CN218569505U - Integrated installation device of airborne power equipment - Google Patents
Integrated installation device of airborne power equipment Download PDFInfo
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- CN218569505U CN218569505U CN202222661394.8U CN202222661394U CN218569505U CN 218569505 U CN218569505 U CN 218569505U CN 202222661394 U CN202222661394 U CN 202222661394U CN 218569505 U CN218569505 U CN 218569505U
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Abstract
The application belongs to the technical field of airborne power supply equipment installation design, concretely relates to airborne power supply equipment integrated installation device includes: a frame; a plurality of brackets connected within the frame; each bracket is provided with a plurality of quick-release pins so as to be convenient for installing the power supply case installed by the bracket, and the power supply case installed by the bracket is installed in the frame; a plurality of brackets attached to the side walls of the frame; four supporting plate nuts are arranged on each support, so that the power panel boxes installed by the bolts can be conveniently installed, and the power panel boxes installed by the bolts are installed in the frame; the wiring harness laying rods are connected to the side wall of the frame and provide laying paths and fixing points for cross-linked wiring harnesses arranged among airborne power supply equipment in the frame; and the plurality of electrical separation surfaces are connected on the side wall of the frame and provide an external electrical switching surface for an external connection wire harness of the airborne power supply equipment installed in the frame.
Description
Technical Field
The application belongs to the technical field of installation and design of airborne power supply equipment, and particularly relates to an airborne power supply equipment integrated installation device.
Background
The airborne power supply equipment comprises a power supply case installed by a bracket and a power supply panel box installed by bolts, wherein the power supply case installed by the bracket is installed on the bracket by a plurality of quick-release pins, and the power supply panel box installed by the bolts is installed on a support by four bolts.
The airborne power supply equipment is numerous in quantity and different in size, if the airborne power supply equipment is dispersedly installed on an airplane, a large amount of space on the airplane can be occupied, the tension of airplane space resources is aggravated, if the airborne power supply equipment is intensively installed on the airplane, a complex cross-linking wire harness exists between the airborne power supply equipment, the outer cross-linking wire harness is numerous, the disassembly and assembly of the airborne power supply equipment are seriously interfered, and the airborne power supply equipment is inconvenient to overhaul.
The present application has been made in view of the above-mentioned technical drawbacks.
It should be noted that the above background disclosure is only used for assisting understanding of the inventive concept and technical solutions of the present invention, and does not necessarily belong to the prior art of the present patent application, and the above background disclosure should not be used for evaluating the novelty and inventive step of the present application in the case that there is no clear evidence that the above content is already disclosed at the filing date of the present application.
Disclosure of Invention
It is an object of the present application to provide an on-board power supply device integrated mounting arrangement that overcomes or mitigates at least one of the technical disadvantages of the known prior art.
The technical scheme of the application is as follows:
an on-board power supply device integrated mounting apparatus, comprising:
a frame;
a plurality of brackets connected within the frame; each bracket is provided with a plurality of quick-release pins so as to be convenient for installing the power supply case installed by the bracket, and the power supply case installed by the bracket is installed in the frame;
a plurality of brackets attached to the side walls of the frame; four supporting plate nuts are arranged on each bracket so as to be convenient for installing the power panel box installed by the bolts, and the power panel box installed by the bolts is installed in the frame;
the wiring harness laying rods are connected to the side wall of the frame and provide laying paths and fixing points for cross-linked wiring harnesses arranged among airborne power supply equipment in the frame;
and the plurality of electrical separation surfaces are connected on the side wall of the frame and provide an external electrical switching surface for an external connection wire harness of the airborne power supply equipment installed in the frame.
According to at least one embodiment of the application, in the onboard power supply equipment integration installation device, each bracket is positioned below the frame;
each bracket is located above the frame.
According to at least one embodiment of the application, in the integrated installation device of airborne power supply equipment, each support comprises two support rods, wherein the two support rods are arranged in parallel, and each support rod is provided with two supporting plate nuts.
According to at least one embodiment of the application, in the integrated mounting device for onboard power supply equipment, each electrical separation surface is provided with a plurality of connectors and binding posts, wherein the connectors are used for external electrical switching of small-current external connection wiring harnesses or signal wiring harnesses of onboard power supply equipment mounted in the frame, and the binding posts are used for external electrical switching of large-current external connection wiring harnesses of onboard power supply equipment mounted in the frame.
