CN213660629U - High-strength honeycomb interlayer antenna housing - Google Patents

High-strength honeycomb interlayer antenna housing Download PDF

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Publication number
CN213660629U
CN213660629U CN202022786500.6U CN202022786500U CN213660629U CN 213660629 U CN213660629 U CN 213660629U CN 202022786500 U CN202022786500 U CN 202022786500U CN 213660629 U CN213660629 U CN 213660629U
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China
Prior art keywords
strengthening rib
covering
honeycomb panel
honeycomb
sandwich structure
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CN202022786500.6U
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Chinese (zh)
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颜景玉
公伟
刘露
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Nanjing Youqiao Electronic Technology Co ltd
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Nanjing Youqiao Electronic Technology Co ltd
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Abstract

The utility model belongs to the technical field of the radar antenna technique and specifically relates to a high strength honeycomb intermediate layer antenna house, including enclosing frame, last covering, covering and load layer down, the load layer sets up and constitutes outer sandwich structure between last covering and lower covering, enclose the frame parcel outer sandwich structure around, a plurality of horizontal strengthening ribs and a plurality of vertical strengthening rib staggered arrangement cut apart into a plurality of bearing regions with the load layer, and every bearing region has all placed the carrier block, the carrier block includes honeycomb panel, lower honeycomb panel and reinforcing plate, the reinforcing plate sets up and constitutes interior sandwich structure between last honeycomb panel and lower honeycomb panel, the utility model discloses can solve the poor problem of antenna house rigidity among the prior art.

Description

High-strength honeycomb interlayer antenna housing
Technical Field
The utility model relates to a radar antenna technical field, concrete field is a high strength honeycomb intermediate layer antenna house.
Background
The radar antenna feeder system is an important component of a radar system and is mainly used for transmitting or receiving electromagnetic wave signals. In the process of the electromagnetic wave propagating in the space, the intensity of the electromagnetic wave is inversely proportional to the transmission distance, and in order to increase the action distance, the power of the transmitted electromagnetic wave signal needs to be increased. When high-power electromagnetic waves are transmitted in the radar antenna feeder system, air breakdown is caused due to overhigh electric field intensity, and therefore a sparking phenomenon is generated in the antenna feeder system, namely, physical damage of antenna feeder devices is caused, and harmonic components of the electromagnetic waves are generated to influence the signal-to-noise ratio of radar signals.
Because the breakdown field intensity is in direct proportion to the gas pressure of the antenna feeder system and in inverse proportion to the water content of the gas, the measures for solving the ignition of the high-power radar antenna feeder system are mainly two: charging a high pressure gas and drying the charged gas.
This puts higher demands on the sealing of the antenna system and the design of the radome.
Traditional radome mainly seals the antenna face, avoids steam and dust to enter into the antenna face, causes antenna face corrosion or pollution, consequently, traditional radome has the poor problem of rigidity. The high-power antenna system requires that air in the antenna feeder system is firstly pumped out and then dried high-pressure air is filled in, and the antenna housing with poor rigidity cannot meet the requirement on strength.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a high strength honeycomb intermediate layer antenna house to solve the poor problem of antenna house rigidity among the prior art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a high strength honeycomb intermediate layer antenna house, includes encloses the frame, goes up the covering, covering and load layer down, load layer sets up constitutes outer sandwich structure between last covering and lower covering, enclose the frame parcel outer sandwich structure around, a plurality of horizontal strengthening ribs and a plurality of vertical strengthening rib staggered arrangement divide into a plurality of bearing regions with load layer, and bearing block has all been placed in every bearing region, bearing block includes honeycomb panel, honeycomb panel and reinforcing plate down, the reinforcing plate sets up and constitutes interior sandwich structure between last honeycomb panel and lower honeycomb panel.
Preferably, there is one horizontal strengthening rib, horizontal strengthening rib is located the positive centre of antenna house and links to each other with vertical strengthening rib, vertical strengthening rib has three, and eight bearing area are evenly cut apart into with the bearer layer to a horizontal strengthening rib and three vertical strengthening ribs.
Preferably, the joint of the transverse reinforcing rib and the vertical reinforcing rib is provided with a matching groove.
Preferably, the upper skin, the lower skin and the enclosure frame are correspondingly provided with mounting and fixing holes.
Preferably, the upper skin, the lower skin, the transverse reinforcing ribs, the vertical reinforcing ribs and the reinforcing plates are all made of epoxy materials.
Compared with the prior art, the beneficial effects of the utility model are that: through the strengthening rib that increases intermediate level epoxy material, improved the bulk strength of antenna face, can bear the inside and outside pressure differential that antenna feeder system evacuation or add highly-compressed air and cause, reduce the electrical property loss of antenna house simultaneously.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is an exploded view of the present invention.
In the figure: the composite plate comprises an upper skin 1, a lower skin 2, a surrounding frame 3, transverse reinforcing ribs 4, vertical reinforcing ribs 5, an upper honeycomb plate 6, a lower honeycomb plate 7 and reinforcing plates 8.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, the present invention provides a technical solution: a high-strength honeycomb sandwich radome comprises a surrounding frame 3, an upper skin 1, a lower skin 2 and a bearing layer, wherein the bearing layer is arranged between the upper skin 1 and the lower skin 2 to form an outer sandwich structure, the surrounding frame 3 wraps the periphery of the outer sandwich structure, the bearing layer is divided into a plurality of bearing areas by the staggered arrangement of a plurality of transverse reinforcing ribs 4 and a plurality of vertical reinforcing ribs 5, concretely, in the embodiment, one transverse reinforcing rib 4 and three vertical reinforcing ribs 5 are arranged, the transverse reinforcing rib 4 is positioned in the middle of the radome and is connected with each vertical reinforcing rib 5, the whole bearing layer is divided into eight bearing areas by the transverse reinforcing ribs 4 and the three vertical reinforcing ribs 5, in order to ensure that the bearing capacity is more uniform, in the embodiment, the eight bearing areas are designed to be consistent in size, each bearing area is provided with a bearing block, each bearing block comprises an upper honeycomb plate 6, a lower honeycomb plate 7 and a reinforcing plate 8, the reinforcing plate 8 is arranged between the upper honeycomb panel 6 and the lower honeycomb panel 7 to form an inner sandwich structure.
Specifically, the joint of the transverse reinforcing rib 4 and the vertical reinforcing rib 5 is provided with a matching groove.
Further, the upper skin 1, the lower skin 2 and the surrounding frame 3 are correspondingly provided with mounting and fixing holes, and connecting pieces such as bolts can be adopted to penetrate through the mounting and fixing holes to fix the upper skin 1, the lower skin 2 and the surrounding frame 3 together to form an external support, so that the damage of the internal honeycomb plate is avoided.
Preferentially, the upper covering 1, the lower covering 2, the transverse reinforcing ribs 4, the vertical reinforcing ribs 5 and the reinforcing plates 8 are made of epoxy materials, the weight of the antenna housing can be reduced while the strength of the antenna housing is improved, and the electrical property loss of the antenna housing is reduced.
The application provides an antenna house has improved the bulk strength of antenna face through the strengthening rib that increases intermediate level epoxy material, can bear the inside and outside pressure differential that antenna feeder system evacuation or add highly-compressed air and cause, reduces the electrical property loss of antenna house simultaneously.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (5)

