WO2023127899A1 - アンテナ装置 - Google Patents

アンテナ装置 Download PDF

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Publication number
WO2023127899A1
WO2023127899A1 PCT/JP2022/048287 JP2022048287W WO2023127899A1 WO 2023127899 A1 WO2023127899 A1 WO 2023127899A1 JP 2022048287 W JP2022048287 W JP 2022048287W WO 2023127899 A1 WO2023127899 A1 WO 2023127899A1
Authority
WO
WIPO (PCT)
Prior art keywords
mount
base portion
power supply
antenna device
skirt
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.)
Ceased
Application number
PCT/JP2022/048287
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
太郎 上田
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to US18/691,894 priority Critical patent/US12218400B2/en
Priority to EP22916121.1A priority patent/EP4459792A4/en
Priority to JP2023535723A priority patent/JP7341377B1/ja
Publication of WO2023127899A1 publication Critical patent/WO2023127899A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/02—Arrangements for de-icing; Arrangements for drying-out ; Arrangements for cooling; Arrangements for preventing corrosion
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/002—Protection against seismic waves, thermal radiation or other disturbances, e.g. nuclear explosion; Arrangements for improving the power handling capability of an antenna
    • 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
    • H01Q1/22—Supports; Mounting means by structural association with other equipment or articles
    • H01Q1/2283—Supports; Mounting means by structural association with other equipment or articles mounted in or on the surface of a semiconductor substrate as a chip-type antenna or integrated with other components into an IC package
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061—Two dimensional planar arrays
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/32—Adaptation for use in or on road or rail vehicles
    • H01Q1/325—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle
    • H01Q1/3275—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle mounted on a horizontal surface of the vehicle, e.g. on roof, hood, trunk