Drawings
Fig. 1 is a schematic view of an onboard power supply equipment integrated installation device provided by an embodiment of the present application;
wherein:
1-a frame; 2-a bracket; 3-a scaffold; 4-laying a wire harness; 5-electrical separation plane.
For the purpose of better illustrating the present embodiments, certain elements of the drawings may be omitted, enlarged or reduced, and do not represent the size of an actual product; furthermore, the drawings are for illustrative purposes only and are not to be construed as limiting the patent.
Detailed Description
In order to make the technical solutions and advantages of the present application clearer, the technical solutions of the present application will be further clearly and completely described in the following detailed description with reference to the accompanying drawings, and it should be understood that the specific embodiments described herein are only some of the embodiments of the present application, and are only used for explaining the present application, but not limiting the present application. It should be noted that, for convenience of description, only the parts related to the present application are shown in the drawings, other related parts may refer to general designs, and the embodiments and technical features in the embodiments in the present application may be combined with each other to obtain a new embodiment without conflict.
In addition, unless otherwise defined, technical or scientific terms used in the description of the present application shall have the ordinary meaning as understood by one of ordinary skill in the art to which the present application belongs. The terms "upper", "lower", "left", "right", "center", "vertical", "horizontal", "inner", "outer", and the like used in the description of the present application, which indicate orientations, are used only to indicate relative directions or positional relationships, and do not imply that devices or elements must have specific orientations, be constructed and operated in specific orientations, and that when the absolute position of an object to be described is changed, the relative positional relationships may be changed accordingly, and thus, should not be construed as limiting the present application. The use of "first," "second," "third," and the like in the description of the present application is for descriptive purposes only to distinguish between different components and is not to be construed as indicating or implying relative importance. The use of the terms "a," "an," or "the" and similar referents in the context of describing the application is not to be construed as an absolute limitation on the number, but rather as the presence of at least one. The word "comprising" or "comprises", and the like, when used in this description, is intended to specify the presence of stated elements or items, but not the exclusion of any other elements or items.
Further, it should be noted that, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and the like as used in the description of the present application are to be construed broadly, e.g., the connection may be a fixed connection, a detachable connection, or an integral connection; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, or they may be connected through the inside of two elements, and those skilled in the art can understand their specific meaning in this application according to the specific situation.
The present application is described in further detail below with reference to fig. 1.
An on-board power supply device integrated mounting apparatus, comprising:
the frame 1 can be designed with corresponding bolt connecting joints and is connected to an airplane through bolts;
a plurality of brackets 2 connected within the frame 1; each bracket 2 is provided with a plurality of quick-release pins so as to be convenient for installing the power supply case installed by the bracket, and the power supply case installed by the bracket is installed in the frame 1;
a plurality of brackets 3 connected to the side walls of the frame 1; four supporting plate nuts are arranged on each bracket 3 so as to be convenient for installing the power panel box installed by the bolts, and the power panel box installed by the bolts is installed in the frame 1;
a plurality of harness laying rods 4 connected to the side wall of the frame 1, for providing laying paths and fixing points for cross-linked harnesses installed between on-board power supply devices in the frame 1;
and the plurality of electrical separation surfaces 5 are connected to the side wall of the frame 1 and provide external electrical switching surfaces for external connection wiring harnesses of on-board power supply equipment arranged in the frame 1.
For the integrated installation device of the onboard power supply equipment disclosed in the above embodiment, it can be understood by those skilled in the art that the integrated installation device is designed to install a plurality of power supply chassis installed by brackets by means of quick-release pins through a plurality of brackets 2 connected in the frame 1, and install a plurality of power supply chassis installed by means of bolts by means of a plurality of brackets 3 connected to the side wall of the frame 1 and support plate nuts, so as to realize the integrated installation of a plurality of power supply chassis installed by means of brackets and power supply chassis installed by means of bolts in the frame 1, thereby saving the space on the aircraft.
To the integrated installation device of airborne power equipment disclosed in the above embodiment, as can be understood by those skilled in the art, the integrated installation device is designed to provide a laying path and a fixing point thereof for a cross-linked wire harness installed between airborne power equipment in the frame 1 by using a plurality of wire harness laying rods 4 connected to the side wall of the frame 1, and to provide an external electrical switching surface for an external wire harness installed on airborne power equipment in the frame 1 by using a plurality of electrical separation surfaces 5 connected to the side wall of the frame 1, so that the degree of interference in the disassembly and assembly of the airborne power equipment installed in the frame 1 can be reduced, and the airborne power equipment installed in the frame 1 can be conveniently overhauled.
