Lightning protection device for an antenna receiver, and aircraft comprising same
A lightning protection device for an antenna receiver includes a shield for a coaxial cable connected to the antenna, and a high-pass filter mounted in series relative to the shield and capable of limiting the low-frequency power flowing in the coaxial cable, including a capacitor and an inductor lower than 1 ohm at the lowest frequency used by the receiver, the capacitor including at least one layer of a conductive material embedded in a printed circuit. The capacitor may be made of a printed circuit including at least two floor plans, each of which is connected to the ground of a connector of the coaxial cable. The printed circuit may include at least one layer of a highly pervious material sandwiched between two layers of a conductive material.
1. A lightning protection device for an antenna connecting to an antenna receiver, comprising:
a printed circuit board with a first side and an opposite, second side, the printed circuit board being comprised of a first ground plane spaced apart from a second ground plane and at least one layer of a conductive material, the printed circuit board being further comprised of a first via extending from a surface of the first side to the first ground plane and a second via extending from a surface of the second side to the second ground plane, the first ground plane being a first plate and the second ground plane being a second plate;
an input coaxial cable connectable to the antenna, the input coaxial cable for transporting signals from the antenna, the input coaxial cable having a first conducting external shield and a first core, the first core connectable to the antenna;
a first connector that connects the input coaxial cable to the first side of the printed circuit board, wherein a ground of the first connector is electrically connected to the first ground plane by the first via;
an output coaxial cable connectable to the antenna receiver, the output coaxial cable for transporting signals to the antenna receiver, the output coaxial cable having a second conducting external shield and a second core, the second core connectable to the antenna receiver;
a second connector that connects the output coaxial cable to the second side of the printed circuit board, wherein a ground of the second connector is electrically connected to the second ground plane by the second via; and
wherein the first and second ground plates and the at least one layer of a conductive material within the printed circuit board together form a capacitor of at least one nF and an inductor lower than one Ohm at a lowest frequency used by said receiver,
wherein the printed circuit board further defines a high-pass filter mounted in series relative to the first and second conducting external shields, the high-pass filter adapted to limit low-frequency power flowing in said output coaxial cable, the high-pass filter being comprised of the capacitor.
2. The device according to claim 1 , wherein,
the at least one layer of a conductive material includes two layers of conducting material, and
the printed circuit board contains at least one layer of high permittivity material sandwiched between the two layers of conducting material.
3. The device according to claim 1 , wherein,
the at least one layer of a conductive material includes two layers of conducting material, and
the printed circuit board contains plural layers of high permittivity material sandwiched between the two layers of conducting material, mounted in series.
4. The device according to claim 1 , wherein said capacitor is incorporated into the first and second connectors.
5. The device according to claim 1 , wherein said capacitor is incorporated into the said input and output coaxial cables.
6. The device according to claim 1 , wherein a dielectric constant of the material separating the first and second plates of the capacitor is greater than four.
7. The device according to claim 1 , wherein a thickness of the printed circuit board between the first and second ground plates is greater than four microns.
8. The device according to claim 1 , wherein an area of each of the first and second plates of the capacitor is greater than one square centimeter.
9. An aircraft comprising:
an antenna;
an antenna receiver; and
lightning protection device that comprises
a printed circuit board with a first side and an opposite, second side, the printed circuit board being comprised of a first ground plane spaced apart from a second ground plane and at least one layer of a conductive material, the printed circuit board being further comprised of a first via extending from a surface of the first side to the first ground plane and a second via extending from a surface of the second side to the second ground plane, the first ground plane being a first plate and the second ground plane being a second plate;
an input coaxial cable connectable to the antenna, the input coaxial cable for transporting signals from the antenna, the input coaxial cable having a first conducting external shield and a first core, the first core connectable to the antenna;
a first connector that connects the input coaxial cable to the first side of the printed circuit board, wherein a ground of the first connector is electrically connected to the first ground plane by the first via;
an output coaxial cable connectable to the antenna receiver, the output coaxial cable for transporting signals to the antenna receiver, the output coaxial cable having a second conducting external shield and a second core, the second core connectable to the antenna receiver;
a second connector that connects the output coaxial cable to the second side of the printed circuit board, wherein a ground of the second connector is electrically connected to the second ground plane by the second via; and
wherein the first and second ground plates and the at least one layer of a conductive material within the printed circuit board together form a capacitor of at least one nF and an inductor lower than one Ohm at a lowest frequency used by said receiver,
wherein the printed circuit board further defines a high-pass filter mounted in series relative to the first and second conducting external shields, the high-pass filter adapted to limit low-frequency power flowing in said output coaxial cable, the high-pass filter being comprised of the capacitor.
10. The device of claim 1 , wherein each of the first and second vias are metalized orifices.
11. The aircraft of claim 9 , wherein each of the first and second vias are metalized orifices.
12. The device according to claim 1 , wherein a thickness of the printed circuit board between the first and second ground plates is between eight and sixteen microns.
13. The aircraft according to claim 9 , wherein a thickness of the printed circuit board between the first and second ground plates is greater than four microns.
14. The aircraft according to claim 13 , wherein a thickness of the printed circuit board between the first and second ground plates is between eight and sixteen microns.
15. The aircraft according to claim 14 , wherein an area of each of the first and second plates of the capacitor is greater than one square centimeter.
16. The aircraft according to claim 15 , wherein a dielectric constant of the material separating the first and second plates of the capacitor is greater than four.
17. The device according to claim 1 , wherein,
a dielectric constant of the material separating the first and second plates of the capacitor is greater than four,
a thickness of the printed circuit board between the first and second ground plates is between eight and sixteen microns, and
an area of each of the first and second plates of the capacitor is greater than one square centimeter.
18. A lightning protection device for an aircraft antenna connecting to an antenna receiver of an aircraft, the lightning protection device comprising:
a printed circuit board with a first side and an opposite, second side, the printed circuit board being comprised of a first ground plane spaced apart from a second ground plane and at least one layer of a conductive material, the first ground plane being a first plate and the second ground plane being a second plate;
an input coaxial cable connectable to the antenna, the input coaxial cable for transporting signals from the aircraft antenna, the input coaxial cable having a first conducting external shield and a first core, the first core connectable to the aircraft antenna;
a first connector that connects the input coaxial cable to the first side of the printed circuit board, wherein a ground of the first connector is electrically connected to the first ground plane;
an output coaxial cable connectable to the aircraft antenna receiver, the output coaxial cable for transporting signals to the antenna receiver, the output coaxial cable having a second conducting external shield and a second core, the second core connectable to the antenna receiver;
a second connector that connects the output coaxial cable to the second side of the printed circuit board, wherein a ground of the second connector is electrically connected to the second ground plane; and
wherein the first and second ground plates and the at least one layer of a conductive material within the printed circuit board together form a capacitor of at least one nF and an inductor lower than one Ohm at a lowest frequency used by said receiver,
wherein the printed circuit board further defines a high-pass filter mounted in series relative to the first and second conducting external shields, the high-pass filter adapted to limit low-frequency power flowing in said output coaxial cable, the high-pass filter being comprised of the capacitor.
19. The device according to claim 18 , wherein,
a dielectric constant of the material separating the first and second plates of the capacitor is greater than four,
a thickness of the printed circuit board between the first and second ground plates is between eight and sixteen microns, and
an area of each of the first and second plates of the capacitor is greater than one square centimeter.
20. The device according to claim 19 , wherein,
the at least one layer of a conductive material includes two layers of conducting material, and
the printed circuit board contains at least one layer of high permittivity material sandwiched between the two layers of conducting material.