Definitions

  • the present disclosure relates to an antenna device mounted on a mobile object.
  • Patent Document 1 For satellite communication antenna devices mounted on mobile objects such as aircraft, it is important to eliminate or minimize the increase in air resistance caused by mounting the antenna device. In moving objects, especially aircraft, fuel efficiency deteriorates as air resistance increases. In order to minimize the increase in air resistance, it is necessary to reduce the height and cross-sectional area of the antenna device when viewed from the nose side (nose direction). In order to reduce the height and cross-sectional area when viewed from the nose direction, an antenna device using a phased array system that electrically changes the directivity direction has been proposed (see, for example, Patent Document 1). In Patent Document 1, by using the phased array method, the height of the antenna device can be reduced compared to the mechanical drive method.
  • phased array type antenna device high heat dissipation is required because the heat generation density of the antenna portion increases compared to the mechanically driven type antenna device. 2. Description of the Related Art In a phased array type antenna device, there is an antenna device that air-cools exhaust heat from the antenna device using a heat pipe and heat radiating fins provided on the heat pipe (see, for example, Patent Document 2).
  • the antenna section is covered with a radome and is not directly exposed to the outside air.
  • a cooling device such as a fan inside the radome
  • the cooling device requires a space.
  • a space for providing a heat pipe inside the radome is required in order to cool the antenna section.
  • the antenna device described in Patent Document 2 has a problem that the height and cross-sectional area of the antenna device when viewed from the nose direction are increased by the space required for the heat pipe.
  • the present disclosure has been made to solve the above-described problems, and aims to obtain an antenna device that can obtain higher heat dissipation than before without increasing the height of the antenna device.
  • An antenna device includes a plurality of element antennas, an integrated circuit that operates the plurality of element antennas, and a plurality of element antennas mounted on one surface, and the other surface opposite to the one surface.
  • an array antenna having an antenna substrate on which an integrated circuit is mounted, a power supply having a power supply component for supplying power to the integrated circuit, and a power supply substrate on which the power supply component is mounted; and the integrated circuit is connected to one surface.
  • a skirt is provided on the surface and dissipates heat transferred from the mount.
  • FIG. 1 is a side view of a moving object equipped with an antenna device according to Embodiment 1;
  • FIG. 2 is a plan view of the antenna device according to Embodiment 1 with the radome removed;
  • FIG. 2 is a cross-sectional view of the antenna device according to Embodiment 1 taken perpendicular to the nose direction;
  • FIG. 4 is an enlarged cross-sectional view of a connection portion between a base portion and an integrated circuit, a connection portion between a base portion and a power supply component, and a connection portion between a base portion and a mount in the antenna device according to the first embodiment;
  • FIG. 4 is an enlarged cross-sectional view of a connecting portion between the skirt and the mount of the antenna device according to Embodiment 1;
  • FIG. 8 is an enlarged cross-sectional view of a connecting portion between the skirt and the mount of the modified example of the antenna device according to the first embodiment; 4 is a diagram showing heat flow in the antenna device according to Embodiment 1.
  • FIG. FIG. 8 is a cross-sectional view of the antenna device according to Embodiment 2 taken perpendicular to the nose direction;
  • FIG. 10 is a diagram showing heat flow in the antenna device according to the second embodiment;
  • FIG. 1 is a side view of a moving body 1 equipped with an antenna device 100 according to Embodiment 1.
  • the antenna device 100 is an antenna device for satellite communication mounted on a mobile body 1 such as an aircraft.
  • the antenna device 100 is mounted, for example, on the upper surface of an aircraft as shown in FIG.
  • the antenna device 100 will be described as being mounted on an aircraft as the mobile object 1 .
  • the antenna device 100 may be mounted on other types of mobile bodies 1 .
  • the antenna device 100 is attached to the surface of the mobile object 1, such as the upper surface or the side surface of the mobile object 1, from which radio waves can be transmitted to and received from a satellite. .
  • the antenna device 100 mainly includes an array antenna 2 , a power source 3 , a base portion 4 , a mount 5 , a radome 6 and a skirt 7 .
  • the array antenna 2 transmits and receives radio waves.
  • a power supply 3 supplies power to the array antenna 2 .
  • the base portion 4 is a member that supports the array antenna 2 and the power supply 3 .
  • the mount 5 is a member that fixes the base portion 4 to the moving body 1 .
  • the radome 6 is a member that covers the upper side of the mount 5 and protects the array antenna 2 , the power supply 3 and the base portion 4 .
  • a skirt 7 is provided at a position outside the mount 5 and between the mount 5 and the moving body 1 .
  • the outer shape of the lower portion of the antenna device 100 is determined by the outer shape of the skirt 7 .
  • the outer shape of the skirt 7 is a shape that reduces air resistance.
  • the skirt 7 is seamlessly connected to the underside of the radome 6 and is provided all around the mount 5 .
  • the skirt 7 gives the lower part of the antenna device 100 a shape with low air resistance, and radiates heat generated in the antenna device 100 .
  • FIG. 2 is a plan view of the antenna device 100 with the radome 6 removed.
  • FIG. 3 is a cross-sectional view of the antenna device 100 according to Embodiment 1.
  • FIG. FIG. 3 is a cross-sectional view of the moving body 1 on which the antenna device 100 is mounted, taken along the plane perpendicular to the nose direction, and is taken along the line AA in FIG.
  • the outer shape of the radome 6 and the skirt 7, that is, the outer shape of the antenna device 100 is an elliptical frustum.
  • the outline of the antenna device 100 is an ellipse elongated in the nose direction.
  • the cone surface of the truncated elliptical cone is inclined at an angle such that the width of the top surface is about 70% of the width of the bottom surface.
  • the air resistance becomes smaller than when the outer shape is, for example, an elliptical cylinder or a square cylinder.