In some alternative embodiments, in the above-mentioned onboard power supply equipment integrated installation device, each bracket 2 is located below the frame 1;
each bracket 3 is located above the frame 1.
For the integrated installation device of the airborne power supply equipment disclosed in the above embodiment, it can be understood by those skilled in the art that each bracket 2 is designed to be located below the frame 1, and each bracket 3 is designed to be located above the frame 1, that is, the power supply chassis installed by the bracket is designed to be installed in a centralized manner below the frame 1, and the power supply chassis installed by the bolts are designed to be installed in a centralized manner above the frame 1, so that the integrated installation device has greater convenience in practice.
In some optional embodiments, in the above-mentioned integrated mounting device for an onboard power supply device, each bracket 3 includes two struts, where the two struts are arranged in parallel, and two pallet nuts are provided on each strut.
In some optional embodiments, in the above-mentioned integrated mounting apparatus for onboard power supply equipment, each electrical separation surface 5 is provided with a plurality of connectors and terminals, wherein the connectors are used for external electrical switching of the small-current external connection harness or the signal harness of the onboard power supply equipment mounted in the frame 1, and the terminals are used for external electrical switching of the large-current external connection harness of the onboard power supply equipment mounted in the frame 1.
In the integrated mounting device for onboard power supply equipment disclosed in the above embodiments, the specific number of the brackets 2, the brackets 3, the harness-laying rods 4 and the electrical separation surfaces 5 thereof and the distribution positions on the frame 1 may be determined by those skilled in the art according to specific practical applications when applying the technical solutions disclosed in this application, and are not further limited herein.
The embodiments are described in a progressive manner in the specification, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other.
Having thus described the present invention in connection with the preferred embodiments illustrated in the accompanying drawings, it will be understood by those skilled in the art that the scope of the present invention is not limited to those specific embodiments, and that equivalent changes or substitutions of the related technical features may be made by those skilled in the art without departing from the principle of the present invention, and those technical aspects after such changes or substitutions will fall within the scope of the present invention.
Claims (4)
1. An integrated installation device of airborne power equipment, comprising:
a frame (1);
a plurality of brackets (2) connected within the frame (1); each bracket (2) is provided with a plurality of quick-release pins so as to be convenient for installing the power supply case installed by the bracket, and the power supply case installed by the bracket is installed in the frame (1);
a plurality of brackets (3) connected to the side walls of the frame (1); four supporting plate nuts are arranged on each bracket (3) so as to be convenient for installing the power panel box installed by bolts, and the power panel box installed by bolts is installed in the frame (1);
a plurality of harness laying rods (4) connected to the side wall of the frame (1) and providing laying paths and fixing points for cross-linked harnesses installed between on-board power supply devices in the frame (1);
the electrical separation surfaces (5) are connected to the side wall of the frame (1) and provide external electrical switching surfaces for external connection wiring harnesses of on-board power equipment installed in the frame (1).
2. The on-board power supply equipment integrated mounting device of claim 1,
each of the brackets (2) is located below the frame (1);
each of the brackets (3) is located above the frame (1).
3. The on-board power supply equipment integrated mounting device of claim 1,
each support (3) comprises two supporting rods, wherein the two supporting rods are arranged in parallel, and each supporting rod is provided with two supporting plate nuts.
4. The on-board power supply equipment integrated mounting device of claim 1,
each electrical separation surface (5) is provided with a plurality of connectors and binding posts, wherein the connectors are used for externally electrically switching small-current externally-connected wiring harnesses or signal wiring harnesses of on-board power supply equipment arranged in the frame (1), and the binding posts are used for externally electrically switching large-current externally-connected wiring harnesses of on-board power supply equipment arranged in the frame (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222661394.8U CN218569505U (en) | 2022-10-10 | 2022-10-10 | Integrated installation device of airborne power equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222661394.8U CN218569505U (en) | 2022-10-10 | 2022-10-10 | Integrated installation device of airborne power equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218569505U true CN218569505U (en) | 2023-03-03 |
Family
ID=85316139
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222661394.8U Active CN218569505U (en) | 2022-10-10 | 2022-10-10 | Integrated installation device of airborne power equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218569505U (en) |
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2022
- 2022-10-10 CN CN202222661394.8U patent/CN218569505U/en active Active
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