Removable Shoulder Panel Antenna Mounting System

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Solution Overview

Problem

The existing methods for installing aircraft antennas and sensors are limited by the need for permanent modifications to the upper fuselage, which restricts the number of possible positions and can interfere with aerodynamics and visibility, and the 'roll-on/roll-off' approach has limited positions for temporary antennas.

Innovation Solution

An aircraft multi-purpose shoulder panel system that allows for easy installation and removal of multiple antenna configurations at the wing shoulder panel, avoiding the need for permanent modifications and maintaining aerodynamic integrity, with a design featuring a shoulder panel insert, circumferential base, antenna compartment, removable mounting plate, and fenestrations for connections.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If permanent modifications are made to the upper fuselage to install antennas, then antenna installation is achieved, but the number of possible positions is limited and aerodynamics are interfered with

Engineering Contradiction:
Improvenumber of antenna positionsVSAvoidaerodynamic interference
Core Design Contradiction:
Adaptability or versatilityVSObject-affected harmful factors

Solution Approach 1:

The antenna system is divided into separate, removable antenna units that can be independently installed and removed from the fuselage surface. This segmentation allows multiple antenna configurations without permanent modifications, enabling versatile positioning while maintaining aerodynamic integrity when antennas are not in use.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The antenna mounting system transitions from static permanent modifications to dynamic removable installations. The fuselage surface maintains its original aerodynamic properties, and antennas can be dynamically positioned or removed based on mission requirements, eliminating aerodynamic interference while providing position flexibility.

Inventive Principle:
Principle #15Dynamics

2Ease of operation

If the roll-on/roll-off approach is used for temporary antennas, then installation flexibility is improved, but the number of positions for temporary antennas is very limited

Engineering Contradiction:
Improveinstallation flexibilityVSAvoidnumber of antenna positions
Core Design Contradiction:
Ease of operationVSAdaptability or versatility

Solution Approach 1:

The fuselage surface is designed with universal mounting interfaces that can accommodate multiple different antenna types and configurations at various positions. This multi-functional capability allows the same mounting system to support diverse antenna installations across numerous locations, greatly expanding position versatility while maintaining ease of installation.

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

3Ease of manufacture

If antennas are installed on the centerline of the aircraft, then installation is simplified, but turbulence from one antenna impacts the next one aft of it

Engineering Contradiction:
Improveinstallation simplicityVSAvoidantenna turbulence interference
Core Design Contradiction:
Ease of manufactureVSObject-generated harmful factors

Solution Approach 1:

The antenna mounting system utilizes asymmetric positioning options off the aircraft centerline, allowing antennas to be distributed in patterns that minimize turbulent interference. By moving antennas away from the crowded centerline to strategically positioned locations on either side, the system maintains installation simplicity while eliminating turbulence interference between adjacent antennas.

Inventive Principle:
Principle #4Asymmetry

4Strength

If access panel is redesigned for satellite communications system, then structural robustness is utilized, but aerodynamically smooth access panel is changed

Engineering Contradiction:
Improvestructural robustnessVSAvoidaerodynamic smoothness
Core Design Contradiction:
StrengthVSShape

Solution Approach 1:

The antenna system is extracted from the fuselage surface as a separate, removable component rather than being integrated into the aerodynamic skin. This allows the access panel to maintain its aerodynamically smooth shape while utilizing the robust underlying structure for mounting purposes. The structural robustness is harnessed for antenna support without compromising aerodynamic smoothness.

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS11364988B2Multi-purpose shoulder panel system
Publication Date: 2022.06.21 R4 INTEGRATION INC
  • US11364988B2 patent drawing
  • US11364988B2 patent drawing
  • US11364988B2 patent drawing

AI summary

An aircraft multi-purpose shoulder panel system having a shoulder panel insert is disclosed. The system features a circumferential base connected to the shoulder panel insert, an antenna compartment positioned on top of the circumferential base, and a removable antenna mounting plate positioned above, and connected to, the antenna compartment. The system also features an overall structure that provides unprecedented ruggedness, and enables aircraft antennae/sensor versatility, adaptability and reversibility.