Special angle detection tool for spaceflight servo mechanism

Abstract

The utility model discloses a special angle detection tool for a spaceflight servo mechanism. The special angle detection tool comprises a fixed seat, the spaceflight servo mechanism, a servo mechanism mirror seat and a special cushion block, a spaceflight servo mechanism is fixedly installed at the top of the fixing base, and a servo mechanism mirror base is fixedly installed at the upper end of the spaceflight servo mechanism. According to the special angle detection tool for the spaceflight servo mechanism, due to the fact that the spaceflight servo mechanism is small, exquisite and compact in structure, the spaceflight servo mechanism cannot be detected by using an angle ruler, and a miniature digital display inclinometer cannot be used for direct measurement, the special cushion block, the standard cushion block, the fixed pressing piece and the inner hexagon screw are designed to be matched with the miniature digital display inclinometer to form the special angle detection tool; the detection tool is small and exquisite in appearance, the matched inclinometer is high in sensitivity, the precision grade meets the detection standard requirement, the micro digital display inclinometer is placed on a special or standard cushion block test surface and clamped on a spaceflight servo mechanism test part for angle detection, and the problem that the angle of the product is difficult to measure is solved.

Description

Technical Field

[0001] This utility model relates to the field of testing tooling technology, specifically a special angle testing tooling for aerospace servo mechanisms. Background Technology

[0002] A certain type of aerospace servo mechanism is characterized by its precise structure, compact size, and high sensitivity. However, when assembling and adjusting the angles of the inner and outer frames, it is impossible to use protractors or other measuring equipment to measure the angles. The existing technology uses a coordinate measuring machine (CMM) to measure the angles, which is very inconvenient due to limitations in space and personnel. Moreover, this angle needs to be measured while being adjusted, and the relevant parts are too small, making installation and disassembly difficult due to space constraints. While a CMM can be used to measure the angles during the research and development stage when the production quantity is small, it will not be suitable after mass production, and the measurement method will become a bottleneck restricting the production progress.

[0003] To address the aforementioned issues, we have made innovative designs based on the existing angle detection fixture structure for aerospace servo mechanisms. Utility Model Content

[0004] The purpose of this utility model is to provide a special angle detection tooling for aerospace servo mechanisms, so as to solve the problem mentioned in the background art that existing devices cannot use protractors or other detection equipment to detect angles when assembling and debugging the inner and outer frame angles.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a special angle detection fixture for aerospace servo mechanisms, comprising a fixed base, an aerospace servo mechanism, a servo mechanism mirror mount, a special pad, a positioning hole, and a miniature digital display inclinometer; the aerospace servo mechanism is fixedly installed on the top of the fixed base, and a servo mechanism mirror mount is fixedly installed on the upper end of the aerospace servo mechanism; the special pad is disposed on the outside of the servo mechanism mirror mount, and a positioning hole is opened on the inner side of the special pad; and a miniature digital display inclinometer is connected to the outside of the special pad.

[0006] Preferably, a fixing plate is provided on the outer side of the special pad, and a through groove is provided on the inner side of the fixing plate.

[0007] Preferably, an internal hexagon screw passes through the inner side of the through groove, and the tail end of the internal hexagon screw is threaded into the inner side of the positioning hole.

[0008] Preferably, the fixing plate and the special pad are distributed in a front-to-back correspondence about the midpoint of the servo mechanism mirror mount.

[0009] Preferably, the special pad and the micro digital display inclinometer form a magnetic attraction structure.

[0010] Compared with the prior art, the beneficial effect of this utility model is that the special angle detection fixture for aerospace servo mechanisms is:

[0011] Because the aerospace servo mechanism is small and compact, it is difficult to measure using an angle ruler or a micro digital inclinometer. Therefore, this invention designs a special pad, a standard pad, a fixing plate, and hex socket screws to work with a micro digital inclinometer to form a special angle detection fixture. This fixture is compact in appearance, and the inclinometer it is paired with has high sensitivity and accuracy that meets the testing standards. The micro digital inclinometer is placed on the test surface of the special or standard pad and clamped to the test part of the aerospace servo mechanism to perform angle detection, thus solving the problem of difficult angle measurement for this product. Attached Figure Description

[0012] Figure 1 This is a schematic diagram of the overall three-dimensional structure of the present invention;

[0013] Figure 2 This is a schematic diagram of the connection structure between the special pad and the fixing plate of this utility model;

[0014] Figure 3 This is an exploded structural diagram of the special pad and fixing plate of this utility model;

[0015] Figure 4 This is a three-dimensional structural diagram of the fixing base of this utility model;

[0016] Figure 5 This is a three-dimensional structural diagram of the special pad block of this utility model;

[0017] Figure 6 This is a schematic diagram of the three-dimensional structure of the fixed pressure plate of this utility model.

