IP Library Granted Patent US 10,734,697
Granted Patent B1
US 10,734,697 · App. 16/165,531 · Granted Aug 4, 2020

Coaxial adjustable wave probe

Inventor: Christos Tsironis (Kirkland, CA)
H01P5/183G01R1/06766H01P3/02H03H7/40G01R31/2822
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Quick Facts
Patent No.
US 10,734,697
App. No.
16/165,531
Granted
Aug 4, 2020
Kind
B1
Abstract

Wideband coaxial low loss signal couplers use an electro-magnetic loop placed perpendicularly in a mantle hole of the external wall of the coaxial airline. The signal coupling factor increases with frequency thus favoring detection of harmonic components generated by the nonlinearly operated RF transistors. In order to adapt also to various power levels and associated harmonic receiver sensitivity the coupling factor can be adjusted either by controlling the penetration of the loop inside the airline cavity or by rotating the loop around its vertical axis.

Claims (22)

1. A signal coupler comprising a coaxial airline, input port, output port, coupled port and isolated port and an electromagnetic “U” form loop sensor, said sensor having a bottom section and two branches,

wherein

the branches of the loop sensor extend into forming the center conductor of coaxial cables,

one branch terminating as coupled port and the other branch terminating as isolated port, and wherein

the loop sensor is inserted perpendicularly through a hole in a mantle of the airline.

2. An assembly comprising the signal coupler as in claim 1 and an impedance tuner, said tuner comprising at least

coaxial test and idle ports, and

a slotted airline (slabline) with two sidewalls and a center conductor between the ports,

wherein the signal coupler forms a coaxial-to-slabline adapter connected to the test or idle ports.

3. The signal coupler as in claim 1 ,

wherein

the coupling factor is adjustable.

4. The signal coupler as in claim 1 ,

wherein

the distance between the loop sensor and a center conductor of the coaxial airline is adjustable.

5. The signal coupler of claim 1

wherein

the loop sensor has a surface and a rotation axis,

said rotation axis being perpendicular to the bottom section of the loop and parallel to and

centered between the two branches of the loop,

and wherein

the angle between the surface of the loop sensor and an axis of the airline is adjustable.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 27, 2019
From: FOCUSMW IP. INC.
To: TSIRONIS, CHRISTOS
Reel/Frame 048449/0245 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 19, 2018
From: TSIRONIS, CHRISTOS
To: FOCUSMW IP. INC.
Reel/Frame 047236/0781 →
Cited By (1)
US 12,352,608