CN108011176B - Array frame structure - Google Patents
Array frame structure Download PDFInfo
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- CN108011176B CN108011176B CN201711219559.3A CN201711219559A CN108011176B CN 108011176 B CN108011176 B CN 108011176B CN 201711219559 A CN201711219559 A CN 201711219559A CN 108011176 B CN108011176 B CN 108011176B
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- array
- frame
- array frame
- darkroom
- frame structure
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
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- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Panels For Use In Building Construction (AREA)
Abstract
The invention provides a novel array surface array frame structure, which comprises a wall body, a darkroom, a reinforcing frame, an array surface array frame and a rotary table, wherein the darkroom, the reinforcing frame, the array surface array frame and the rotary table are positioned in the wall body; the array frame is of an aluminum framework skin structure, so that the weight is favorably reduced; the array frame has small self-weight, which is beneficial to reducing deformation and improving rigidity.
Description
Technical Field
The invention relates to a structural design form, in particular to a array surface array frame structure.
Background
The array frame is a specially designed structural frame, has the functions of installing and supporting the radiation antenna array to form a radiation field, provides a platform field for the maintenance of the radiation antenna array and the placement of radio frequency feed system equipment, and provides a working platform and a space for system installation, integration, debugging and maintenance for workers. The wavefront array frame tends to be large in size and mass due to the need for radius of curvature and surface area, which in turn leads to a weakening in stiffness. In order to improve the rigidity, the specifications of the section bars and the plates of the array frame are further increased, and finally the mass of the array frame reaches hundreds of tons, and the array frame can only be placed on the bottom layer, so that the placement space is limited.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to provide a array surface array frame structure which is light in weight, high in rigidity and high in space utilization rate, can fully utilize the existing space, maximizes the curvature radius and the surface area of the array surface, and is light in overall weight and high in rigidity.
According to one aspect of the invention, the array surface array frame structure comprises a wall body, a darkroom, a reinforcing frame, an array surface array frame and a rotary table, wherein the darkroom, the reinforcing frame, the array surface array frame and the rotary table are all located inside the wall body, the reinforcing frame, the array surface array frame and the rotary table are all located inside the darkroom, the array surface array frame is fixed on the reinforcing frame, and the rotary table is located on one side of the reinforcing frame.
Preferably, the array frame is a spherical sector of revolution.
Preferably, the array frame of the array is arranged along the diagonal of the darkroom.
Preferably, the array frame is an upper aluminum framework skin structure.
Preferably, the skin is attached to the array frame by rivets.
Preferably, the stiffening frame and the front array frame are connected by welding.
Preferably, the reinforcing frame is a lattice frame structure.
Compared with the prior art, the invention has the following beneficial effects:
1. the radius of curvature is maximized. The array frame of the invention is arranged along the diagonal line of the darkroom, realizes the maximization of the curvature radius of the array frame of the array surface, solves the problem that the curvature radius of the array frame of the prior inverted or side-standing bowl type array surface is relatively small,
the problem of low space utilization rate;
2. the weight is light. By adopting the aluminum structure and the optimized design of the reinforcing frame, the quality of the array frame is only one tenth of that of a steel array surface array frame with the same specification;
3. the cost is low. By reducing the quality, the array surface array frame cost is obviously reduced compared with the existing design;
4. the rigidity is high. By adopting the aluminum material and the reinforcing frame, the array surface array frame has higher rigidity;
5. the adaptability is good. The invention has no special requirement on the bearing capacity of floors, and solves the problems that the prior array plane array frame can only be placed on the bottom layer, if the array plane array frame is not on the bottom layer, the design needs to be planned in advance at the beginning of the design of a laboratory, and otherwise, the array plane array frame cannot be additionally built at the later stage.
The array frame structure design form of the array surface has light weight, high rigidity and high space utilization rate, can fully utilize the existing space, maximizes the curvature radius and the surface area of the array surface, and has light overall weight and high rigidity. The array surface array frame solves the problems that the existing array surface array frame is large in mass, high in cost, limited in curvature radius, incapable of maximizing, and required to be arranged on the bottom layer, and incapable of being built in later period.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
FIG. 1 is a top view of a wavefront array frame structure according to the present invention.
FIG. 2 is a cross-sectional view of a wavefront array frame structure of the present invention.
FIG. 3 is a front view of one array frame configuration of the present invention.
Detailed Description
The present invention will be described in detail with reference to specific examples. The following examples will assist those skilled in the art in further understanding the invention, but are not intended to limit the invention in any way. It should be noted that variations and modifications can be made by persons skilled in the art without departing from the spirit of the invention. All falling within the scope of the present invention.
