CN109149126A - Phased array antenna gap waveguide layer preparation process - Google Patents

Phased array antenna gap waveguide layer preparation process Download PDF

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Publication number
CN109149126A
CN109149126A CN201811003599.9A CN201811003599A CN109149126A CN 109149126 A CN109149126 A CN 109149126A CN 201811003599 A CN201811003599 A CN 201811003599A CN 109149126 A CN109149126 A CN 109149126A
Authority
CN
China
Prior art keywords
gap
waveguide layer
outer rim
array antenna
phased array
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201811003599.9A
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Chinese (zh)
Inventor
文忠
罗忠超
林虎
刘海
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chengdu Sail Com Technology Co Ltd
Original Assignee
Chengdu Sail Com Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chengdu Sail Com Technology Co Ltd filed Critical Chengdu Sail Com Technology Co Ltd
Priority to CN201811003599.9A priority Critical patent/CN109149126A/en
Publication of CN109149126A publication Critical patent/CN109149126A/en
Pending legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0087Apparatus or processes specially adapted for manufacturing antenna arrays

Abstract

The invention discloses the preparation processes of phased array antenna gap waveguide layer, the structure of gap waveguide layer is split as entity between outer rim and gap in the design phase, reach reduction difficulty of processing, improve machining accuracy, ensure the purpose of yields, it is processed between outer rim and gap after entity by most practical technique, then entity between outer rim and gap is assembled, welding or bonding can be used in a combination thereof mode.

Description

Phased array antenna gap waveguide layer preparation process
Technical field
The present invention relates to especially phased array antenna gap waveguide layer preparation processes.
Background technique
It is more and more in high frequency antenna to use phased array antenna with the development of radar and communication technology of satellite, in phase Gap waveguide layer is often used in control array antenna (such as CTS antenna, VCTS antenna) structure.Currently, gap in the prior art The common preparation process of ducting layer is added using monolith machine, and this preparation process is in the presence of structure is complicated, processing difficulties, cost High, the disadvantages of overall weight is big.
Summary of the invention
It is an object of the invention to overcome the deficiencies of the prior art and provide phased array antenna gap waveguide layer preparation processes.
The purpose of the present invention is achieved through the following technical solutions: a kind of phased array antenna gap waveguide layer preparation process, The gap waveguide layer is formed by outer rim and as entity between multiple gaps in outer rim, comprising the following steps:
S1. gap waveguide layer is split to design, i.e., the gap waveguide layer is split as entity two between outer rim and gap Part;
S2. because between gap solid cross-section it is identical, therefore processed by the way of extrudate, and outer rim then using mechanical plus Either type is processed in work, die casting or injection molding;
S3. solid profile and outer rim between the gap processed are combined into one.
Further, solid profile and the outer rim are connected by bonding way between the gap.
Further, solid profile and the outer rim are connected by welding manner between the gap.
Further, entity is hollow structure between the gap.
The invention has the following advantages that
1. simplifying structure, by complicated structurally reasonable fractionation, each section is made to become simple structure;
2. simplifying processing, outer rim installation positioning position precision is high after fractionation, and the processing is simple using extrudate for entity between gap;
3. reducing processing cost, entity is processed in a manner of profile between gap, and processing charges can be greatly reduced;
4. mitigating weight, entity is processed in a manner of profile between gap, can be made into hollow structure, overall weight can be effectively reduced.
Detailed description of the invention
Fig. 1 is the front elevation of gap waveguide layer;
Fig. 2 is the side view of gap waveguide layer;
Fig. 3 is the front elevation of outer rim;
Fig. 4 is the side view of outer rim;
The front elevation of Fig. 5 entity between single gap;
The side view of Fig. 6 entity between single gap.
Specific embodiment
To keep the purposes, technical schemes and advantages of inventive embodiments clearer, below in conjunction in the embodiment of the present invention Attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is this Invention a part of the embodiment, instead of all the embodiments.The present invention for usually describing and indicating in attached drawing here is implemented The component of example can be arranged and be designed with a variety of different configurations.Based on the embodiments of the present invention, ordinary skill Personnel's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
The present embodiment provides phased array antenna gap waveguide layer preparation processes.
Gap waveguide layer is as shown in Figure 1 and Figure 2, has outer rim 1, entity 3 and is made of entity between gap between gap Gap waveguide 2, first in the design phase, to gap ducting layer carry out it is reasonable split design, gap waveguide layer is split as Entity 3 between outer rim 1 and gap, such as the front elevation that Fig. 3 is outer rim 1 and the side view that Fig. 4 is outer rim 1, for another example Fig. 5 is The side view of the front elevation of entity 3 and Fig. 6 entity 3 between single gap between single gap, by complicated structurally reasonable fractionation, Each section is set to become simple structure, to achieve the purpose that simplified structure.
Suitable technique is selected to process entity 3 between the outer rim 1 and gap for splitting design, according to outer rim 1 Architectural characteristic may be selected add using machine, processed by the way of die casting or injection molding, and entity 3 then more uses shape extrusion between gap Mode it is processed;After fractionation sub-unit processing avoid overall processing structure is complicated, processing difficulties, it is at high cost and The big disadvantage of overall weight is realized and simplifies processing, and the precision at the installation positioning of outer rim 1 position is improved, and entity 3 passes through type between gap Material processing, is made into hollow structure, processing charges can be greatly reduced and overall weight is effectively reduced, facilitate installation personnel Installation operation in high altitude operation.
Entity 3 is assembled further according to the product parameters of phased array antenna between the outer rim 1 processed and gap, outside Entity 3 can be used the mode being bonded or welded and be combined into one between frame 1 and gap.
The phased array antenna gap waveguide layer manufactured by the technique has the following advantages:
Splitting gap waveguide layer structure is that processing greatly simplifies, and the simplification of processing is torn open simultaneously so that the expense of processing is greatly reduced Separation structure is processed so that the mode that shape extrusion can be used in entity 3 between gap is processed, by physical treatment between gap at Hollow structure, significantly mitigation weight of equipment.

