Directional coupler for the high-frequency range

• US 5,825,260 A
• Filed: 02/18/1997
• Issued: 10/20/1998
• Est. Priority Date: 02/15/1996
• Status: Expired due to Fees

• Current Assignee: Daimler-Benz Aerospace AG (Mercedes-Benz Group AG)
• Original Assignee: Daimler-Benz Aerospace AG (Mercedes-Benz Group AG)
• Inventors: Rieger, Ralf, Ludwig, Michael
• Primary Examiner(s): GENSLER, PAUL L
• Application Number:
  US08/801,418
• Time in Patent Office: 609 Days
• Field of Search: 333/115, 333/116
• US Class Current: 333/116
• CPC Class Codes: H01P 5/184 the guides being strip lines or microstrips

Abstract

A directional coupler that can be produced entirely in integrated technology (MIC or MMIC), particularly for the X-band. The directional coupler can be designed for a high coupling attenuation (>30 dB) and a high directivity (>30 dB) with a large relative bandwidth (approximately 20%). This is achieved with a stepped arrangement comprising a plurality of λ/4 waveguide sections and coupling capacitors disposed between the respective paths of the coupler.

Claims

1. A directional coupler for the high-frequency range, comprising, in combination:

a through path and a coupling path, each extending between respective ports, and with the through and coupling paths each being symmetrically configured as sections of flat conductors in integrated waveguide technology;

at least three coupling points for coupling waves, which are conducted in the flat conductors, between the through and coupling paths are present in each path in the direction of propagation of an incident TEM mode fed to one port of the through path;

each flat conductor section in each path disposed between two adjacent of the coupling points has an electrical length equal to λ

/4, where λ

indicates the wavelength of the wave conducted in the flat conductors; and

,

a respective coupling capacitor is connected between associated respective coupling points of the through and coupling paths.

2. The directional coupler as defined in claim 1, wherein the coupling points are configured as junctions in integrated waveguide technology.

3. The directional coupler as defined in claim 1, wherein the coupling capacitors are configured as a flat conductor line interruption in integrated waveguide technology.

4. The directional coupler as defined in claim 1, wherein the capacity of the respective coupling capacitors is selected as a function of the HF power to be coupled into the coupling path from the through path.

5. The directional coupler as defined in claim 1, wherein the same number of coupling points and the same number of λ

/4 flat conductor sections are present in each path, and that the numbers of coupling points and λ

/4 flat conductor sections, as well as the number of the coupling capacitors between the paths, are selected as a function of a predetermined relative frequency bandwidth of the coupler.

6. The directional coupler as defined in claim 1, wherein the coupling points, λ

/4 flat conductor sections and coupling capacitors are designed in integrated waveguide technology for the radar frequency range.

7. The directional coupler as defined in claim 1, wherein the integrated waveguide technology is microstrip technology.

8. The directional coupler as defined in claim 1, wherein at least the coupling capacitors are designed for a high predetermined coupling attenuation of the coupler.

9. The directional coupler as defined in claim 1, wherein the coupler is designed for use in the X-band (8 GHz to 12 Ghz).