1. A high strength honeycomb intermediate layer antenna house which characterized in that: including enclosing frame (3), going up covering (1), covering (2) and load layer down, the load layer sets up and constitutes outer sandwich structure at last covering (1) under and between covering (2), enclose frame (3) parcel outer sandwich structure around, a plurality of horizontal strengthening rib (4) and a plurality of vertical strengthening rib (5) staggered arrangement divide into a plurality of bearing regions with the load layer, and bearing block has all been placed in every bearing region, bearing block includes honeycomb panel (6), honeycomb panel (7) and reinforcing plate (8) down, sandwich structure in reinforcing plate (8) set up between last honeycomb panel (6) and lower honeycomb panel (7).
2. The high-strength honeycomb sandwich radome of claim 1, wherein: horizontal strengthening rib (4) have one, horizontal strengthening rib (4) are located the positive centre of antenna house and link to each other with vertical strengthening rib (5), vertical strengthening rib (5) have three, and horizontal strengthening rib (4) and three vertical strengthening rib (5) evenly divide into eight bearing area with the bearer layer.
3. The high-strength honeycomb sandwich radome of claim 2, wherein: and a conjunction groove is formed at the joint of the transverse reinforcing rib (4) and the vertical reinforcing rib (5).
4. The high-strength honeycomb sandwich radome of claim 1, wherein: and the upper skin (1), the lower skin (2) and the enclosure frame (3) are correspondingly provided with mounting and fixing holes.
5. The high-strength honeycomb sandwich radome of claim 1, wherein: the upper skin (1), the lower skin (2), the transverse reinforcing ribs (4), the vertical reinforcing ribs (5) and the reinforcing plates (8) are all made of epoxy materials.
CN202022786500.6U 2020-11-26 2020-11-26 High-strength honeycomb interlayer antenna housing Active CN213660629U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022786500.6U CN213660629U (en) 2020-11-26 2020-11-26 High-strength honeycomb interlayer antenna housing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022786500.6U CN213660629U (en) 2020-11-26 2020-11-26 High-strength honeycomb interlayer antenna housing

Publications (1)

Publication Number Publication Date
CN213660629U true CN213660629U (en) 2021-07-09

Family

ID=76688085

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202022786500.6U Active CN213660629U (en) 2020-11-26 2020-11-26 High-strength honeycomb interlayer antenna housing

Country Status (1)

Country Link
CN (1) CN213660629U (en)

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