Claims (4)

1. a kind of phased array antenna gap waveguide layer preparation process, the gap waveguide layer is by outer rim and as in outer rim Entity forms between multiple gaps, which comprises the following steps:
S1. gap waveguide layer is split to design, i.e., the gap waveguide layer is split as entity two between outer rim and gap Part;
S2. because between gap solid cross-section it is identical, therefore processed by the way of extrudate, and outer rim then using mechanical plus Either type is processed in work, die casting or injection molding;
S3. solid profile and outer rim between the gap processed are combined into one.
2. phased array antenna gap waveguide layer preparation process according to claim 1, which is characterized in that real between the gap Frame body sectional material and the outer rim are connected by bonding way.
3. phased array antenna gap waveguide layer preparation process according to claim 1, which is characterized in that real between the gap Frame body sectional material and the outer rim are connected by welding manner.
4. phased array antenna gap waveguide layer preparation process according to claim 1, which is characterized in that real between the gap Body is hollow structure.
CN201811003599.9A 2018-08-30 2018-08-30 Phased array antenna gap waveguide layer preparation process Pending CN109149126A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811003599.9A CN109149126A (en) 2018-08-30 2018-08-30 Phased array antenna gap waveguide layer preparation process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811003599.9A CN109149126A (en) 2018-08-30 2018-08-30 Phased array antenna gap waveguide layer preparation process

Publications (1)

Publication Number Publication Date
CN109149126A true CN109149126A (en) 2019-01-04

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811003599.9A Pending CN109149126A (en) 2018-08-30 2018-08-30 Phased array antenna gap waveguide layer preparation process

Country Status (1)

Country Link
CN (1) CN109149126A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115117616A (en) * 2022-08-25 2022-09-27 成都国恒空间技术工程股份有限公司 VICTS antenna based on RGW structure

