 2 are detached, and the angle sensor body is connected with the connection joint 210.
Specifically, in the present embodiment, after aligning the first connection portion 211 of the connection joint 210 and the second connection portion 221 of the link 220, the first connection portion 211 and the second connection portion 221 are drilled, and then the first connection portion 211 and the second connection portion 221 are connected by a connection member such as a bolt. To completely fix the fitting position of the connection joint 210.
Specifically, in this embodiment, as shown in fig. 1, the mounting plate 1 rotates in the first time pin direction until the first positioning member 3 provided on the mounting plate 1 abuts against the side wall of the outer flap rocker arm 100, and the mounting plate 1 cannot rotate in the first time pin direction any more; the connection joint 210 rotates in the second clockwise direction until the connection joint 210 abuts against the second positioning member 5 on the mounting plate 1, and the connection joint 210 cannot rotate in the second clockwise direction any more. Specifically, in the present embodiment, the first hour hand direction and the second hour hand direction are in the same direction. As shown in fig. 1, the ab direction is the first time pin direction.
It will be appreciated that the direction of rotation of the mounting plate 1 may change as the setting position of the first positioning member 3 is adjusted; when the setting position of the second positioning member 5 is adjusted, the rotational direction of the connection joint 210 may be changed.
As shown in fig. 1-3, the mounting board 1 is provided with a first mounting surface 11 and a second mounting surface 12, the first mounting component 2 and the first positioning piece 3 are distributed on the first mounting surface 11 at intervals, the second mounting component 4 and the second positioning piece 5 are distributed on the second mounting surface 12 at intervals, and the first mounting surface 11 and the second mounting surface 12 are parallel and distributed along the thickness direction of the mounting board 1 at intervals. Since the thickness of the outer flap rocker arm 100 gradually increases from the portion connected to the first connection assembly to the direction in which the link 220 is provided, the first mounting surface 11 and the second mounting surface 12 are provided in parallel and are spaced apart in the thickness direction of the mounting plate 1, so that the first connection portion 211 of the connection joint 210 and the second connection portion 221 of the link 220 can be effectively aligned.
Specifically, since a gap exists between the first connection portion 211 of the connection joint 210 and the second connection portion 221 of the link 220 after the first connection portion 211 of the connection joint 210 and the second connection portion 221 of the link 220 are aligned. A third adjustment washer is provided between the first connection portion 211 of the connection joint 210 and the second connection portion 221 of the link 220. The change of the setting position of the connection joint 210 is avoided, and the assembly precision is effectively improved. It is understood that the third adjustment shim is a rigid shim. Design cost can be reduced, and maintainability is improved.
Preferably, the mounting plate 1 is integrally formed by casting or machining. The number of parts can be reduced, and the structural strength and the service life of the mounting plate 1 are improved.
1-5, the first mounting assembly 2 includes a first connector 21 and a first nut 22, the first connector 21 passing through the mounting plate 1 and the outer flap rocker arm 100 and threadably engaging the first nut 22. Specifically, when the first connecting piece 21 passes through the mounting plate 1 and the outer flap rocker 100 to be in threaded connection with the first nut 22, but the first nut 22 is not screwed to the first connecting piece 21, the mounting plate 1 can rotate around the central axis of the first connecting piece 21, so that the first positioning piece 3 on the mounting plate 1 can abut against the side wall of the outer flap rocker 100, and after the first positioning piece 3 on the mounting plate 1 abuts against the side wall of the outer flap rocker 100, the first nut 22 is screwed to the first connecting piece 21, thereby realizing locking of the relative positions of the mounting plate 1 and the outer flap rocker 100; it will be appreciated that when the first connector 21 is threaded through the mounting plate 1 and the outer flap rocker 100 with the first nut 22, but the first nut 22 is not tightened to the first connector 21, the first mounting assembly 2 does not lock the relative positions of the mounting plate 1 and the outer flap rocker 100.
Specifically, as shown in fig. 1 to 5, the first mounting assembly 2 further includes a first bushing 23 and a first adjusting washer 24, the first bushing 23 is inserted into the mounting plate 1, and the first connecting member 21 sequentially passes through the first bushing 23, the mounting plate 1, the outer flap rocker arm 100 and the first adjusting washer 24 and is in threaded connection with the first nut 22. The mounting plate 1 can rotate around the central axis of the first mounting assembly 2, and the relative positions of the mounting plate 1 and the outer flap rocker arm 100 can be locked or unlocked, wherein the first adjusting gasket 24 is arranged between the first nut 22 and the outer flap rocker arm 100, so that the surface of the outer flap rocker arm 100 can be effectively prevented from being damaged in the process of tightening the first nut 22; through setting up first bush 23 between first connecting piece 21 and mounting panel 1, can effectually prevent to damage the surface of mounting panel 1 at the in-process of tightening first nut 22 to the life and the performance of mounting panel 1 and outer flap rocking arm 100 have been promoted.
