CN112577523B - Adjustable inertial navigation test switching tool and adjusting and installing method - Google Patents
Adjustable inertial navigation test switching tool and adjusting and installing method Download PDFInfo
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- CN112577523B CN112577523B CN202011453838.8A CN202011453838A CN112577523B CN 112577523 B CN112577523 B CN 112577523B CN 202011453838 A CN202011453838 A CN 202011453838A CN 112577523 B CN112577523 B CN 112577523B
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- guide rail
- axis direction
- double guide
- direction double
- inertial navigation
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
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- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
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- Machine Tool Units (AREA)
- Details Of Measuring And Other Instruments (AREA)
Abstract
The invention provides an adjustable inertial navigation test transfer tool and an adjusting and installing method, wherein the adjustable inertial navigation test transfer tool comprises an adjustable flange plate (1), an X-axis direction double guide rail (4), a Y-axis direction double guide rail (5) and a guide rail base (3); the adjusting and installing method is mainly based on an X-axis direction double guide rail (4) and a Y-axis direction double guide rail (5) to form a 'groined' structure, the Y-axis direction double guide rail (5) can slide and be fixed on the X-axis direction double guide rail (4), and the inertial navigation device is fixedly connected to the Y-axis direction double guide rail (5). The designed adjustable inertial navigation test switching tool is simple in structure, convenient to operate and capable of adapting to the inertial navigation test switching installation requirements of different external dimensions.
Description
Technical Field
The invention belongs to the field of mechanical design, and particularly relates to an adjustable inertial navigation test switching tool and an adjustable installation method.
Background
The inertial navigation test equipment consists of a three-axis turntable and an operation table, wherein the rotation angle of the three-axis turntable is set by the operation table, and data are fed back to the operation table after the turntable reaches the set angle. At present, when inertial navigation is installed on a three-axis turntable for testing, the installed three-axis turntable table top is a sunken circular groove, and the adaptive inertial navigation can only meet the installation requirement if the adaptive inertial navigation meets certain size and has circular appearance. Rectangular inertial navigation or inertial navigation of other shapes cannot be mounted in such a depressed circular groove because of the different layout of mounting holes, resulting in inapplicability of the test equipment. In actual work, a special fixed switching support is required to be customized according to the inertial navigation appearance, and the universality is lacking.
Disclosure of Invention
In order to solve the technical problems, an adjustable inertial navigation test switching tool is designed, so that the tool is suitable for being connected with a three-axis turntable during testing of inertial navigation with different external dimensions.
The adjustable inertial navigation test switching tool comprises a switching flange plate, an X-axis direction double guide rail, a Y-axis direction double guide rail and a guide rail base; the four mounting screws are used for mounting and fastening the switchable flange plate into the sunken circular groove of the three-axis turntable through the mounting holes on the switchable flange plate; a guide rail base is arranged in the vertical direction outside the switchable flange plate; two parallel X-axis direction double guide rails are arranged on the guide rail base, and two parallel Y-axis direction double guide rails are arranged above the X-axis direction double guide rails; the X-axis direction double guide rail and the Y-axis direction double guide rail form a 'groined' structure, the Y-axis direction double guide rail can slide and be fixed on the X-axis direction double guide rail, and the inertial navigation device is fixedly connected to the Y-axis direction double guide rail.
Further, two movable connecting studs are respectively arranged on each guide rail of the Y-axis direction double guide rail, two groups of four movable connecting studs can form a virtual quadrilateral, and the sliding Y-axis direction double guide rail and the movable connecting studs can form virtual quadrilaterals with different sizes.
Similarly, two groups of four movable bolts are arranged on two guide rails on the double guide rails in the X-axis direction and are used for adjusting and fixing the two guide rails of the double guide rails in the Y-axis direction.
Further, two flange locating pins are arranged on the switchable flange, and the switchable flange can be installed and fastened into the sunken circular groove of the three-axis turntable more quickly and accurately through the flange locating pins.
By adopting the adjustable inertial navigation test transfer tool, the adjusting and mounting method comprises the following steps:
firstly, installing an adapter flange plate: the two flange locating pins are used for accurately locating, and the four mounting screws are used for mounting and fastening the switchable flange into the sunken circular groove of the three-axis turntable through the mounting holes on the switchable flange;
second, installing a guide rail base: mounting the guide rail base to the outer side of the switchable flange in the vertical direction;
thirdly, adjusting and fixing the Y-axis direction double guide rails: according to the inertial navigation radial installation size, the movable bolts on the four X-axis direction double guide rails are used for adjusting and fixing the Y-axis direction double guide rails;
fourth, adjusting and fixing the movable connecting stud: according to the transverse installation size of the inertial navigation size, adjusting and fixing four movable connecting studs;
fifthly, installing inertial navigation: inertial navigation is mounted to four movable connecting studs.
In the technical scheme, the designed adjustable inertial navigation test switching tool is simple in structure and convenient to operate, and can adapt to the inertial navigation test switching installation requirements of different external dimensions.
Drawings
FIG. 1 is a structural diagram of an adjustable inertial navigation test transfer tool.
Fig. 2 is a schematic view of a special-shaped inertial navigation installation.
In fig. 1-2: 1. the flange plate can be connected in an adapting mode, the flange plate positioning pin is 2, the guide rail base is 3, the X-axis direction double guide rail is 4, the Y-axis direction double guide rail is 5, the movable connecting stud is 6, and the movable bolt is 7.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to fig. 1 and 2.
