Granted Patent B2

US 12,230,857 · App. 17/537,781 · Granted Feb 18, 2025

Inventors: Ricardo Andres Perez Benitez (Auckland, NZ); Michael Cann (Auckland, NZ); Lindsay Lilburn (Auckland, NZ); Cameron Malcolm Arthur (Auckland, NZ)

Assignee: Navico, Inc.

H01P3/123H01P1/2088

Abstract

Claims (30)

1. A system for limiting radio-frequency power leakage, the system comprising: a first component having a first surface and a first waveguide that defines a first cavity; a second component having a second surface and a second waveguide that defines a second cavity; and a first groove that is configured to act as a choke, wherein the first component and the second component are assembled so that an air gap is maintained between the first waveguide and the second waveguide, wherein the first waveguide and the second waveguide are configured to facilitate transmission of radio-frequency power, wherein the first groove is configured to reduce leakage of radio-frequency power through the air gap by (1) redirecting radio-frequency power from the first groove back towards the first waveguide and the second waveguide, or (ii) combining electromagnetic waves of the radio-frequency power destructively in the first groove, and wherein the first groove is defined in the first surface or the second surface.

2. The system of claim 1 , further comprising a second groove, wherein the second groove is defined in one of the first surface or the second surface.

3. The system of claim 1 , further comprising a housing, wherein the first component and the second component are disposed in the housing.

4. The system of claim 1 , wherein the first cavity and the second cavity are aligned along an axis.

5. The system of claim 1 , wherein the first component is configured to move relative to the second component.

6. The system of claim 1 , wherein thickness of the air gap is greater than zero.

7. The system of claim 6 , wherein the air gap has a maximum thickness that is 0.034 of a guide wavelength.

8. The system of claim 1 , wherein the total transmission coefficient is −30 decibels or more negative.

9. The system of claim 8 , wherein the total transmission coefficient is −50 decibels or more negative.

10. The system of claim 9 , wherein the total transmission coefficient is −50 decibels or more negative at an operating frequency of 9.5 gigahertz or lower, wherein the total transmission coefficient is determined by obtaining a partial transmission coefficient using an adapter having a measurement waveguide and a Vector Network Analyzer, wherein radio frequency-power is configured to move from the first waveguide towards the second waveguide, wherein a first port of the Vector Network Analyzer is provided at the first waveguide to provide an indication of the radio frequency-power at the first waveguide, wherein the first port is configured to provide a first input, wherein a second port of the Vector Network Analyzer is provided at the measurement waveguide of the adapter, wherein the second port is configured to provide a second input, wherein the partial transmission coefficient is calculated based on the first input and the second input, and wherein the total transmission coefficient is determined using the partial transmission coefficient.

11. The system of claim 1 , wherein the first groove has a width that is between 0.057 of a guide wavelength and 0.061 of a guide wavelength.

12. The system of claim 1 , wherein the first groove defines an inner diameter that is between 0.606 of a guide wavelength and 0.611 of a guide wavelength.

13. The system of claim 12 , further comprising a second groove, wherein the second groove is defined in one of the first surface or the second surface, wherein the second groove defines an inside diameter that is between 1.019 of a guide wavelength and 1.024 of a guide wavelength.

14. A radar device for limiting radio-frequency power leakage, the radar device comprising:

a first component having a first surface and a first waveguide that defines a first cavity;

a second component having a second surface and a second waveguide that defines a second cavity; and

a first groove that is configured to act as a choke,

wherein the first component and the second component are assembled so that an air gap is maintained between the first waveguide and the second waveguide, wherein the first waveguide and the second waveguide are configured to facilitate transmission of radio-frequency power, wherein the first groove is configured to reduce leakage of radio-frequency power through the air gap, and wherein the first groove is defined in the first surface or the second surface,

wherein the air gap is configured to enhance heat dissipation by isolating the first component from the second component to enable separate heat dissipation from each of the first component and the second component to one or more external walls.

15. The radar device of claim 14 , wherein the first surface and the second surface are configured to form the air gap extending between the first surface and the second surface.

16. The radar device of claim 14 , further comprising a second groove that is defined in the first surface or the second surface.

17. The radar device of claim 14 , further comprising an antenna, wherein the antenna is configured to rotate relative to the second component of the radar device.

18. A waveguide assembly for limiting radio-frequency power leakage and increasing heat dissipation comprising:

a first component having a first surface and a first waveguide that defines a first cavity;

a second component having a second surface and a second waveguide that defines a second cavity; and

a first groove that is configured to act as a choke,

wherein the first component and the second component are assembled so that an air gap is maintained between the first waveguide and the second waveguide, wherein the first waveguide and the second waveguide are configured to facilitate transmission of radio-frequency power, wherein the first groove is configured to reduce leakage of radio-frequency power through the air gap, and wherein the first groove is defined in the first surface or the second surface,

wherein the total transmission coefficient is −30 decibels or more negative.

19. The waveguide assembly of claim 18 , wherein the total transmission coefficient is −50 decibels or more negative at an operating frequency of 9.5 gigahertz or lower, wherein the total transmission coefficient is determined by obtaining a partial transmission coefficient using an adapter having a measurement waveguide and a Vector Network Analyzer, wherein radio frequency-power is configured to move from the first waveguide towards the second waveguide, wherein a first port of the Vector Network Analyzer is provided at the first waveguide to provide an indication of the radio frequency-power at the first waveguide, wherein the first port is configured to provide a first input, wherein a second port of the Vector Network Analyzer is provided at the measurement waveguide of the adapter, wherein the second port is configured to provide a second input, wherein the partial transmission coefficient is calculated based on the first input and the second input, and wherein the total transmission coefficient is determined using the partial transmission coefficient.

20. The waveguide assembly of claim 18 , wherein the first groove is configured to reduce leakage of radio-frequency power through the air gap by (i) redirecting radio-frequency power from the first groove back towards the first waveguide and the second waveguide; or (ii) combining electromagnetic waves of the radio-frequency power destructively in the first groove.

Assignments (2)

Continuity (1)

References Cited (94)