  • the mount 5 and the base portion 4 are also elliptical in plan view.
  • the shape of the ellipse of the base part 4 is determined so that the minor axis is as small as possible and is equal to or larger than the width of the array antenna 2, and the major axis is equal to or larger than the required length.
  • the array antenna 2 has a receiving array antenna 21 and a transmitting array antenna 22 .
  • the receiving array antenna 21 and the transmitting array antenna 22 are flat active electronically scanned array antennas.
  • the receiving array antenna 21 and the transmitting array antenna 22 are arranged with a gap in the machine direction, and arranged in the center in the direction perpendicular to the nose direction.
  • the receiving array antenna 21 is arranged closer to the nose than the transmitting array antenna 22. - ⁇ By arranging the receiving array antenna 21 and the transmitting array antenna 22 in the nose direction, the width and area of the antenna device 100 viewed from the nose direction are reduced.
  • the width of the antenna device 100 is the length of the antenna device 100 in the direction perpendicular to the nose direction.
  • the receiving array antenna 21 and the transmitting array antenna 22 are rectangular in plan view.
  • the receiving array antenna 21 and the transmitting array antenna 22 are arranged such that the longer side of the rectangle is parallel to the nose direction.
  • the receiving array antenna 21 and the transmitting array antenna 22 each have an antenna substrate 12 .
  • a plurality of element antennas 10 are mounted on the surface (one surface) farther from the mobile object 1, and the RFIC 11 (Radio Frequency IC) arranged on the surface (other surface) closer to the mobile object 1.
  • Integrated Circuit, radio frequency integrated circuit is implemented.
  • the RFIC 11 is an integrated circuit that processes radio frequency signals and operates the plurality of element antennas 10 .
  • the array antenna 2 can change the directional direction of radio waves to any direction within a determined range by controlling the phase of the element radio waves emitted from each element antenna 10 .
  • the array antenna 2 tracks satellites to be communicated with.
  • the antenna device 100 can communicate with a satellite by electronically scanning to track the satellite without scanning in a mechanically driven manner.
  • the power supply 3 has a power supply component 13 that supplies power to the RFIC 11 and a power supply board 14 on which the power supply component 13 is mounted.
  • a power supply 3 is arranged between the base portion 4 and the mount 5 .
  • the RFIC 11 of the array antenna 2 and the power source component 13 of the power source 3 generate heat when the antenna device 100 transmits and receives radio waves.
  • the RFIC 11 and the power supply component 13 are components that generate a large amount of heat.
  • the RFIC 11 is mounted on the antenna board 12, and the power supply component 13 is mounted on the power supply board 14. Thus, the components are separately mounted on separate boards.
  • the base part 4 is a member to which the array antenna 2 and the power supply 3 are attached.
  • the base portion 4 has a plate-like member, the antenna substrate 12 is arranged on one side of the plate-like member, and the plate-like member supports the antenna substrate 12 .
  • a power substrate 14 is provided on the surface opposite to the one surface of the plate member of the base portion 4 (the other surface). Specifically, the top surface (heat radiation surface) of the RFIC 11 mounted on the antenna substrate 12 is connected to one surface of the base portion 4 which is the surface farther from the moving object 1 .
  • a power source component 13 mounted on a power substrate 14 is connected to the other surface of the base portion 4 .
  • the other surface of the base portion 4 is the surface closer to the moving body 1 .
  • An RFIC 11 and a power supply component 13 that are heat generating components are separately connected to two different surfaces of the base portion 4 .
  • the heat from the RFIC 11 and the heat from the power supply component 13, which are components that generate a large amount of heat, can be transmitted to the base portion 4 through separate paths, and the heat can be efficiently transmitted.
  • the base portion 4 has an elliptical plate-like member and a cylindrical side member.
  • An antenna substrate 12 and a power supply substrate 14 are provided on the plate member.
  • the tubular side member connects the peripheral edge of the plate member and the mount 5 .
  • Each of the antenna board 12 and the power supply board 14 is fixed to the base portion 4 by a fixture (not shown).
  • the upper end of the cylindrical side member is closed with a plate member, and the lower end is open.
  • the base portion 4 has an elliptical cylindrical shape.
  • the lower end of the side member of base portion 4 is connected to mount 5 .
  • Base portion 4 is supported by mount 5 .
  • the base portion 4 is fixed to the mount 5 .
  • the shape of the plate member of the base portion 4 may be any shape.
  • the elliptical plate member fits into the internal space of the radome 6, which has the shape of an elliptical truncated cone.
  • the shape of the plate member of the base portion 4 is desirably elliptical.
  • the shape of the plate member may be any shape such as a polygon or a circle as long as it can support the antenna substrate 12 and the power supply substrate 14 .
  • the side member of the base portion 4 may have any other shape as long as it connects the peripheral edge of the plate member and the mount 5 .
  • the side member may be composed of a plurality of members connecting the periphery of the plate member and the mount 5 .
  • the heat generated by the RFIC 11 and the power supply component 13 is transferred to the base portion 4 .
  • the base portion 4 transfers heat transferred from the RFIC 11 and the power supply component 13 to the mount 5 .
  • the base portion 4 protects the RFIC 11 , the antenna substrate 12 , the power source component 13 , and the power source substrate 14 from a load such as vibration applied from the outside to the antenna device 100 mounted on the moving object 1 . It is desirable that the base portion 4 be made of a material having high thermal conductivity and high rigidity.
  • the base portion 4 is formed of a first member 41 that conducts heat and a second member 42 that supports the antenna substrate 13 and the power supply substrate 14 .
  • the first member 41 is connected to the RFIC 11, the power supply component 13 and the mount 5.
  • the first member 41 is made of a material with high thermal conductivity.