[0018] In the diagram: 1. Mounting base; 2. Aerospace servo mechanism; 3. Servo mechanism mirror mount; 4. Special pad; 5. Positioning hole; 6. Miniature digital display inclinometer; 7. Fixing plate; 8. Through slot; 9. Socket head screw. Detailed Implementation

[0019] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0020] Please see Figures 1-6This utility model provides a technical solution: a special angle detection fixture for aerospace servo mechanisms, including: a fixed base 1, an aerospace servo mechanism 2, a servo mechanism mirror base 3, a special pad 4, a positioning hole 5, and a miniature digital display inclinometer 6; the aerospace servo mechanism 2 is fixedly installed on the top of the fixed base 1, and the servo mechanism mirror base 3 is fixedly installed on the upper end of the aerospace servo mechanism 2; the special pad 4 is located on the outside of the servo mechanism mirror base 3, and the positioning hole 5 is opened on the inner side of the special pad 4; and the miniature digital display inclinometer 6 is connected to the outside of the special pad 4.

[0021] A fixing plate 7 is provided on the outer side of the special pad 4, and a through groove 8 is provided on the inner side of the fixing plate 7; an internal hexagon screw 9 passes through the inner side of the through groove 8, and the tail end of the internal hexagon screw 9 is threaded to the inner side of the positioning hole 5; the fixing plate 7 and the special pad 4 are distributed in a front-to-back correspondence about the midpoint of the servo mechanism mirror base 3; the special pad 4 and the micro digital display inclinometer 6 form a magnetic attraction structure;

[0022] A special angle detection fixture for aerospace servo mechanisms consists of two sets of fixtures: an inner frame angle detection fixture and an outer frame angle detection fixture. It includes a miniature digital inclinometer 6, a special pad 4, a fixed base 1, a fixing plate 7, and hex socket screws 9. When the outer frame rotates clockwise or counterclockwise, the aerospace servo mechanism 2 is placed on the fixed base 1. The special pad 4 is clamped onto the servo mechanism's mirror base 3 using the fixing plate 7 and hex socket screws 9. The miniature digital inclinometer 6 is then attached to the detection table of the special pad 4 for measurement. When measuring the pitch angle of the inner frame of the aerospace servo mechanism 2, the aerospace servo mechanism 2 is placed on the fixed base 1. The special pad 4 is placed on the servo mechanism's mirror base 3 and clamped. The miniature digital inclinometer 6 is then attached to the detection table of the special pad 4 for measurement. The aerospace servo mechanism 2 features a precise, compact structure and high sensitivity. When measuring the pitch angle of the inner frame and the clockwise / counterclockwise rotation angle of the outer frame, it is difficult to... Using protractors and other measuring equipment cannot guarantee the required pitch angle of the inner frame to be no less than ±10° and no more than ±10.5°, and the clockwise and counterclockwise rotation angle of the outer frame to be ±20°. This design provides a dedicated angle measuring fixture for the aerospace servo mechanism 2, which can quickly and accurately measure angles, solving the problem of angle control difficulties during assembly and manufacturing, greatly reducing cost budget and assembly difficulty, and ensuring product quality and schedule. Compared with the original solution of using three-coordinate measuring, the use of this angle measuring fixture makes angle measurement of this product more convenient, allowing measurement to be performed while repairing. The original repair, adjustment and measurement of one set of aerospace servo mechanism 2 required an average of 0.5 days, while the repair, adjustment and measurement of one set requires an average of about 0.1 days after using this dedicated angle measuring fixture, greatly reducing the time. Furthermore, the use of this dedicated angle measuring fixture is not limited by site or equipment, and can be performed anytime and anywhere, laying a solid foundation for mass production.

[0023] The contents not described in detail in this specification are existing technologies known to those skilled in the art.

[0024] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A special angle detection tool for aerospace servo mechanism, comprising a fixing seat (1), an aerospace servo mechanism (2), a servo mechanism mirror seat (3), a special pad (4), a positioning hole (5) and a micro digital inclinometer (6); characterized in that, The top of the fixed base (1) is fixedly installed with an aerospace servo mechanism (2), and the upper end of the aerospace servo mechanism (2) is fixedly installed with a servo mechanism mirror base (3). The special pad (4) is set on the outside of the servo mechanism mirror base (3), and the special pad (4) has a positioning hole (5) on its inner side. The special pad (4) is connected to a miniature digital display tilt meter (6) on its outer side.

2. The angle detection tool for a spaceflight servo mechanism according to claim 1, characterized in that: The special pad (4) is provided with a fixing plate (7) on the outside, and a through groove (8) is provided on the inside of the fixing plate (7).

3. The angle detection tool for a spaceflight servo mechanism according to claim 2, characterized in that: The inner side of the through groove (8) is penetrated by an internal hexagon screw (9), and the tail end of the internal hexagon screw (9) is threaded into the inner side of the positioning hole (5).

4. The aerospace servo mechanism special angle detection fixture according to claim 2, characterized in that: The fixed pressure plate (7) and the special pad (4) are distributed in a front-to-back correspondence about the midpoint of the servo mechanism mirror mount (3).

5. The angle detection tool for a spaceflight servo mechanism according to claim 1, characterized in that: The special pad (4) and the micro digital display inclinometer (6) form a magnetic attraction structure.

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