CN209841057U - Inertia measurement unit assembly structure with prevent slow-witted design - Google Patents

Inertia measurement unit assembly structure with prevent slow-witted design Download PDF

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Publication number
CN209841057U
CN209841057U CN201920622634.9U CN201920622634U CN209841057U CN 209841057 U CN209841057 U CN 209841057U CN 201920622634 U CN201920622634 U CN 201920622634U CN 209841057 U CN209841057 U CN 209841057U
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China
Prior art keywords
measurement unit
fool
inertia measurement
assembly structure
base
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CN201920622634.9U
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Chinese (zh)
Inventor
嵇明辉
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Zhejiang Geely Holding Group Co Ltd
Zhejiang Liankong Technologies Co Ltd
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Zhejiang Geely Holding Group Co Ltd
Zhejiang Geely Automobile Research Institute Co Ltd
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Priority to CN201920622634.9U priority Critical patent/CN209841057U/en
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Abstract

The utility model provides an inertia measurement unit assembly structure with foolproof design, which comprises a base, an independent inertia measurement unit and a foolproof piece, wherein the independent inertia measurement unit comprises a unit main body and a wire harness connector; the independent inertia measurement unit is arranged on the base, the fool-proof piece is arranged on the base, and the fool-proof piece is positioned on one side of the independent inertia measurement unit; the height of the fool-proof piece is higher than the lower surface of the wire harness connector, and the distance between the fool-proof piece and the unit main body is smaller than the length of the wire harness connector. The inertia measurement unit assembly structure with foolproof design provided by the utility model does not change the structure of the original independent inertia measurement unit, is simple to realize, has low cost, and has no special requirement on the material of the foolproof piece; and the realization is flexible, and for different installation positions or different installation directions, only the fool-proof piece is needed to be arranged corresponding to the installation position of the independent inertia measurement unit.

