Microstrip to waveguide transition systems and methods

US10707549B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10707549-B2
Application numberUS-201815950130-A
CountryUS
Kind codeB2
Filing dateApr 10, 2018
Priority dateApr 10, 2018
Publication dateJul 7, 2020
Grant dateJul 7, 2020

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A radio frequency (RF) assembly that includes a microstrip to waveguide transition is described herein. In one example, the RF assembly can include a substrate, a microstrip, and a waveguide. The substrate can include an antenna that includes an antenna slot. A portion of the microstrip, such as an end of the microstrip, can be disposed within and/or underneath the antenna slot. The microstrip can be embedded within the substrate and can be electrically coupled to the antenna. At least a portion of the waveguide can be disposed over the antenna slot.

First claim

Opening claim text (preview).

What is claimed is: 1. An apparatus comprising: a substrate comprising an antenna, wherein the antenna comprises an antenna slot; a microstrip embedded within the substrate, comprising a first microstrip end disposed under the antenna slot, and electrically coupled to the antenna; and a waveguide comprising a first waveguide end and a second waveguide end, wherein the first waveguide end is disposed over the antenna. 2. The apparatus of claim 1 , wherein the antenna further comprises an antenna layer disposed on a top layer of the substrate, and wherein the antenna layer comprises the antenna slot. 3. The apparatus of claim 2 , wherein the substrate further comprises a dielectric layer disposed between the antenna layer and the microstrip. 4. The apparatus of claim 2 , wherein the microstrip is electrically coupled to the antenna layer. 5. The apparatus of claim 2 , wherein the substrate further comprises a ground plane layer disposed below the microstrip. 6. The apparatus of claim 5 , wherein the substrate further comprises a dielectric layer disposed between the ground plane layer and the microstrip. 7. The apparatus of claim 1 , wherein a major length of the antenna slot is oriented at an angle to a length direction of the microstrip. 8. The apparatus of claim 1 , wherein the waveguide is a cylindrical waveguide. 9. The apparatus of claim 1 , wherein the waveguide is a substantially rectangular waveguide. 10. The apparatus of claim 9 , wherein a slot major length of the antenna slot is oriented at an angle to a waveguide major length of the waveguide. 11. A steerable array comprising the apparatus of claim 1 , wherein the apparatus further comprises a plurality of waveguides, wherein each of the plurality of waveguides comprise a first waveguide end and a second waveguide end, and wherein each of the first waveguide ends is disposed over a corresponding antenna slot. 12. The steerable array of claim 11 , wherein the plurality of waveguides are disposed within a waveguide panel. 13. The steerable array of claim 11 , wherein the plurality of waveguides are coupled to a phased array. 14. The steerable array of claim 13 , wherein the phased array comprises a dielectric lens. 15. An aircraft comprising the steerable array of claim 11 , wherein the aircraft further comprises: a fuselage; and a wing, wherein the steerable array is coupled to the fuselage and/or the wing. 16. The aircraft of claim 15 , further comprising a navigational device, wherein the steerable array is communicatively coupled to the navigational device. 17. The aircraft of claim 16 , wherein the steerable array is configured to generate directed electromagnetic waves and output radar data based on the generated electromagnetic waves. 18. A method of manufacturing the apparatus of claim 1 , the method comprising: forming a first dielectric layer of the substrate; forming the microstrip above the first dielectric layer; forming a second dielectric layer of the substrate above the microstrip; forming an antenna layer of the substrate above the second dielectric layer; and disposing the waveguide over the antenna slot of the antenna layer. 19. The method of claim 18 , further comprising: forming a ground plane layer, wherein the first dielectric layer is formed above the ground plane layer. 20. The method of claim 18 , wherein the microstrip is patterned or printed on the first dielectric layer, wherein the antenna layer is patterned or printed on the second dielectric layer, and wherein at least a portion of the second dielectric layer is laminated or printed on the first dielectric layer.

Assignees

Inventors

Classifications

  • H01P5/107Primary

    Hollow-waveguide/strip-line transitions · CPC title

  • Earthing means; Earth screens; Counterpoises · CPC title

  • of aircraft or spacecraft · CPC title

  • Phased-array fed focussing structure · CPC title

  • Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US10707549B2 cover?
A radio frequency (RF) assembly that includes a microstrip to waveguide transition is described herein. In one example, the RF assembly can include a substrate, a microstrip, and a waveguide. The substrate can include an antenna that includes an antenna slot. A portion of the microstrip, such as an end of the microstrip, can be disposed within and/or underneath the antenna slot. The microstrip …
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification H01P5/107. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue Jul 07 2020 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).