Integrated Single-Piece Antenna Feed for Satellite Systems

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Solution Overview

Problem

Conventional antenna feeds for ring focus dish antennas suffer from performance degradation due to mechanical supports, increased complexity and cost from separate component assembly, and material limitations for space applications, particularly in SATCOM systems.

Innovation Solution

An integrated single-piece antenna feed with a circular waveguide input, coaxial feed horn, and turnstile polarizer, fabricated using 3D metal printing, which eliminates the need for separate components and supports, providing a unified structure for both transmitting and receiving modes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If mechanical support structures (struts, dielectric) are used to support the subreflector, then structural stability is achieved, but aperture blockage increases and antenna performance degrades

Engineering Contradiction:
Improvestructural stabilityVSAvoidaperture blockage
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The patent removes mechanical support structures (struts, dielectric supports) from the antenna aperture region. The subreflector is supported without requiring physical supports within the aperture, eliminating the blockage caused by these structures while maintaining structural stability through alternative support mechanisms outside the aperture.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent replaces mechanical support structures with a different configuration where the feed horn assembly itself provides the necessary support. The integrated single-piece feed structure eliminates the need for separate mechanical supports, substituting the traditional mechanical support system with an integrated structural design.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Ease of manufacture

If separate components are used for antenna feed assembly (input section, polarizer, feed horn, subreflector), then manufacturing flexibility is improved, but assembly complexity and manufacturing cost increase

Engineering Contradiction:
Improvemanufacturing flexibilityVSAvoidassembly complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The patent combines multiple separate components (input section, polarizer, feed horn, subreflector) into a single integrated feed structure. This merging eliminates the need for complex assembly operations, reduces the number of parts, and simplifies manufacturing while maintaining the functional capabilities of each individual component.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The integrated single-piece structure performs multiple functions simultaneously - it serves as the input section, polarizer, feed horn, and subreflector support all in one component. This multi-functionality reduces assembly complexity while maintaining manufacturing flexibility through the ability to design different functional regions within the unified structure.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Manufacturing precision

If conventional separate-component antenna feeds are used, then component optimization is improved, but fabrication time and test time increase

Engineering Contradiction:
Improvecomponent optimizationVSAvoidfabrication time
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The patent integrates multiple components into a single piece that can be manufactured in one fabrication process. This eliminates the sequential fabrication of separate components and their subsequent assembly, significantly reducing total fabrication time while maintaining the optimized performance of each functional region through integrated design.

Inventive Principle:
Principle #5Merging (Combining)

4Stability of the object's composition

If dielectric or strut supports are used in space applications, then structural support is achieved, but material limitations and performance degradation occur

Engineering Contradiction:
Improvestructural supportVSAvoidspace application suitability
Core Design Contradiction:
Stability of the object's compositionVSReliability

Solution Approach 1:

The patent removes dielectric and strut supports from the antenna structure, eliminating the material limitations associated with these components in space environments. The integrated single-piece structure, likely made from space-grade metal or composite material, provides structural support without relying on dielectric materials that may not be suitable for space applications.

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS10468773B2Integrated single-piece antenna feed and components
Publication Date: 2019.11.05 OPTISYS INC
  • US10468773B2 patent drawing
  • US10468773B2 patent drawing
  • US10468773B2 patent drawing

AI summary

Embodiments of the invention include an integrated single-piece antenna feed and a turnstile circular polarizer suitable for use in a satellite communications system. One embodiment of the integrated single-piece antenna includes a circular waveguide input, a turnstile, a coaxial feed horn, subreflector and subreflector support. Alternative embodiments utilize symmetrically oriented struts with or without a coaxial subreflector support to physically support a subreflector.