Patent ID: 12261356

DESCRIPTION OF EMBODIMENTS

Embodiments of this application provide an antenna apparatus, to change flowing of an airflow at a surface boundary layer when the airflow passes through a surface of the antenna apparatus, thereby reducing a resultant force of windload and improving safety of connecting a radome to a communications tower.

In this specification, the claims, and the accompanying drawings of this application, terms “first”, “second”, “third”, “fourth”, and the like (if existent) are intended to distinguish between similar objects but do not necessarily indicate a specific order or sequence. It should be understood that the data used in such a way are interchangeable in appropriate circumstances, so that embodiments described herein can be implemented in an order other than the content illustrated or described herein. In addition, terms such as “include”, “have”, and any variations thereof are intended to cover non-exclusive inclusions, for example, a process, method, system, product, or device that includes a series of steps or units is not necessarily limited to those clearly listed steps or units, but may include other steps or units that are not clearly listed or inherent to such a process, method, product, or device.

Implementation principles and specific implementations of technical solutions in this application and beneficial effects that can be correspondingly achieved by the technical solutions are described below in detail with reference to the accompanying drawings.

FIG.1is a schematic diagram of a structure of an antenna apparatus according to this application.

The antenna apparatus includes an antenna body101, a radome102, a mounting assembly103, and a pole104. The antenna body101is disposed in the radome102, a fixing point is disposed on a surface of the radome102, the fixing point is configured to fasten the mounting assembly103, and the mounting assembly103is configured to fasten the radome102and the pole104.

It may be understood that there may be one, two, or more antenna bodies101built in the radome102. This is not specifically limited herein.

The mounting assembly103may be movably connected to the radome102by using a bolt, or the mounting assembly103may be fastened to the radome102through pasting. It may be understood that the mounting assembly103may be connected to the radome102in another manner, provided that the mounting assembly103is tightly connected to the radome102. This is not specifically limited herein.

For example, when the mounting assembly103is movably connected to the radome102by using a bolt, the mounting assembly103includes a base with bolt holes. The bolt holes of the base are in a one-to-one correspondence with bolt holes on a side surface of the radome, so that the base can be fastened to the radome by using the bolt. The mounting assembly103is fastened to the base. The other side of the mounting assembly103may also be movably connected to the pole104by using a bolt. It may be understood that the mounting assembly103may not be movably connected to the radome102by using the base with bolt holes, but is directly movably connected to the radome102by using bolt holes on one side of the mounting assembly103. This is not specifically limited herein.

In an actual application process, the mounting assembly103may be alternatively tightly connected to the radome102by using a top surface of the radome102. This is not specifically limited herein. For example, bolt holes are disposed on the top surface of the radome102, and the mounting assembly103is tightly connected to the radome102by using the bolt holes on the top surface of the radome102.

The pole104may be shaped in a cylinder or a cuboid, or may be a pole of another shape. This is not specifically limited herein.

The following describes the antenna apparatus in this application in detail with reference to the foregoing structure of the antenna apparatus.

FIG.2is a schematic diagram of a structure of an antenna according to this application.

The antenna includes a radome201, an antenna body202, an upper-end cover203, and a lower-end cover204. The antenna body202is built in the radome201. The upper-end cover203is tightly connected to an upper end of the radome201, and the lower-end cover204is tightly connected to a lower end of the radome201, so that the upper-end cover203, the radome201, and the lower-end cover204form an entire antenna apparatus.

As shown inFIG.2, in an actual application process, bolt holes may be disposed on the lower-end cover204and/or the upper-end cover203, and the lower-end cover204and/or the upper-end cover203are or is tightly connected to the radome201by using the bolt holes of the lower-end cover204and/or the upper-end cover203. It may be understood that the lower-end cover204and/or the upper-end cover203may be tightly connected to the radome201in another manner. For example, the lower-end cover204and/or the upper-end cover203are or is tightly connected to the radome201through a buckle connection. For example, buckle slots or a buckle slot are or is disposed on the lower-end cover204and/or the upper-end cover203, and buckles are disposed at the upper end or the lower end of the radome201, so that when the lower end or the upper end of the radome201is connected to the lower-end cover204and/or the upper-end cover203, a lower-end buckle part or an upper-end buckle part of the radome201is exactly built into the buckle slot, and therefore the lower-end cover204and/or the upper-end cover203are tightly connected to the radome201. It may be understood that the upper-end cover203and the lower-end cover204may be connected to the radome in another manner. This is not specifically limited herein.

An interference structure is disposed on the side surface (an arc-shaped corner surface) of the radome201, and the interference structure is configured to change flowing of an airflow at a surface boundary layer when the airflow passes through a surface of the radome, to reduce windload.

It may be understood that, in an actual application process, four corners of a cross section of the radome may be of another shape. For example, the four corners of the cross section of the radome may be right angles. This is not specifically limited herein.

