Helical Antenna with Segmented Pitch for High Gain

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Solution Overview

Problem

Space-based communication systems face challenges in achieving high gain and efficiency with traditional helical antennas, particularly at lower frequencies, due to size constraints and interference issues, such as signal attenuation in tropical environments and backlobe radiation.

Innovation Solution

The configuration of a helical antenna with a proximal segment having linearly progressing pitch angles and a distal segment with a constant pitch angle, coupled in series, along with structural support and a deployable ground plane structure, to optimize radio wave velocity and reduce sidelobes, enhancing gain and bandwidth.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional helical antenna structures are used, then the antenna can be deployed in space, but the gain and efficiency are insufficient particularly at lower frequencies

Engineering Contradiction:
Improveantenna gain and efficiencyVSAvoidantenna structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The helical antenna is divided into multiple discrete helical elements (first helical element, second helical element, third helical element, etc.) arranged in a specific geometric pattern. Each element contributes to the overall radiation pattern, and the segmented structure allows for optimized current distribution and reduced sidelobes while maintaining high gain at lower frequencies.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Multiple helical elements are combined in a coordinated arrangement where their electromagnetic fields interact constructively. The elements are positioned and phased to create a unified radiation pattern with enhanced main lobe gain and suppressed sidelobes, achieving high efficiency without requiring excessive structural complexity.

Inventive Principle:
Principle #5Merging (Combining)

2Reliability

If antenna size is increased to achieve high gain at lower frequencies, then the receive aperture increases, but the antenna becomes too large for small satellites

Engineering Contradiction:
Improvereceive apertureVSAvoidantenna volume
Core Design Contradiction:
ReliabilityVSVolume of moving object

Solution Approach 1:

The antenna transitions from a planar or simple linear structure to a three-dimensional geometric arrangement of multiple helical elements. By utilizing spatial dimensions strategically, the design achieves an effective receive aperture equivalent to a much larger single-element antenna while keeping the physical volume compact enough for small satellite deployment.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The multiple helical elements are arranged in a nested or compact geometric configuration where elements are positioned close to each other in space. This nesting allows the antenna to achieve a large effective aperture through coherent combination of elements while maintaining a small overall volume that fits within small satellite constraints.

Inventive Principle:
Principle #7Nested doll (Nesting)

3Ease of operation

If lower frequency antennas are used, then the beamwidth broadens and aiming requirements are reduced, but the antenna size becomes excessively large

Engineering Contradiction:
Improveantenna beamwidthVSAvoidantenna length
Core Design Contradiction:
Ease of operationVSLength of stationary object

Solution Approach 1:

The antenna uses multiple helical elements arranged to create a broad beamwidth through their combined radiation patterns. The segmentation allows each element to contribute to the overall wide coverage area, achieving the desired ease of operation without requiring any single element to be excessively long.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The design optimizes parameters such as element spacing, helical winding characteristics, and phase relationships to achieve a broad beamwidth at lower frequencies. By carefully controlling these parameters, the antenna maintains wide coverage for reduced aiming requirements while keeping the physical dimensions within acceptable limits for space deployment.

Inventive Principle:
Principle #35Parameter changes

4Object-generated harmful factors

If directional helical antennas are mounted over a ground plane structure, then backlobe radiation is avoided, but the structure becomes more complex and heavier

Engineering Contradiction:
Improvebacklobe radiationVSAvoidground plane structure weight
Core Design Contradiction:
Object-generated harmful factorsVSWeight of stationary object

Solution Approach 1:

The geometric arrangement of the multiple helical elements creates an asymmetric radiation pattern where the main lobe is directed forward and sidelobes are naturally suppressed. This asymmetric configuration achieves backlobe reduction without requiring a heavy ground plane structure, as the element positioning and phasing inherently control the radiation distribution.

Inventive Principle:
Principle #4Asymmetry

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This configuration results in a high-gain helical antenna with reduced sidelobes and increased bandwidth, effectively addressing size and interference challenges, while maintaining efficient use of resources on small satellites.

Implementation Method 1

a radio wave traveling along the conductive helix element reaches a terminal velocity at a point of the coupling

Methodology Applied
Scientific EffectRadio wave propagation: Electromagnetic Induction

Data Source

PatentUS11258181B2Systems and methods for providing a high gain space deployable helix antenna
Publication Date: 2022.02.22 EAGLE TECHNOLOGY LLC
  • US11258181B2 patent drawing
  • US11258181B2 patent drawing
  • US11258181B2 patent drawing

AI summary

Systems and methods for improving an efficiency and a gain of a helical antenna. The methods comprise: configuring a conductive helix element of the helical antenna to comprise a proximal segment having a helical winding that extends along an axis of the conductive helix element and has a plurality of turns with linearly progressing pitch angles; configuring the conductive helix element to comprise a distal segment having a helical winding that extends along the axis of the conductive helix element and has a constant pitch angle; and coupling the distal segment to the proximal segment in a series arrangement so that a radio wave reaches a terminal velocity at a point of the coupling.