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040080463A1 (en) * 2001-03-21 2004-04-29 Jeong Kyeong Hwan Waveguide slot antenna and manufacturing method thereof
CN201134511Y (en) * 2007-01-16 2008-10-15 北京海域天华通讯设备有限公司 Wave-guide gap array antenna
CN104105330A (en) * 2014-06-17 2014-10-15 合肥聚能电物理高技术开发有限公司 High-accuracy, high-strength and low-hybrid wave antenna structure and preparation technology
CN104518289A (en) * 2014-12-22 2015-04-15 中国电子科技集团公司第三十八研究所 Dual-polarized slotted waveguide antenna array
CN204424458U (en) * 2014-12-22 2015-06-24 中国电子科技集团公司第三十八研究所 Dual polarization slotted guide antenna battle array
CN105762491A (en) * 2016-02-03 2016-07-13 中国科学院国家空间科学中心 Terahertz transmission array antenna and preparation method thereof
CN106099337A (en) * 2016-01-12 2016-11-09 中国电子科技集团公司第十研究所 Large-scale K-band conformal antenna front and preparation method thereof
CN106784335A (en) * 2017-03-06 2017-05-31 东南大学 A kind of surface plasmon-polarition type heterogeneous integrated solar cell of conduction
CN106848601A (en) * 2017-01-17 2017-06-13 宁波大学 A kind of processing method of planar waveguide CTS array antennas
CN107732466A (en) * 2017-09-25 2018-02-23 陕西黄河集团有限公司 A kind of high-precision slotted waveguide antenna structure and manufacturing process
CN108258427A (en) * 2017-12-22 2018-07-06 珠海纳睿达科技有限公司 A kind of concealed feed ridge waveguide slot antenna

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040080463A1 (en) * 2001-03-21 2004-04-29 Jeong Kyeong Hwan Waveguide slot antenna and manufacturing method thereof
CN201134511Y (en) * 2007-01-16 2008-10-15 北京海域天华通讯设备有限公司 Wave-guide gap array antenna
CN104105330A (en) * 2014-06-17 2014-10-15 合肥聚能电物理高技术开发有限公司 High-accuracy, high-strength and low-hybrid wave antenna structure and preparation technology
CN104518289A (en) * 2014-12-22 2015-04-15 中国电子科技集团公司第三十八研究所 Dual-polarized slotted waveguide antenna array
CN204424458U (en) * 2014-12-22 2015-06-24 中国电子科技集团公司第三十八研究所 Dual polarization slotted guide antenna battle array
CN106099337A (en) * 2016-01-12 2016-11-09 中国电子科技集团公司第十研究所 Large-scale K-band conformal antenna front and preparation method thereof
CN105762491A (en) * 2016-02-03 2016-07-13 中国科学院国家空间科学中心 Terahertz transmission array antenna and preparation method thereof
CN106848601A (en) * 2017-01-17 2017-06-13 宁波大学 A kind of processing method of planar waveguide CTS array antennas
CN106784335A (en) * 2017-03-06 2017-05-31 东南大学 A kind of surface plasmon-polarition type heterogeneous integrated solar cell of conduction
CN107732466A (en) * 2017-09-25 2018-02-23 陕西黄河集团有限公司 A kind of high-precision slotted waveguide antenna structure and manufacturing process
CN108258427A (en) * 2017-12-22 2018-07-06 珠海纳睿达科技有限公司 A kind of concealed feed ridge waveguide slot antenna

Non-Patent Citations (5)

* Cited by examiner, † Cited by third party
Title
《化工百科全书》编辑委员会 编: "《化工百科全书 第8卷 计算机控制系统-聚硅氧烷 ji-ju》", 30 September 1994 *
姜义: "《大学物理演示实验》", 31 August 2016 *
廖健 等: "《铝合金挤压材生产与应用》", 31 March 2018 *
文根保 等: "《复杂注塑模现代设计》", 31 July 2018 *
邹子和 等: "《不锈钢管和型钢的热挤压》", 31 August 2014 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115117616A (en) * 2022-08-25 2022-09-27 成都国恒空间技术工程股份有限公司 VICTS antenna based on RGW structure
CN115117616B (en) * 2022-08-25 2022-12-02 成都国恒空间技术工程股份有限公司 VICTS antenna based on RGW structure
US11728575B1 (en) 2022-08-25 2023-08-15 Chengdu Guoheng Space Technology Engineering Co., Ltd. VICTS antenna based on RGW structure

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Application publication date: 20190104