  • a high thermal conductivity means that the thermal conductivity is equal to or higher than a predetermined value. The determined value is, for example, 700 W/mK or more, preferably 1000 W/mK.
  • the first member 41 is made of a material having higher thermal conductivity than the second member 42 .
  • the first member 41 is made of a material containing graphite.
  • the second member 42 is made of a material having higher rigidity than the first member 41 .
  • the antenna board 13 and the power board 14 are fixed to the second member 42 .
  • the second member 42 supports the antenna board 13 and the power supply board 14 so that the load is not applied to the first member 41 .
  • the second member 42 is made of a material containing aluminum.
  • the plate-like member of the base part 4 has a central portion in the thickness direction (thickness central portion), a region on one side connected to the RFIC 11, and a thickness central portion.
  • a connecting portion and a portion connecting the area of the other surface connected to the power supply component 13 and the central portion of the thickness are formed of the first member 41 .
  • the side member of the base portion 4 is formed of the first member 41 at the central portion of the thickness. In the plate-shaped member and the side member of the base portion 4, the thickness central portions formed by the first member 41 are connected to each other.
  • the periphery of the first member 41 is covered with the second member 42 .
  • the first member 41 is exposed on the surface of the plate-like member of the base portion 4 in the area of one surface connected to the RFIC 11 and the area of the other surface connected to the power supply component 13 .
  • the first member 41 at the center of the thickness of the side member is exposed on the side of the side member connected to the mount 5 .
  • Graphite is characterized by its thermal conductivity, which is about eight times higher than that of aluminum.
  • a first member 41 containing graphite with high thermal conductivity connects the RFIC 11 and the mount 5 and connects the power supply component 13 and the mount 5 .
  • the base portion 4 functions as a heat spreader to quickly diffuse the heat generated by the RFIC 11 and the power supply component 13 to the entire first member 41 .
  • the base portion 4 can suppress the occurrence of temperature unevenness in the RFIC 11 , the antenna substrate 12 , the power supply component 13 and the power supply substrate 14 .
  • the first member 41 containing graphite with high thermal conductivity heat can be efficiently conducted even to a place away from the RFIC 11, the antenna substrate 12, the power source component 13, and the power source substrate 14, which are heat sources. Therefore, the temperature rise of the RFIC 11, the antenna substrate 12, the power supply component 13, and the power supply substrate 14 can be suppressed, and the temperatures thereof can be made appropriate. It is possible to suppress deterioration of electrical performance due to high temperatures of the RFIC 11 and the antenna substrate 12 . Shortening of the life of the power supply component 13 and the power supply board 14 can be reduced.
  • Graphite has a specific gravity about 0.8 times that of aluminum. Compared to the case where the base portion 4 is entirely made of aluminum, the base portion 4 is formed by combining the first member 41 made of a material containing graphite and the second member made of a material containing aluminum. In this case, the base portion 4 becomes lighter.
  • the base portion 4 has a structure in which a first member 41 containing graphite is covered with a second member 42 made of a material containing aluminum having higher rigidity than graphite. Compared to the base portion made entirely of graphite, the base portion 4 has a structure that is strong against external loads such as vibration applied from the outside.
  • the base portion 4 has a structure in which the first member 41 containing graphite and the second member 42 containing aluminum are combined, so that the base portion 4 has high thermal conductivity and high rigidity. can be done.
  • FIG. 4 is an enlarged view of a connection portion between the base portion 4 and the RFIC 11, a connection portion between the base portion 4 and the power source component 13, and a connection portion between the base portion 4 and the mount 5 in the antenna device 100 according to the first embodiment. It is a sectional view.
  • the RFIC 11 and the base portion 4 are brought into close contact and the power source component 13 and the base portion 4 are brought into close contact and connected.
  • the close connection means that the connection is made so that air does not enter between them.
  • connection surface between the RFIC 11 and the base portion 4 and the connection surface between the power supply component 13 and the base portion 4 are processed so as to reduce surface unevenness.
  • the base portion 4 and the RFIC 11 are closely connected via a thermal interface material 9 that contacts the base portion 4 and the RFIC 11 without a gap.
  • the thermal interface material 9 is made of a material having a thermal conductivity equal to or higher than a predetermined value.
  • the base portion 4 and the power source component 13 are closely connected via a thermal interface material 9 that contacts the base portion 4 and the power source component 13 without gaps.
  • the thermal interface material 9 can fill small gaps between the RFIC 11 and the base portion 4 and between the power supply component 13 and the base portion 4 .
  • the thermal interface material 9 can reduce thermal resistance on the contact surface between the RFIC 11 and the base portion 4 and the contact surface between the power supply component 13 and the base portion 4 .
  • the thermal interface material 9 connecting between the base portion 4 and the RFIC 11 and the thermal interface material 9 connecting between the base portion 4 and the power supply component 13 may be of the same type or may be of different types. You can use things.
  • a determined value (necessary thermal conductivity value) for the thermal conductivity of the thermal interface material 9 connecting between the base part 4 and the RFIC 11 and the need for the thermal interface material 9 connecting between the base part 4 and the power supply component 13 The thermal conductivity values may be the same value or different values. At least one of the necessary thermal conductivity and the type of the thermal interface material 9 may be changed for each connection point.
  • the mount 5 is arranged on the side of the base portion 4 to which the power supply component 13 is connected (the other side).
  • a mount 5 is fixed to the moving body 1 .
  • Mount 5 supports base 4 , radome 6 and skirt 7 .