Description

Inertia measurement unit assembly structure with prevent slow-witted design
Technical Field
The utility model relates to an inertia measurement unit assembles technical field, in particular to inertia measurement unit assembly structure with prevent slow-witted design.
Background
The Inertial measurement unit is used for measuring the yaw angle of the vehicle and the acceleration in the X and Y directions under the whole vehicle coordinate system, and the measured values are vector values. The inertial measurement unit is very sensitive to vibration, and the technical progress leads to the realization of the inertial measurement unit from a previous large electronic component to a present small chip, and the weight is reduced from hundreds of grams to hundreds of grams.
The general independent inertia measurement unit is directly installed on the base through bolts, and usually, fixing bolts are installed on two symmetrical sides of the independent inertia measurement unit for fixing, but when the existing independent inertia measurement unit is installed on the base, the risk of 180-degree reverse error installation easily occurs on the horizontal plane.
Because the yaw angle of the vehicle and the acceleration in the X and Y directions under the whole vehicle coordinate system which need to be measured by the inertia measurement unit are vector values, the error of the installation direction can influence the measurement output value. Therefore, there is a need to solve the problem of the inertial measurement unit being prone to misorientation. And the existing inertia measurement units are all independent inertia measurement units produced in batch, and if the structure of the original independent inertia measurement unit is changed, resources such as manpower and material resources are caused, so that the problem that the inertia measurement unit is easy to be installed wrongly in the direction is solved on the basis of not changing the structure of the existing independent inertia measurement unit.
Disclosure of Invention
An object of the utility model is to provide an inertia measurement unit assembly structure with prevent slow-witted design, the technical problem of direction installation mistake appears easily when solving the installation of current independent inertia measurement unit.
In order to solve the technical problem, the utility model provides a:
an inertia measurement unit assembly structure with a fool-proof design comprises a base, an independent inertia measurement unit and a fool-proof piece, wherein the independent inertia measurement unit comprises a unit main body and a wire harness connector; the independent inertia measurement unit is arranged on the base, the fool-proof piece is arranged on the base, and the fool-proof piece is positioned on one side of the independent inertia measurement unit; the height of the fool-proof piece is higher than the lower surface of the wire harness connector, and the distance between the fool-proof piece and the unit main body is smaller than the length of the wire harness connector.
Further, the height of the fool-proof member is lower than the upper surface of the unit main body.
Further, the unit body has four sides, and the harness connector is located on one side of the unit body.
Furthermore, the independent inertia measurement unit further comprises two installation parts, and the two installation parts are symmetrically positioned on two opposite side surfaces of the unit main body.
Further, the installation department is equipped with the screw hole, the installation department spiro union in the base.
Further, the harness connector is integrally formed with the unit main body, and when the independent inertia measurement unit is correctly installed, the fool-proof piece is located on one side of the unit main body and opposite to the harness connector.
Further, the fool-proof piece is a fool-proof bolt, and the fool-proof bolt is installed on the base.
Further, the fool-proof piece is of a columnar structure and is installed on the base.
Further, the fool-proof piece is of a cone-shaped body structure, and the fool-proof piece is installed on the base.
Further, the fool-proof piece is detachably mounted on the base.
Adopt above-mentioned technical scheme, have following beneficial effect:
1) the inertia measurement unit assembly structure with foolproof design provided by the utility model does not change the structure of the original independent inertia measurement unit, is simple to realize, has low cost, and has no special requirement on the material of the foolproof piece;
2) the utility model provides a pair of inertia measurement unit assembly structure with prevent slow-witted design realizes in a flexible way, to different mounted position or different installation orientation, only need correspond independent inertia measurement unit mounted position setting prevent slow-witted can.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
FIG. 1 is a perspective view of an inertial measurement unit assembly with a foolproof design of the present invention;
FIG. 2 is another perspective view of the inertial measurement unit assembly with a foolproof design of the present invention;
fig. 3 is a side view of an inertial measurement unit mounting structure with a foolproof design.
The following is a supplementary description of the drawings:
10. an independent inertial measurement unit; 11. a unit main body; 12. a harness connector; 13. an installation part; 20. a fool-proof piece; 30. a base.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. It is to be understood that the embodiments described are only some embodiments of the invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Reference herein to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic described in connection with at least one implementation of the invention is included. In the description of the present invention, it is to be understood that the terms "upper", "lower", "top", "bottom", 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 referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus should not be construed as limiting the present invention. Furthermore, the terms "first", "second" and "first" 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" or "second" may explicitly or implicitly include one or more of that feature. Moreover, the terms "first," "second," and the like are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used is interchangeable under appropriate circumstances such that the embodiments of the invention described herein are capable of operation in sequences other than those illustrated or otherwise described herein.
Example 1:
an inertial measurement unit assembly structure with a fool-proof design includes an independent inertial measurement unit 10, a fool-proof piece 20 and a base 30. The foolproof member 20 and the independent inertial measurement unit 10 are both mounted on a base 30.
The independent inertia measurement unit 10 includes a unit main body 11, a harness connector 12, and two mounting portions 13.
In this embodiment, the unit body 11 has four sides, and the harness connector 12 is located on one side of the unit body 11, and may be integrally formed with the unit body 11 or may be fixedly mounted on the unit body 11. The two mounting portions 13 are symmetrically located on the remaining opposite two side surfaces of the unit main body 11, the mounting portions 13 and the unit main body 11 are integrally formed, threaded holes are formed in the mounting portions 13, and the mounting portions 13 are mounted on the base 30 through screws.
When the installation direction of the independent inertia measurement unit 10 is correct, the fool-proof member 20 is located on one side of the unit main body 11, the fool-proof member 20 and the wire harness connector 12 are located on two opposite sides of the unit main body 11, the height of the fool-proof member 20 is higher than the lower surface of the wire harness connector 12, and the height of the fool-proof member 20 is lower than the upper surface of the unit main body 11, so that the fool-proof member 20 is not interfered with the unit main body 11. The distance between the fool-proof piece 20 and the unit body 11 is smaller than the length of the wire harness connector 12 protruding out of the unit body 11.
Since the position where the individual inertia measurement unit 10 is mounted on the base 30 is fixed and the position where the mounting portion 13 is screwed to the base 30 is previously known, it is easy to have a 180-degree reverse direction of the mounting direction of the individual inertia measurement unit 10 in the mounting process, and at this time, the mounting direction of the harness connector 12 is reversed.
When a 180-degree error occurs in the installation direction of the separate unit body 11, the harness connector 12 and the fool-proof piece 20 are simultaneously located on the same side of the unit body 11. Since the height of the fool-proof member 20 is higher than the lower surface of the wire harness connector 12 and the distance between the fool-proof member 20 and the unit body 11 is smaller than the length of the wire harness connector 12 extending out of the unit body 11, the fool-proof member 20 interferes with the wire harness connector 12 when the wire harness connector 12 and the fool-proof member 20 are located on the same side of the unit body 11.
In this embodiment, the fool-proof member 20 is a fool-proof bolt screwed to the base 30, and after the installation of the independent inertia measurement unit 10 is completed, the fool-proof bolt can be detached for reuse.
Example 2:
the second embodiment has a structure substantially the same as that of the first embodiment, except that the fool-proof member 20 is a cylindrical structure, such as a cylinder, which may be a hollow structure or a solid structure, and the fool-proof member 20 of the cylindrical structure may be detachably connected to the base 30 by means of plugging, bonding, etc.
Further, the fool-proof piece 20 may be a cone-shaped body structure as long as it is satisfied that the height of the tip of the cone from the base 30 is higher than the height of the lower surface of the wire harness connector 12 from the base 30 and lower than the height of the upper surface of the unit main body 11 from the base 30. The distance between the fool-proof piece 20 and the unit body 11 is smaller than the length of the wire harness connector 12 protruding out of the unit body 11.
Adopt above-mentioned technical scheme, the utility model discloses following beneficial effect has: the inertia measurement unit assembly structure with foolproof design provided by the utility model does not change the structure of the original independent inertia measurement unit, is simple to realize, has low cost, and has no special requirement on the material of the foolproof piece 20; and the realization is flexible, and for different installation positions or different installation directions, the fool-proof piece 20 only needs to be arranged corresponding to the installation position of the independent inertia measurement unit 10.
The above description is only for the preferred embodiment of the present invention, and is not intended to limit the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included within the protection scope of the present invention.

