Modular Satellite Panel Docking Structure

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Solution Overview

Problem

Conventional satellite technology requires custom-designed, large, and heavy electronics boxes that are difficult to integrate and connect, making series production unsuitable and time-consuming, with complex cable harnesses and inaccessible electrical interfaces.

Innovation Solution

A modular device support panel with standardized docking structures and connectors allows for quick mechanical and electrical attachment of prefabricated electronics boxes, forming a 'harness bus' that can be integrated in half a day, using ARINC connectors for standardized interfaces and efficient heat dissipation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If custom-designed electronics boxes are used for each satellite project, then the electronics can be tailored to specific project requirements, but the integration time increases significantly and series production becomes unsuitable

Engineering Contradiction:
Improvecustomization of electronicsVSAvoidintegration speed
Core Design Contradiction:
Adaptability or versatilityVSProductivity

Solution Approach 1:

The satellite electronics system is segmented into standardized, modular electronics boxes that can be independently designed, tested, and manufactured. Each box contains complete functional units with standardized interfaces, allowing parallel development and rapid assembly for different satellite projects without requiring complete custom design of entire systems.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Standardized interfaces and mounting structures are designed to be universally compatible across different satellite projects. The same electronics box design can be adapted to multiple applications through configuration rather than redesign, enabling series production while maintaining project-specific functionality through modular assembly.

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

2Reliability

If conventional cable harnesses with multiple connector types are used, then electrical connections can be established, but the manual connection process becomes extremely time-consuming

Engineering Contradiction:
Improveelectrical connectionVSAvoidconnection time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

Multiple separate electrical connections are merged into a single integrated connector interface. The standardized electrical interface combines power, data, and control signals into one unified connection point, allowing all electrical connections to be established simultaneously through a single plugging action rather than manual connection of numerous individual connectors.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

Electrical connections are pre-configured and tested within the standardized electronics boxes before integration into the satellite. The connector interfaces are designed and validated in advance, so that during assembly, connections are made automatically without requiring manual routing or configuration of individual wires and connectors.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If electrical interfaces with multiple connectors are used, then comprehensive electrical connectivity is achieved, but the interfaces become difficult to access and connect

Engineering Contradiction:
Improveelectrical interfaceVSAvoidaccessibility of connectors
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The complex internal wiring and multiple connectors are extracted and consolidated into a single accessible interface on the electronics box exterior. The standardized connector is positioned and designed for easy access during assembly operations, eliminating the need to access difficult-to-reach areas within the satellite structure for electrical connections.

Inventive Principle:
Principle #2Taking out (Extraction)

4Quantity of substance

If large and heavy electronics boxes are used, then all necessary electronic assemblies can be accommodated, but crane assistance is required for integration

Engineering Contradiction:
Improveelectronic assembliesVSAvoidintegration process
Core Design Contradiction:
Quantity of substanceVSEase of operation

Solution Approach 1:

The electronics system is divided into modular boxes of manageable size and weight, each containing specific functional assemblies. This segmentation allows standard handling equipment to be used instead of heavy cranes, while still accommodating all necessary electronic components through modular configuration of multiple standardized boxes.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP3095713B1Device holder panel of a satellite
Publication Date: 2017.08.02 AIRBUS DEFENCE & SPACE GMBH
  • EP3095713B1 patent drawingFigure 1
  • EP3095713B1 patent drawingFigure 2
  • EP3095713B1 patent drawingFigure 3

AI summary

In a satellite instrument panel with a plurality of electronic boxes (3) accommodating electrical and/or electronic assemblies, wherein the electronic boxes are electrically connected or connectable to one another, it is provided that the instrument panel (1; 12, 13, 14; 16, 17, 18) is provided with at least one docking structure (2; 2A, 2A', 2A"; 2B, 2b', 2B"); that the at least one docking structure (2; 2A, 2A', 2A"; 2B, 2b', 2B") and/or a base plate (10) of the instrument panel (1; 12, 13, 14; 16, 17, 18) has first mechanical connecting means (20, 21) for holding electronic boxes (3); that the at least one docking structure (2; 2A, 2A', 2A";2B, 2b', 2B") first electrical connecting means (22, 23, 24) for electrical connection with the electronic boxes (3) and that the electronic boxes (3) are provided with mechanical counter-connecting means (30, 31) and electrical counter-connecting means (32, 33, 34) in order to mechanically hold and electrically contact a respective electronic box (3) on the docking structure (2; 2A, 2A', 2A"; 2B, 2b', 2B") and/or the device carrier panel (1; 12, 13, 14; 16, 17, 18).