  • the mount 5 supports the base portion 4 so that the power supply substrate 14 faces one surface thereof.
  • the mount 5 is fixed to the moving body 1 on the side of the other surface opposite to the one surface.
  • the mount 5 is a member for attaching the antenna device 100 to the mobile object 1 .
  • the mount 5 is made of a highly rigid metal material so as not to transmit the influence of disturbance due to vibration load, wind load, etc. to the array antenna 2, and has a cross-sectional shape that increases the rigidity.
  • the base portion 4 is fixed to the upper surface of the mount 5 with a fixture (not shown).
  • the connection surface between the base portion 4 and the mount 5 is processed so that the unevenness of the surface is reduced.
  • the base portion 4 and the mount 5 are in contact with each other without a gap, and are closely connected via the thermal interface material 9 .
  • the mount 5 is a member having the shape of a hollow truncated elliptical cone with a low height.
  • the upper surface of the truncated elliptical cone is closed with a plate-like member to which the base portion 4 is fixed, and the lower surface is open.
  • the mount 5 is arranged so that the plate-like member has a predetermined distance from the moving body 1 .
  • the mount 5 is fixed to the moving body 1 with a mounting bracket 8 .
  • a base portion 4 is attached to the surface of the mount 5 on the far side from the moving body 1 .
  • the mount 5 has an elliptical plate member provided with the base portion 4 and side members.
  • a side member of the mount 5 is a tubular member having an inclined side surface.
  • the upper ends of the side members of the mount 5 are connected to the peripheral edge of the plate member.
  • the side member of the mount 5 has a cylindrical shape (truncated elliptical cone shape) whose diameter increases from the end connected to the plate-like member toward the end on the moving body 1 side.
  • the shape of the plate member of the mount 5 may be any shape.
  • the shape of the plate-like member of the mount 5 may be any shape such as a polygon or a circle as long as the base portion 4 can be mounted thereon.
  • the elliptical mount 5 can be reduced in area when viewed from above, and the radome 6 and skirt 7 can be shaped to reduce air resistance. It is desirable that the mount 5 has an elliptical shape in plan view.
  • the shape of the plate-like member of the mount 5 is preferably an ellipse in plan view.
  • the side member of the mount 5 may have a shape different from the cylindrical shape of the truncated elliptical cone.
  • the mount 5 may be a member having the shape of a solid truncated elliptical cone.
  • the radome 6 is attached above the mount 5. Radome 6 and mount 5 form an enclosed space above mount 5 .
  • the array antenna 2, the power supply 3, and the base portion 4 are accommodated in this closed space.
  • Radome 6 is provided to protect array antenna 2 , power supply 3 and base portion 4 .
  • the radome 6 is arranged to cover the side of the mount 5 on which the base portion 4 is provided.
  • the radome 6 protects the array antenna 2, the power supply 3, and the base portion 4 from external environments such as hot air, cold air, rain, and wind.
  • the radome 6 is made of a material having a high dielectric constant and dielectric loss tangent so as to transmit radio waves.
  • the radome 6 has a strong strength so as to protect the array antenna 2, the power supply 3, and the base portion 4 from external environments such as wind loads and collisions with foreign objects.
  • the thickness of the radome 6 is necessary and sufficient to withstand the assumed load.
  • the radome 6 has the shape of a hollow truncated elliptical cone with a closed upper end and an open lower end.
  • the radome 6 has a planar member serving as an upper surface and a side member connected to the lower side of the planar member.
  • the side member of the radome 6 is cylindrical with inclined side surfaces.
  • the side members of the radome 6 increase in diameter from the closed upper end to the open lower end.
  • a radome 6 is provided on the outer peripheral surface of the mount 5 .
  • the side members of the radome 6 connect with the side members of the mount 5 at the same angle of inclination as the side members of the mount 5 . At least one of the side member of the mount 5 and the side member of the radome 6 may change the inclination angle depending on the height.
  • the radome 6 is fixed to the mount 5 with fastening parts 15 .
  • a part of the upper side of the mount 5 (the side on which the base portion 4 is provided) is fitted inside the radome 6 .
  • Radome 6 and mount 5 form an enclosed space in which array antenna 2, power supply 3 and base 4 reside.
  • the mount 5 protrudes from the radome 6 at its lower side (the side opposite to the side where the base portion 4 is provided).
  • the inner peripheral surface of the open end of the radome 6 is fixed to a side surface member that forms the outer peripheral surface of the mount 5 .
  • a side member of the mount 5 has a surface to which the inner peripheral surface of the radome 6 is attached and a surface formed outside the radome 6 .
  • the mount 5 may have a structure in which the whole is fitted into the radome 6 .
  • the entire surface of the side member of mount 5 is attached to the inner peripheral surface of radome 6 .
  • a fastening part 15 is attached from the outside of the radome 6 toward the mount 5 .
  • the fastening part 15 is a part for fastening the radome 6 and the mount 5, and is a bolt, a rivet, or the like.
  • Loosening prevention measures are taken to prevent loosening of the fastening part 15 from loosening due to load and vibration during flight of the moving body 1 .
  • FIG. 5 is an enlarged cross-sectional view of the connecting portion between the skirt 7 and the mount 5 of the antenna device 100 according to the first embodiment.
  • Skirt 7 is a member provided between moving body 1 and radome 6 in order to reduce the air resistance of antenna device 100 .
  • a skirt 7 is provided on the outer peripheral surface of the mount 5 between the radome 6 and the moving body 1 .
  • the skirt 7 dissipates heat transmitted from the mount 5.
  • the skirt 7 has a shape that fits the shape of the portion of the mount 5 to which the skirt 7 is attached.
  • the skirt 7 is in the shape of a hollow elliptical frustum.
  • the skirt 7 has a side surface having the same shape as the side member forming the outer peripheral surface of the mount 5 , an end surface connected to the open lower end of the radome 6 , and an end surface connected to the surface of the moving body 1 .
  • the skirt 7 has an inner peripheral surface connected to an outer peripheral surface of the mount 5 .
  • the skirt 7 has an upper end face (one end) connected to the open lower end of the radome 6 .
