Deployable Phased Array Antenna Sequential Panel Hinge

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Solution Overview

Problem

Conventional phased array antennas onboard telecommunications satellites are limited by their fixed, compact designs, which restrict their ability to generate smaller spot beams and increase system capacity, and they require higher power and larger, more complex structures.

Innovation Solution

A deployable planar phased array antenna system with a polygonal cross-sectional base member and hinged antenna panels that unfold to form a large aperture, allowing for sequential deployment and providing a continuous, flat surface for optimal electromagnetic energy directionality.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If fixed compact phased array antennas are used onboard satellites, then the satellite structure is simplified and deployment is easier, but the aperture size is limited and system capacity cannot be increased

Engineering Contradiction:
Improveantenna aperture areaVSAvoidantenna deployment mechanism
Core Design Contradiction:
Area of stationary objectVSDevice complexity

Solution Approach 1:

The antenna is divided into multiple deployable panels that can be stacked during launch and sequentially deployed to form a large aperture surface. Each panel is a separate module that can be independently positioned and electrically connected, allowing the overall aperture area to be expanded while keeping individual panel complexity manageable.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The antenna transitions from a static compact configuration during launch to a dynamic deployed configuration in orbit. The panels are designed to be movable relative to each other through mechanical deployment mechanisms, allowing the antenna to achieve its full large aperture dimension after satellite deployment.

Inventive Principle:
Principle #15Dynamics

2Productivity

If large aperture antennas are deployed, then smaller spot beams and higher system capacity are achieved, but the antenna structure becomes more complex and deployment mechanisms are required

Engineering Contradiction:
Improvesystem capacityVSAvoidantenna structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The large aperture antenna is segmented into multiple panels that can be manufactured and assembled more easily than a single large structure. This segmentation allows the large aperture to be achieved while managing structural complexity through modular design.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The antenna achieves large aperture area by extending in multiple dimensions through panel deployment. The panels are arranged to form a two-dimensional array surface, maximizing the effective aperture area for generating multiple small spot beams and increasing system capacity.

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

3Power

If fixed separate receive and transmit arrays are used, then the antenna structure is simplified, but the aperture is small and requires higher power and larger structures

Engineering Contradiction:
Improvetransmitter powerVSAvoidantenna aperture area
Core Design Contradiction:
PowerVSArea of stationary object

Solution Approach 1:

The patent combines transmit and receive arrays into a single integrated phased array structure. This merging allows the full aperture area to be utilized for both transmission and reception, increasing the effective aperture area without requiring separate large structures for each function.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The phased array technology enables electronic beam forming and steering, changing the directional parameters of the antenna without physical movement. This allows a single large aperture to serve multiple functions that would otherwise require separate smaller arrays, reducing the total power and structural requirements.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS7714797B2Phased array antenna
Publication Date: 2010.05.11 ASTRIUM LTD
  • US7714797B2 patent drawing
  • US7714797B2 patent drawing
  • US7714797B2 patent drawing

AI summary

A phased array antenna for a telecommunications satellite, that is deployable from a retracted condition to a deployed condition when the satellite is on-station, comprising a base member of hexagonal form, and a plurality of deployable antenna panels stacked one on top of the other on the base member in the retracted condition, each antenna panel being connected to a respective side edge region of the base by means of a respective back flap hinge, and the hinges having pivot points that are offset relative to one another, such that the antenna panels can be hinged sequentially one after the other from the stick to a position in which each panel is adjacent a respective base side edge region to provide an extended flat two-dimensional area when deployed.