Preferably, the first nut 22, the first bushing 23 and the first adjusting washer 24 are all standard components. Design cost can be effectively reduced, and maintainability is improved. Wherein the first adjustment washer 24 is a rubber washer.
Further specifically, as shown in fig. 1-5, the first connector 21 and/or the first nut 22 are provided with a first handle 25. By providing the first handle 25, it is facilitated to screw the first nut 22 to the first connector 21, thereby enabling a convenient and quick locking of the relative positions of the mounting plate 1 and the outer flap rocker arm 100 by the first mounting assembly 2. Preferably, in the present embodiment, both the first connector 21 and the first nut 22 are provided with a first handle 25.
As shown in fig. 1 to 3, 6 and 7, the second mounting assembly 4 includes a second connection member 41 and a second nut 42, and the second connection member 41 sequentially passes through the mounting plate 1 and the connection joint 210 and is screw-coupled with the second nut 42. Specifically, when the second connector 41 passes through the mounting plate 1 and the connector 210 and is in threaded connection with the second nut 42, but the second nut 42 is not screwed to the second connector 41, the connector 210 may rotate around the central axis of the second connector 41, so that the connector 210 may abut against the second positioning member 5, and after the connector 210 abuts against the second positioning member 5, the second nut 42 is screwed to the second connector 41, thereby achieving locking of the relative positions of the connector 210 and the mounting plate 1; it will be appreciated that when the second connector 41 is threaded through the mounting plate 1 and the connector sub 210 and with the second nut 42, but the second nut 42 is not tightened to the second connector 41, the second mounting assembly 4 does not lock the relative positions of the connector sub 210 and the mounting plate 1.
Specifically, as shown in fig. 1 to 3, 6 and 7, the second mounting assembly 4 further includes a second bushing 43 and a second adjustment washer 44, the second bushing 43 is inserted into the mounting plate 1, and the second connecting member 41 sequentially passes through the second adjustment washer 44, the connecting joint 210, the mounting plate 1 and the second bushing 43, and is screwed with the second nut 42. By providing the second adjustment washer 44, the surface of the connection joint 210 can be effectively prevented from being damaged during the tightening of the second nut 42; by providing the second bushing 43, damage to the surface of the mounting plate 1 during tightening of the second nut 42 can be avoided, thereby improving the service life and usability of the mounting plate 1 and the connection joint 210.
Further specifically, the connection joint 210 is provided with a through hole, and the second connection member 41 sequentially passes through the second adjustment washer 44, the through hole, the mounting plate 1, and the second bushing 43, and is screwed with the second nut 42, and the through hole is used for connecting the angle sensor body. The positioning angle sensor is arranged in such a way to realize accurate and efficient positioning of the positioning angle sensor.
Preferably, the second nut 42, the second bushing 43 and the second adjusting washer 44 are all standard components, which can reduce design cost and promote maintainability.
Further specifically, as shown in fig. 1-3, 6 and 7, the second connector 41 and/or the second nut 42 is provided with a second handle 45. By providing the second handle 45, the second nut 42 is conveniently screwed to the second connector 41, so that the relative positions of the mounting plate 1 and the connection joint 210 can be conveniently and rapidly locked by the second mounting assembly 4. As shown in fig. 1 to 3, 6 and 7, in the present embodiment, the second handle 45 is merely exemplified as being provided on the second connecting member 41.
Further specifically, the mounting plate 1 is provided with a first slot and a second slot, the first positioning piece 3 is inserted into the first slot, and the second positioning piece 5 is inserted into the second slot. Specifically, the first slots are distributed on the first mounting surface 11, and the second slots are distributed on the second mounting surface 12. The first positioning piece 3 is convenient to assemble and disassemble, and the setting position of the first positioning piece 3 is also convenient to adjust; the second positioning piece 5 is convenient to assemble and disassemble, and the setting position of the second positioning piece 5 is also convenient to adjust.
As an alternative, the first positioning member 3 is integrally formed with the mounting plate 1, and the second positioning member 5 is integrally formed with the mounting plate 1. The number of parts can be reduced. As another alternative, the first positioning member 3 may be connected to the mounting plate 1 by welding or the like, and the second positioning member 5 may be connected to the mounting plate 1 by welding or the like.
Wherein the mounting plate 1 is provided with lightening holes 13 as shown in figures 1-4. The mounting plate 1 is provided with the lightening hole 13, so that the weight of the mounting plate 1 can be effectively lightened, the light-weight design is satisfied, and the handheld positioning in the use process is also convenient. Specifically, in the present embodiment, two lightening holes 13 are exemplarily provided.
It is to be understood that the above examples of the present utility model are provided for clarity of illustration only and are not limiting of the embodiments of the present utility model. Other variations or modifications of the above teachings will be apparent to those of ordinary skill in the art. It is not necessary here nor is it exhaustive of all embodiments. Any modification, equivalent replacement, improvement, etc. which come within the spirit and principles of the utility model are desired to be protected by the following claims.