  • the skirt 7 is connected to the surface of the mobile body 1 so that the lower end face (the other end) follows the curved surface of the mobile body 1 .
  • the skirt 7 is provided so as to cover the surface formed outside the radome 6 among the side members of the mount 5 .
  • the skirt 7 is secured to the mount 5 with fasteners 15 .
  • a fastening part 15 is attached from the outside of the skirt 5 toward the mount 5 .
  • the fastening parts 15 are bolts, rivets, or the like.
  • the side surfaces of the radome 6 and the skirt 7 are shaped to minimize an increase in air resistance caused by mounting the antenna device 100 thereon.
  • the antenna device 100 can reduce an increase in air resistance, and can suppress transmission of vibration due to vibration load, wind load, and the like to the array antenna 2 .
  • the skirt 7 is provided on the surface formed outside the radome 6 on the side member of the mount 5 .
  • the skirt 7 may have another structure as long as it is provided between the radome 6 and the moving body 1 .
  • the mount 5 and the skirt 7 are closely connected via the thermal interface material 9 described above.
  • the mount 5 and the skirt 7 are in close contact with each other without a gap, and are closely connected via a thermal interface material 9 made of a material having a thermal conductivity equal to or higher than a predetermined value.
  • the skirt 7 is attached to the moving body 1 via an elastic material 16 such as rubber.
  • the elastic member 16 is a member for filling a small gap between the skirt 7 and the moving body 1. As shown in FIG.
  • the elastic member 16 allows the skirt 7 and the moving body 1 to be closely attached and connected. Therefore, it is possible to prevent the wind received by the antenna device 100 from entering the inside of the antenna device 100 from between the skirt 7 and the moving body 1 during operation of the moving body, thereby preventing the generation of lift force. It is also possible to prevent water or the like from entering the inside of the antenna device 100 from between the skirt 7 and the moving body 1 .
  • the outer peripheral surface of the skirt 7, the radome 6, and the outer peripheral surface are arranged so that there is no step.
  • a step is not formed on the outer peripheral surface of the antenna device 100, and air resistance can be reduced.
  • the outer peripheral surface of the skirt 7 may be arranged slightly inside the outer peripheral surface of the radome 6 . Also in this structure, since the steps on the outer peripheral surface are small, the air resistance can be reduced.
  • the skirt 7 is made of, for example, metal with high thermal conductivity such as aluminum.
  • the skirt 7 may have radiation fins formed on its outer peripheral surface in order to increase the area of contact with cold air outside the moving body 1 .
  • a structure may be adopted in which a plurality of slits are formed in the outer peripheral surface of the skirt 7 to serve as heat radiation fins.
  • FIG. 7 is a diagram showing heat flow in the antenna device 100.
  • FIG. The arrows in the figure indicate the direction of heat flow.
  • the heat generated by RFIC 11 and power supply component 13 is transmitted to base portion 4 through different paths.
  • the heat transmitted to the base portion 4 is mainly transmitted through the first member 41 of the base portion 4 , diffused throughout the base portion 4 , and transmitted to the mount 5 .
  • Heat transferred from the base portion 4 to the mount 5 is diffused throughout the mount 5 and transferred to the skirt 7 .
  • the heat transferred to the skirt 7 is released outside the radome 6 .
  • the skirt 7 serves as a heat radiating portion for radiating heat generated by the RFIC 11 and the power supply component 13 to the outside of the radome 6 .
  • the RFIC 11 and the power supply component 13 which are components that generate a large amount of heat, are mounted separately on the antenna substrate 12 and the power supply substrate 14, which are different substrates.
  • the antenna substrate 12 and power supply substrate 14 are connected to the base portion 4, which is a member having high thermal conductivity.
  • heat generated by the RFIC 11 and the power supply component 13 can be efficiently transferred to the mount 5 via the base portion 4 .
  • Heat is transmitted from the mount 5 to the skirt 7, and the skirt 7 dissipates the heat to the outside air.
  • the heat generated by the RFIC 11 and the power supply component 13 can be efficiently dissipated to the outside of the radome 6 without providing a cooling device such as a fan inside the radome 6 .
  • the radome 6 is essential when the antenna device 100 is mounted on an aircraft.
  • the RFIC 11 and the power source component 13 are sealed inside the radome 6 and are not directly exposed to the outside air. It is difficult to dissipate heat from the RFIC 11 and the power source component 13 to the moving body 1 side due to restrictions on equipment. Even in such a case, the antenna device 100 can efficiently dissipate the heat generated by the RFIC 11 and the power supply component 13 to the outside through the base portion 4 , the mount 5 and the skirt 7 .
  • the antenna device 100 can obtain higher heat dissipation than the conventional one. Since the antenna device 100 does not have a component only for cooling, the height of the antenna device 100 does not increase.
  • the base portion 4 has a structure in which a first member 41 containing graphite and a second member 42 containing aluminum are combined. By doing so, the base portion 4 can have high thermal conductivity and high rigidity. Since the structure is such that heat is transferred from the base portion 4 to the skirt 7 and the skirt 7 dissipates the heat, the wind blowing against the moving body 1 in operation can be utilized for cooling the antenna device 100 .
  • the moving body 1 is an aircraft, the higher the altitude at which the moving body 1 flies, the lower the temperature of the outside air of the moving body 1 and the more the cooling efficiency is improved.
  • FIG. 8 is a cross-sectional view of the antenna device 200 according to Embodiment 2 taken perpendicular to the nose direction. The position of the cross section is the same as in FIG. 3, which is the AA cross section shown in FIG. Antenna device 200 differs from antenna device 100 according to Embodiment 1 in the structure of mount 5 . Other configurations are substantially the same. Hereinafter, the same reference numerals are given to the same or corresponding configurations as those described in the above-described embodiments, and the description of those configurations will not be repeated.
  • the mount 5 is arranged with a gap from the surface of the mobile object 1 .