As shown in fig. 1, the array frame structure of the array surface of the invention comprises a wall body 1, a darkroom 2, a reinforcing frame 3, an array surface frame 4 and a turntable 5, wherein the darkroom 2, the reinforcing frame 3, the array surface frame 4 and the turntable 5 are all positioned in the wall body 1, the reinforcing frame 3, the array surface frame 4 and the turntable 5 are all positioned in the darkroom 2, the array surface frame 4 is fixed on the reinforcing frame 3, and the turntable 5 is positioned at one side of the reinforcing frame 3.
The array surface array frame 4 is a rotary spherical sector and is arranged along the diagonal line of the darkroom, so that the space utilization rate is maximized.
The array frame 4 is an aluminum framework skin structure, which is beneficial to reducing the weight.
The covering is connected with the array frame 4 through rivets, so that the covering is convenient to connect.
The reinforcing frame 3 and the array frame 4 are connected through welding, so that the structure is firmer.
The reinforcing frame 3 is of a grid frame structure, so that the strength of the reinforcing frame 3 can be increased.
In conclusion, the array surface array frame has high space utilization rate, and the curvature radius and the surface area are maximized; the array frame is of an aluminum framework skin structure, so that the weight is favorably reduced; the array frame has small self-weight, which is beneficial to reducing deformation and improving rigidity.
The foregoing description of specific embodiments of the present invention has been presented. It is to be understood that the present invention is not limited to the specific embodiments described above, and that various changes and modifications may be made by one skilled in the art within the scope of the appended claims without departing from the spirit of the invention.
Claims (6)
1. A array surface array frame structure is characterized by comprising a wall body, a darkroom, a reinforcing frame, an array surface array frame and a rotary table, wherein the darkroom, the reinforcing frame, the array surface array frame and the rotary table are all positioned in the wall body;
the darkroom comprises a rectangular array surface frame space on the ground; the array surface array frame is a rotary spherical sector and is arranged along the diagonal of the horizontal section of the darkroom.
2. The array frame structure of claim 1, characterized in that the array frame is a spherical sector of revolution.
3. The array frame structure of claim 1, wherein the array frame is an aluminum-based skeletal skin structure.
4. The array frame structure of claim 3, wherein the skin is attached to the array frame by rivets.
5. The array frame structure of claim 1, wherein the stiffener and array frame are joined by welding.
6. The array frame structure of claim 1, wherein the stiffener is a lattice frame structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201711219559.3A CN108011176B (en) | 2017-11-28 | 2017-11-28 | Array frame structure |
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CN201711219559.3A CN108011176B (en) | 2017-11-28 | 2017-11-28 | Array frame structure |
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CN108011176A CN108011176A (en) | 2018-05-08 |
CN108011176B true CN108011176B (en) | 2020-07-14 |
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CN201711219559.3A Active CN108011176B (en) | 2017-11-28 | 2017-11-28 | Array frame structure |
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Citations (5)
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---|---|---|---|---|
CN203406411U (en) * | 2013-08-22 | 2014-01-22 | 中国电子科技集团公司第三十八研究所 | Composite material antenna backboard used for radar array plane electric connection |
CN104535858A (en) * | 2014-12-18 | 2015-04-22 | 北京无线电计量测试研究所 | Compact field antenna measurement synchronization reflection point region determination method |
CN104596357A (en) * | 2013-11-01 | 2015-05-06 | 上海机电工程研究所 | Radio frequency/optical semi-physical simulation composite target simulation system |
CN204536364U (en) * | 2014-12-31 | 2015-08-05 | 苏州市大富通信技术有限公司 | For the testing apparatus of antenna intermodulation testing |
TW201619619A (en) * | 2014-11-26 | 2016-06-01 | 泓淋科技有限公司 | Microwave dark room with absorbing body changing reflection path |
-
2017
- 2017-11-28 CN CN201711219559.3A patent/CN108011176B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN203406411U (en) * | 2013-08-22 | 2014-01-22 | 中国电子科技集团公司第三十八研究所 | Composite material antenna backboard used for radar array plane electric connection |
CN104596357A (en) * | 2013-11-01 | 2015-05-06 | 上海机电工程研究所 | Radio frequency/optical semi-physical simulation composite target simulation system |
TW201619619A (en) * | 2014-11-26 | 2016-06-01 | 泓淋科技有限公司 | Microwave dark room with absorbing body changing reflection path |
CN104535858A (en) * | 2014-12-18 | 2015-04-22 | 北京无线电计量测试研究所 | Compact field antenna measurement synchronization reflection point region determination method |
CN204536364U (en) * | 2014-12-31 | 2015-08-05 | 苏州市大富通信技术有限公司 | For the testing apparatus of antenna intermodulation testing |
Non-Patent Citations (2)
Title |
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"微波暗室面阵结构设计新方案";周艳阳,王李宁;《电子机械工程》;20100831;第26卷(第4期);第25-27页 * |
周艳阳,王李宁."微波暗室面阵结构设计新方案".《电子机械工程》.2010,第26卷(第4期), * |
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