Claims (10)
1. The utility model provides an angle sensor auxiliary positioning frock for outer flap rocking arm of aircraft for assemble angle sensor in outer flap rocking arm (100), angle sensor includes angle sensor body, attach fitting (210) and connecting rod (220), the angle sensor body can dismantle connect in attach fitting (210), connecting rod (220) fixed connection in outer flap rocking arm (100), its characterized in that includes:
the device comprises a mounting plate (1), a first mounting assembly (2) and a first positioning piece (3) arranged on the mounting plate (1), wherein the first mounting assembly (2) can rotationally connect the mounting plate (1) to the outer flap rocker arm (100) so that the first positioning piece (3) can be abutted against the side wall of the outer flap rocker arm (100), and the first mounting assembly (2) can lock or unlock the relative positions of the mounting plate (1) and the outer flap rocker arm (100);
a second mounting assembly (4) and a second positioning member (5) arranged on the mounting plate (1), wherein the second mounting assembly (4) can rotationally connect the connecting joint (210) to the mounting plate (1) so that the connecting joint (210) can be abutted against the second positioning member (5), and the second mounting assembly (4) can lock or unlock the relative positions of the mounting plate (1) and the connecting joint (210);
when the first positioning piece (3) is abutted against the side wall of the outer flap rocker arm (100), the connecting joint (210) is abutted against the second positioning piece (5), a first connecting portion (211) of the connecting joint (210) is aligned with a second connecting portion (221) of the connecting rod (220), and the first connecting portion (211) is used for being connected with the second connecting portion (221).
2. The auxiliary positioning tool for the angle sensor for the outer flap rocker arm of the aircraft according to claim 1, wherein a first mounting surface (11) and a second mounting surface (12) are arranged on the mounting plate (1), the first mounting assembly (2) and the first positioning piece (3) are distributed on the first mounting surface (11) at intervals, the second mounting assembly (4) and the second positioning piece (5) are distributed on the second mounting surface (12) at intervals, and the first mounting surface (11) and the second mounting surface (12) are parallel and distributed along the thickness direction of the mounting plate (1) at intervals.
3. The auxiliary positioning fixture for an angle sensor for an outer flap rocker arm of an aircraft according to claim 1, characterized in that the first mounting assembly (2) comprises a first connecting piece (21) and a first nut (22), the first connecting piece (21) passing through the mounting plate (1) and the outer flap rocker arm (100) and being in threaded connection with the first nut (22).
4. The auxiliary positioning tool for the angle sensor for the outer flap rocker arm of the aircraft according to claim 3, wherein the first mounting assembly (2) further comprises a first bushing (23) and a first adjusting gasket (24), the first bushing (23) is inserted into the mounting plate (1), and the first connecting piece (21) sequentially penetrates through the first bushing (23), the mounting plate (1), the outer flap rocker arm (100) and the first adjusting gasket (24) and is in threaded connection with the first nut (22).
5. An auxiliary positioning fixture for an angle sensor for an aircraft outer flap rocker arm according to claim 3, characterized in that the first connecting piece (21) and/or the first nut (22) are provided with a first handle (25).
6. The auxiliary positioning fixture for an angle sensor for an aircraft outer flap rocker arm according to claim 1, characterized in that the second mounting assembly (4) comprises a second connecting piece (41) and a second nut (42), the second connecting piece (41) passing through the mounting plate (1) and the connecting joint (210) and being in threaded connection with the second nut (42).
7. The auxiliary positioning tool for an angle sensor for an aircraft outer flap rocker arm according to claim 6, characterized in that the second connecting piece (41) and/or the second nut (42) are provided with a second handle (45).
8. The auxiliary positioning tooling for the angle sensor for the outer flap rocker arm of the aircraft according to any one of claims 1 to 7, characterized in that a third adjusting gasket is arranged between the first connecting portion (211) of the connecting joint (210) and the second connecting portion (221) of the connecting rod (220).
9. The auxiliary positioning tool for the angle sensor for the outer flap rocker arm of the aircraft according to any one of claims 1 to 7, wherein the mounting plate (1) is provided with a first slot and a second slot, the first positioning piece (3) is inserted into the first slot, and the second positioning piece (5) is inserted into the second slot.
10. The auxiliary positioning fixture for an angle sensor for an aircraft outer flap rocker arm according to any one of claims 1 to 7, characterized in that the mounting plate (1) is provided with a lightening hole (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321841503.2U CN220410898U (en) | 2023-07-13 | 2023-07-13 | Auxiliary positioning tool for angle sensor for outer flap rocker arm of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321841503.2U CN220410898U (en) | 2023-07-13 | 2023-07-13 | Auxiliary positioning tool for angle sensor for outer flap rocker arm of airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220410898U true CN220410898U (en) | 2024-01-30 |
Family
ID=89641050
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321841503.2U Active CN220410898U (en) | 2023-07-13 | 2023-07-13 | Auxiliary positioning tool for angle sensor for outer flap rocker arm of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220410898U (en) |
-
2023
- 2023-07-13 CN CN202321841503.2U patent/CN220410898U/en active Active
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