  • a heat-generating component 17 is placed in contact with the surface of the mount 5 on the side closer to the moving body 1 .
  • the component 17 may be any one of components constituting the antenna device 200 , component of a device related to the antenna device 200 , and component of a device not related to the antenna device 200 .
  • a plurality of components 17 may be arranged. Heat generated by component 17 is transferred to mount 5 .
  • the surface of the mount 5 on the side closer to the moving body 1 and the part 17 are arranged in contact with each other so as to efficiently conduct heat.
  • the mount 5 and the part 17 are in contact with the mount 5 and the part 17 without gaps, and are connected via a thermal interface material 9 made of a material having a thermal conductivity equal to or higher than a predetermined value. good too.
  • the mount 5 transfers heat transferred from the component 17 to the skirt 7 .
  • the mount 5 is made of a material containing graphite in order to increase thermal conductivity. As shown in FIG. 8, the mount 5 has a structure in which a third member 51 containing graphite and a fourth member 52 containing aluminum are combined, like the base portion 4 .
  • the mount 5 is formed of a third member 51 that conducts heat and a fourth member 52 that supports the base portion 4 , the radome 6 and the skirt 7 .
  • the third member 51 is connected to the first member 41 , part 17 and skirt 7 of the base portion 4 .
  • the third member 51 is made of a material with high thermal conductivity. The thermal conductivity of the third member 51 is higher than that of the fourth member 52 .
  • the third member 51 is made of a material containing graphite.
  • the fourth member 52 supports the base portion 4 , the radome 6 and the skirt 7 and is made of a material having higher rigidity than the third member 51 .
  • Each of the base portion 4 , the radome 6 and the skirt 7 is fixed to the fourth member 52 of the mount 5 so that the load is not applied to the third member 51 .
  • the fourth member 52 is made of a material containing aluminum.
  • the plate-shaped member of the mount 5 has a thickness central portion, a portion connecting the region of one surface connected to the base portion 4 and the thickness central portion, and a part 17 connected to the plate-like member.
  • a third member 51 forms a portion connecting the area of the other surface and the central portion of the thickness.
  • the side member of the mount 5 is formed with a third member 51 at a predetermined thickness portion (thickness outer peripheral portion) of the outer peripheral surface region connected to the skirt 7 .
  • the thickness central portion of the plate member of the mount 5 and the thickness outer peripheral portion of the side member are connected to each other.
  • the periphery of the third member 51 is covered with the fourth member 52. As shown in FIG.
  • the third member 51 is exposed on the surface of the plate member of the mount 5 in the area of one surface connected to the base portion 4 and the area of the other surface connected to the component 17 .
  • the third member 51 is exposed on the surface in the region of the outer peripheral surface connected to the skirt 7 of the side member.
  • FIG. 9 is a diagram showing heat flow in the antenna device 100.
  • FIG. The arrows in the figure indicate the direction of heat flow.
  • the heat generated by RFIC 11 and power supply component 13 is transmitted to base portion 4 through different paths.
  • the heat transmitted to the base portion 4 is mainly transmitted through the first member 41 of the base portion 4 , diffused throughout the base portion 4 , and transmitted to the mount 5 .
  • Heat generated by component 17 is transferred to mount 5 .
  • the heat transmitted to the mount 5 is mainly transmitted through the third member 51 of the mount 5 and diffused throughout the mount 5 and transmitted to the skirt 7 outside the radome 6 .
  • the heat transferred to the skirt 7 is released to the outside air.
  • the skirt 7 serves as a heat radiating portion for radiating heat generated by the RFIC 11 , the power supply component 13 and the component 17 to the outside of the radome 6 .
  • the antenna device 200 has the same configuration as the antenna device 100 with respect to the RFIC 11, the power source component 13, and the base portion 4, and the heat flow is also the same.
  • third member 51 of mount 5 is also connected to part 17 .
  • the mount 5 has a structure having a third member 51 made of a material with high thermal conductivity and a fourth member 52 made of a material with higher rigidity than the third member 51 .
  • the mount 5 transfers heat transferred from the base portion 4 to the skirt 7, and the skirt 7 dissipates the heat to the outside air.
  • a component 17 that generates a large amount of heat is arranged on the surface (the other surface) of the mount 5 on the moving body 1 side. Devices that generate heat rather than components may be placed on the other side of the mount 5 .
  • a heating element which is a component or device that generates heat, may be connected to the other surface of the mount 5 . Heat is transmitted from the heating element to the mount 5, and the heat transmitted to the mount 5 is transmitted to the skirt 7. - ⁇ The skirt 7 also dissipates the heat generated by the heating element to the outside air.
  • the mount 5 has a structure having a third member 51 made of a material with high thermal conductivity and a fourth member 52 made of a material with higher rigidity than the third member 51, even when not connected to a heating element. can be In that case, the third member 51 connects the base portion 4 and the skirt 7 .
  • the plate-like member of the mount 5 is formed of the third member 51 with a central thickness portion and a portion connecting the region connecting to the base portion 4 and the central thickness portion.
  • the side member of the mount 5 is formed of a third member 51 with a central thickness portion and a portion connecting the region connected to the skirt 7 and the central thickness portion. In the plate-like member and the side member of the mount 5, the thickness center portions formed by the third member 51 are connected to each other.
  • the periphery of the third member 51 is covered with the fourth member 52 in the plate member and the side member of the mount 5 .
  • 1 mobile body 2 array antenna, 21 receiving array antenna, 22 transmitting array antenna, 3 power supply, 4 base part, 5 mount, 6 radome, 7 skirt, 8 mounting bracket, 9 thermal interface material, 10 element antenna, 11 RFIC (integrated circuit), 12 antenna substrate, 13 power source component, 14 power source substrate, 15 fastening component, 16 elastic material, 17 component, 100, 200 antenna device.
  • RFIC integrated circuit