As shown in fig. 1, the adapter part in the invention is composed of an adapter flange 1 and a flange locating pin 2. The adaptor flange 1 is circular and is provided with four mounting holes, two flange locating pins 2 are arranged on one side, and a guide rail base 3 is arranged on the other side in the vertical direction. When the test switching tool is installed, the switching flange plate 1 is installed in the sunken circular groove of the three-axis turntable, and is positioned through the flange plate positioning pin 2, and the installation hole is fastened by the installation screw.
Two parallel X-axis direction double guide rails 4 are arranged on the guide rail base 3; two parallel Y-axis double guide rails 5 are also arranged above the X-axis double guide rail 4; two movable connecting studs 6 are respectively arranged on each guide rail of the double guide rail 5 in the Y-axis direction, two groups of four movable connecting studs 6 can form a virtual quadrangle, and the double guide rail 5 in the Y-axis direction and the movable connecting studs 6 can form the virtual quadrangle with different sizes; the X-axis direction double guide rail 4 is adjusted and fixed with the Y-axis direction double guide rail 5 through two groups of four movable bolts 7.
The mounting holes on the inertial navigation mounting chassis with different shapes can be virtualized to form a quadrangle, and the virtual quadrangle can be overlapped with the quadrangle virtualized by the mounting holes on the different inertial navigation mounting chassis by adjusting the distance between the double guide rails 5 in the Y-axis direction and the movable connecting stud 6 and changing the relative position, so that the tool can be used for mounting different inertial navigation. As shown in fig. 2, an installation schematic diagram of a special-shaped inertial navigation device is shown.
Claims (1)
1. An installation method for performing inertial navigation adjustment based on an adjustable inertial navigation test transfer tool comprises an adjustable flange plate (1), an X-axis direction double guide rail (4), a Y-axis direction double guide rail (5) and a guide rail base (3); the four mounting screws are used for mounting and fastening the switchable flange plate (1) into the sunken circular groove of the three-axis turntable through the mounting holes on the switchable flange plate (1); a guide rail base (3) is arranged on the outer side of the switchable flange plate (1) in the vertical direction; two parallel X-axis direction double guide rails (4) are arranged on the guide rail base (3), and two parallel Y-axis direction double guide rails (5) are arranged above the X-axis direction double guide rails (4); x axis direction double guide rail (4) and Y axis direction double guide rail (5) form "well font" structure, Y axis direction double guide rail (5) slide and fix on X axis direction double guide rail (4), inertial navigation device fixed connection is on Y axis direction double guide rail (5), every guide rail of Y axis direction double guide rail (5) on install two movable connection studs (6) respectively, two sets of four movable connection studs (6) altogether constitute a virtual quadrangle, slide Y axis direction double guide rail (5) and movable connection studs (6), form the virtual quadrangle of equidimension not, two guide rails on X axis direction double guide rail (4) on be provided with two sets of four movable bolts (7) altogether for adjust two guide rails of fixed Y axis direction double guide rail (5), rotatable flange (1) on be provided with two flange locating pins (2), through flange locating pin (2) locate function, will rotatable flange (1) install the method of sinking into its recess of triaxial turntable that falls down more accurately fast.
Firstly, mounting an adapter flange plate (1): the two flange locating pins (2) are used for accurately locating, and the four mounting screws are used for mounting and fastening the switchable flange (1) into the sunken circular groove of the triaxial turntable through the mounting holes on the switchable flange (1);
second, the guide rail base (3) is installed: the guide rail base (3) is arranged on the outer side of the switchable flange plate (1) in the vertical direction;
thirdly, adjusting and fixing a Y-axis direction double guide rail (5): according to the inertial navigation radial installation size, the movable bolts (7) on the four X-axis direction double guide rails (4) are used for adjusting and fixing the Y-axis direction double guide rails (5);
fourth, adjust fixed movable connection stud (6): according to the transverse installation size of the inertial navigation size, adjusting and fixing four movable connecting studs (6);
fifthly, installing inertial navigation: inertial navigation is mounted on four movable connecting studs (6).
Priority Applications (1)
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CN202011453838.8A CN112577523B (en) | 2020-12-12 | 2020-12-12 | Adjustable inertial navigation test switching tool and adjusting and installing method |
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CN202011453838.8A CN112577523B (en) | 2020-12-12 | 2020-12-12 | Adjustable inertial navigation test switching tool and adjusting and installing method |
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CN112577523A CN112577523A (en) | 2021-03-30 |
CN112577523B true CN112577523B (en) | 2023-10-03 |
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CN114509092B (en) * | 2022-02-14 | 2022-09-16 | 青岛智腾微电子有限公司 | Double-shaft rotary table for inertial navigation product test |
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DE102015113486A1 (en) * | 2015-08-14 | 2017-02-16 | Northrop Grumman Litef Gmbh | Navigation device with turntable for a turnover measurement and method for operating the navigation device |
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CN204461444U (en) * | 2015-01-30 | 2015-07-08 | 北京航天时代光电科技有限公司 | A kind of applicable difference is used to the transition tool of group Fast Installation in single-shaft-rotation mechanism |
CN205745900U (en) * | 2016-06-12 | 2016-11-30 | 深圳市赋鑫信息科技有限公司 | A kind of five-axis flight table |
CN207171971U (en) * | 2017-09-04 | 2018-04-03 | 江西洪都航空工业集团有限责任公司 | A kind of inertial navigation location and installation support |
CN108032264A (en) * | 2017-12-13 | 2018-05-15 | 陕西宝成航空仪表有限责任公司 | The adjustable turntable clamper in mounting hole position |
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