Helical Satellite Antenna Array Layout for Low-Sidelobe Gain
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Solution Overview
Problem
Existing satellite communication antenna structures face challenges in achieving good quality communication with reduced bulk, efficient gain, and minimized sidelobe levels, particularly in applications where motorization and large size constraints are limiting factors.
Innovation Solution
The proposed antenna structure features a helical shape with a transmission-reception surface of circular shape, utilizing a dielectric insulation device and radome configuration, allowing for compact size and efficient electromagnetic wave transmission and reception within the X and Ku bands without the need for additional polarizers or motorization.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a parabolic antenna structure with diameter of at least 40 cm is used, then gain and sidelobe level performance is improved, but the size and weight of the antenna structure increases
Solution Approach 1:
The antenna structure is segmented into multiple elementary sources arranged in specific geometric patterns (parabola, circle, square) rather than using a single large continuous reflector. This segmentation allows achieving the required radiation pattern performance with smaller individual elements, reducing overall structure weight and size while maintaining communication quality.
2Reliability
If a parabolic antenna structure with diameter of at least 40 cm is used, then gain and sidelobe level performance is improved, but the overall size of the antenna structure increases
Solution Approach 1:
The antenna structure is segmented into multiple elementary sources arranged in specific geometric patterns (parabola, circle, square) rather than using a single large continuous reflector. This segmentation allows achieving the required radiation pattern performance with smaller individual elements, reducing overall structure weight and size while maintaining communication quality.
3Ease of operation
If electronic phase-shift scanning with multiple elementary sources is used, then beam direction control is improved, but the overall size of the antenna structure increases
Solution Approach 1:
The patent implements electronic phase-shift scanning capability that allows dynamic control of beam direction without mechanical movement. Multiple elementary sources with independent phase control enable electronic steering of the radiated beam, providing flexible and rapid direction changes while maintaining a compact antenna structure.
Solution Approach 2:
The antenna structure is segmented into multiple elementary sources arranged in specific geometric patterns (parabola, circle, square) rather than using a single large continuous reflector. This segmentation allows achieving the required radiation pattern performance with smaller individual elements, reducing overall structure weight and size while maintaining communication quality.
4Adaptability or versatility
If circular polarization emission is desired with electronic phase-shift scanning, then polarization capability is improved, but gain is degraded due to additional polarizer
Solution Approach 1:
The patent combines circular polarization capability with electronic phase-shift scanning in a unified antenna structure. By integrating the polarization function into the elementary sources themselves rather than adding a separate polarizer, the system achieves both circular polarization and beam steering capabilities while maintaining high gain performance without the losses associated with additional components.
5Ease of operation
If motorization device is used to point the radiated beam, then beam direction control is improved, but the device complexity and torque requirements increase
Solution Approach 1:
The patent replaces mechanical motorization systems with electronic phase-shift scanning for beam direction control. Instead of using motors to physically rotate or reposition the antenna, the system electronically steers the beam by adjusting the phase of signals at multiple elementary sources, eliminating complex mechanical components and their associated torque requirements.
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 achieves better performance in terms of gain and reduced sidelobe levels, enabling compact and lightweight satellite communication systems with improved radiation efficiency and reduced weight, suitable for various platforms including aerial and underwater applications.
Implementation Method 1
at least one elementary antenna having a helical shape and dimensioned to transmit and/or receive at least one electromagnetic wave
Implementation Method 2
utilizing a dielectric insulation device
Data Source
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AI summary
The invention relates to an arrangement (200) of antenna structures (10) for telecommunications, in particular by satellite, characterised in that each antenna structure (10) includes a transmission-reception surface (14) comprising an axis of symmetry and at least one dipole antenna (12) having a helical shape and sized such as to transmit and/or receive at least one electromagnetic wave having a frequency higher than 4 GHz, preferably 4 GHz to 50 GHz, in particular in a spectral band selected among the X band and the Ku band, and in that at least two axes of symmetry are concurrent.