Claims (10)

1. The utility model provides an inertia measurement unit assembly structure with prevent slow-witted design which characterized in that: the device comprises a base, an independent inertia measurement unit and a fool-proof piece, wherein the independent inertia measurement unit comprises a unit main body and a wiring harness connector; the independent inertia measurement unit is arranged on the base, the fool-proof piece is arranged on the base, and the fool-proof piece is positioned on one side of the independent inertia measurement unit; the height of the fool-proof piece is higher than the lower surface of the wire harness connector, and the distance between the fool-proof piece and the unit main body is smaller than the length of the wire harness connector.
2. The inertial measurement unit assembly structure of claim 1, wherein: the fool-proof member is lower in height than the upper surface of the unit main body.
3. The inertial measurement unit assembly structure of claim 1, wherein: the unit body has four sides, and the harness connector is located on one side of the unit body.
4. The inertial measurement unit assembly structure of claim 3, wherein: the independent inertia measurement unit further comprises two installation parts, and the two installation parts are symmetrically located on two opposite side faces of the unit main body.
5. The inertial measurement unit assembly structure of claim 4, wherein: the installation department is equipped with the screw hole, the installation department spiro union in the base.
6. The inertial measurement unit assembly structure of claim 5, wherein: the harness connector and the unit main body are integrally formed, and when the independent inertia measurement unit is correctly installed, the fool-proof piece is located on one side of the unit main body and opposite to the harness connector.
7. The inertial measurement unit assembly structure of claim 1, wherein: the fool-proof piece is a fool-proof bolt, and the fool-proof bolt is installed on the base.
8. The inertial measurement unit assembly structure of claim 1, wherein: the fool-proof piece is of a columnar structure and is installed on the base.
9. The inertial measurement unit assembly structure of claim 1, wherein: the fool-proof piece is of a cone-shaped body structure and is installed on the base.
10. The inertial measurement unit assembly structure of claim 1, wherein: the fool-proof piece is detachably arranged on the base.
CN201920622634.9U 2019-04-30 2019-04-30 Inertia measurement unit assembly structure with prevent slow-witted design Active CN209841057U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920622634.9U CN209841057U (en) 2019-04-30 2019-04-30 Inertia measurement unit assembly structure with prevent slow-witted design

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920622634.9U CN209841057U (en) 2019-04-30 2019-04-30 Inertia measurement unit assembly structure with prevent slow-witted design

Publications (1)

Publication Number Publication Date
CN209841057U true CN209841057U (en) 2019-12-24

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920622634.9U Active CN209841057U (en) 2019-04-30 2019-04-30 Inertia measurement unit assembly structure with prevent slow-witted design

Country Status (1)

Country Link
CN (1) CN209841057U (en)

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Effective date of registration: 20220331

Address after: 310051 No. 1760, Jiangling Road, Hangzhou, Zhejiang, Binjiang District

Patentee after: ZHEJIANG GEELY HOLDING GROUP Co.,Ltd.

Patentee after: Zhejiang liankong Technology Co., Ltd

Address before: 310051 No. 1760, Jiangling Road, Hangzhou, Zhejiang, Binjiang District

Patentee before: ZHEJIANG GEELY HOLDING GROUP Co.,Ltd.

Patentee before: Zhejiang Geely Automobile Research Institute Co., Ltd