Optionally, in a possible implementation, as shown inFIG.2, the interference structure may be a tripwire205, and the tripwire205is disposed on the side surface of the radome201. The tripwire205may be obtained by performing special process processing on the radome201, or may be pasted to the surface of the radome201. This is not specifically limited herein.

For example, the tripwire205may be obtained through an extrusion process when the radome is produced. It may be understood that the tripwire205may be alternatively obtained through a knurling process, a molding process, a blister molding process, an injection molding process, or a blow molding process when the radome is produced. This is not specifically limited herein.

FIG.3is a cross-sectional view of a radome. As shown inFIG.3, the tripwire205may be a tripwire protruding from the side surface of the radome. It may be understood that the tripwire205may be a tripwire of another form.FIG.4is a cross-sectional view of a radome. As shown inFIG.4, the tripwire205may be a tripwire recessed in the side surface of the radome. A specific existence form of the tripwire is not limited herein.

In an actual application process, the tripwire205may be alternatively disposed on another surface of the radome.FIG.5is a cross-sectional view of a radome. For example, as shown inFIG.5, the tripwire205is disposed on three side surfaces of the radome. It may be understood that the tripwire may be alternatively disposed on another surface of another radome. This is not specifically limited herein.

Optionally, in a possible implementation, as shown inFIG.2, the interference structure may be a rough point206, and the rough point206is disposed on the side surface of the radome201. The rough point206may be obtained by performing special process processing on the radome201, or may be pasted to the surface of the radome201. This is not specifically limited herein.

For example, the rough point206may be obtained through an extrusion process when the radome is produced. It may be understood that the rough point206may be alternatively obtained through a knurling process, a molding process, a blister molding process, an injection molding process, or a blow molding process when the radome is produced, or a material molding parameter is adjusted when the radome is produced, so that a rough point is formed on the surface of the radome. This is not specifically limited herein.

FIG.6is a cross-sectional view of a radome. As shown inFIG.6, the rough point206may be a circular convex or concave point protruding from the side surface of the radome. It may be understood that the rough point206may be a rough point of another form.FIG.7is a cross-sectional view of a radome. For example, as shown inFIG.7, the rough point206may be a polygonal convex or concave point. The rough point206may be alternatively a rough point of another shape. This is not specifically limited herein.

In an actual application process, the rough point206may be alternatively disposed on another surface of the radome. For example, the rough point206is disposed on three surfaces of the radome. It may be understood that the rough point may be alternatively disposed on another surface of another radome. This is not specifically limited herein.

In a possible implementation, the interference structure may alternatively include both the tripwire205and the rough point206. This is not specifically limited herein.

When the antenna is installed on the pole, the antenna is in a high-altitude environment, and strength of an airflow is relatively large. In a process in which the airflow passes through a surface of the antenna, because airflows are from different angles, when there is a deviation angle between the antenna and a wind direction of the airflow; the radome is like an airplane wing and boundary layer separation is relatively late because of a streamline type feature of the antenna.FIG.8is a cross-sectional view of a radome. As shown inFIG.8, an airflow velocity on an upper surface of the antenna is large, an airflow velocity on a lower surface is small. According to Bernoulli's principle, pressure is small on the upper surface with a large airflow velocity, and pressure is large on the lower surface with a small airflow velocity. Therefore, a relatively large lift force acts on the antenna. When the lift force and a resistance are combined, a relatively large resultant force of windload acts on the antenna. The resultant force of windload acting on the antenna is finally transmitted to the pole through the mounting assembly. Therefore, the pole is subjected to relatively large windload, and safety of the antenna and the pole is affected.

In this embodiment of this application, the interference structure such as the tripwire205or the rough point206is disposed on the surface of the radome201. Therefore, when the airflow passes through the interference structure such as the tripwire205or the rough point206on the surface of the radome201, flowing of the airflow at the surface boundary layer is changed, and a turbulent wake is generated on the surface of the antenna, as shown inFIG.9.FIG.9is a cross-sectional view of a radome. Therefore, the antenna is in a stalled state, and the lift force significantly decreases, so that the resultant force of windload acting on the antenna decreases, and the windload on the pole is reduced, thereby improving safety of the antenna and the pole.

In several embodiments provided in this application, it should be understood that the disclosed apparatuses and methods may be implemented in other manners. For example, the described apparatus embodiment is merely an example. For example, division into the units is merely logical function division and may be other division in actual implementation. For example, a plurality of units or components may be combined or integrated into another system, or some features may be ignored or not performed. In addition, the displayed or discussed mutual couplings or direct couplings or communications connections may be implemented through some interfaces. The indirect couplings or communications connections between the apparatuses or units may be implemented in electrical, mechanical, or another form.

The units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one position, or may be distributed on a plurality of network units. Some or all of the units may be selected based on actual requirements to achieve the objectives of the solutions of embodiments.

In addition, function units in embodiments of this application may be integrated into one processing unit, each of the units may exist alone physically, or two or more units may be integrated into one unit. The integrated unit may be implemented in a form of hardware, or may be implemented in a form of a software function unit.