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Details Of Aerials (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
PCT/JP2022/048287 2021-12-28 2022-12-27 アンテナ装置 Ceased WO2023127899A1 (ja)

Priority Applications (3)

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US18/691,894 US12218400B2 (en) 2021-12-28 2022-12-27 Antenna device
EP22916121.1A EP4459792A4 (en) 2021-12-28 2022-12-27 ANTENNA DEVICE
JP2023535723A JP7341377B1 (ja) 2021-12-28 2022-12-27 アンテナ装置

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JP2021-213629 2021-12-28
JP2021213629 2021-12-28

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EP4270634A4 (en) * 2020-12-28 2024-11-06 Kyocera Corporation Antenna device

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JP2003298270A (ja) 2002-03-29 2003-10-17 Mitsubishi Electric Corp アンテナ装置
JP2016539606A (ja) 2013-11-11 2016-12-15 ゴーゴー・エルエルシー 低無線信号減衰量のローカルエリアを有するレードーム
WO2020136861A1 (ja) * 2018-12-28 2020-07-02 三菱電機株式会社 アンテナ装置
WO2020261706A1 (ja) * 2019-06-28 2020-12-30 三菱電機株式会社 アンテナ装置
WO2021046527A1 (en) * 2019-09-06 2021-03-11 Carlisle Interconnect Technologies, Inc. Mounting system for mounting an element to an aircraft surface

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WO2021080932A1 (en) * 2019-10-23 2021-04-29 Commscope Technologies Llc Integrated active antennas suitable for massive mimo operation
US12034206B2 (en) * 2020-03-17 2024-07-09 Mitsubishi Electric Corporation Antenna device
US11522279B1 (en) * 2020-06-05 2022-12-06 Xilinx, Inc. Radome with integrated antenna array and antenna assembly having the same

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JP2003298270A (ja) 2002-03-29 2003-10-17 Mitsubishi Electric Corp アンテナ装置
JP2016539606A (ja) 2013-11-11 2016-12-15 ゴーゴー・エルエルシー 低無線信号減衰量のローカルエリアを有するレードーム
WO2020136861A1 (ja) * 2018-12-28 2020-07-02 三菱電機株式会社 アンテナ装置
WO2020261706A1 (ja) * 2019-06-28 2020-12-30 三菱電機株式会社 アンテナ装置
WO2021046527A1 (en) * 2019-09-06 2021-03-11 Carlisle Interconnect Technologies, Inc. Mounting system for mounting an element to an aircraft surface

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Title
See also references of EP4459792A4

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US20240387975A1 (en) 2024-11-21
JP7341377B1 (ja) 2023-09-08
EP4459792A4 (en) 2025-05-07
US12218400B2 (en) 2025-02-04
EP4459792A1 (en) 2024-11-06

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