Aircraft Intercept Lines for Airborne Target Control

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Solution Overview

Problem

Existing methods for intercepting airborne targets, such as unmanned rotorcraft, often leave disabled targets difficult to control due to interference with rotors and additional mass, posing a continued threat due to uncontrolled landing.

Innovation Solution

An aircraft equipped with two types of lines - thinner lines for tangling with rotors and thicker, adhesive-expressing lines for bonding to non-moving parts, allowing for reliable attachment and control of the target.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a net is fired towards the target to intercept it, then the target rotorcraft becomes disabled by interference with rotors, but the disabled target remains difficult to control for safe landing

Engineering Contradiction:
Improvetarget disablementVSAvoidtarget control
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The intercepting system is divided into two distinct line types: thinner lines for rotor tangling and thicker adhesive lines for body attachment. This segmentation allows each line type to perform its specific function optimally, with the adhesive lines providing control capability that the net alone cannot achieve.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention uses composite line structures combining different materials and properties - thin flexible lines for rotor interaction and thick adhesive lines for body attachment. This composite approach integrates the advantages of both line types to achieve both disablement and control functions simultaneously.

Inventive Principle:
Principle #40Composite materials

2Reliability

If thicker adhesive lines are used to attach to non-moving parts, then reliable bonding is achieved, but the device complexity increases

Engineering Contradiction:
Improveattachment reliabilityVSAvoidline system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The frame structure serves multiple functions: it provides attachment points for both thin and thick lines, maintains proper spatial arrangement, and enables the aircraft to perform both rotor tangling and body attachment operations. This multi-functionality reduces the need for separate specialized structures.

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

Solution Approach 2:

Different regions of the frame are equipped with different line types based on local requirements - thinner lines attached to the inner member for rotor interaction and thicker lines attached to the outer member for body attachment. This local differentiation optimizes performance while managing complexity.

Inventive Principle:
Principle #3Local quality

3Adaptability or versatility

If multiple types of lines are provided on the aircraft, then more attachment possibilities are available, but the manufacturing complexity increases

Engineering Contradiction:
Improveattachment versatilityVSAvoidaircraft manufacturing
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

Both thin and thick lines are pre-attached to the frame during manufacturing, with their attachment points and spatial arrangements predetermined. This preliminary configuration simplifies assembly operations during actual intercept missions while maintaining manufacturing efficiency through standardized frame designs.

Inventive Principle:
Principle #10Preliminary action

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

The solution effectively inhibits the target's flight by tangling with rotors and bonding to the aircraft, enabling safe disposal by dragging the target to a controlled location.

Implementation Method 1

a fluid adhesive housed within the flexible tubular member, wherein the flexible tubular member is configured to express the fluid adhesive through the wall

Methodology Applied
Scientific EffectAdhesion: Adhesive

Data Source

PatentUS11897609B2Aircraft and method for intercepting an airborne target
Publication Date: 2024.02.13 BAE SYSTEMS PLC
  • US11897609B2 patent drawing
  • US11897609B2 patent drawing
  • US11897609B2 patent drawing

AI summary

There is disclosed an aircraft for intercepting an airborne target, the aircraft comprising: a frame; a plurality of lines of a first type, each attached to the frame at a first end, and free at the other end; and a plurality of lines of a second, different, type, each attached to the frame at a first end, and free at the other end.