Angled Spring Probe Mechanism for Stable UAV Contact

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Unmanned aerial vehicles face instability and control challenges when probes contact targets due to reaction forces, with compression springs increasing length and mass, and requiring space, while setting spring constants for gradual force changes complicates contact management.

Innovation Solution

A floating moving object with a base member and shaft connected by a spring, where the spring's central axis is angled to the shaft's, allowing for controlled contact and separation forces through nonlinear reaction force adjustment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If a compression spring is used to alleviate impact and maintain contact, then the stability of contact is improved, but the overall length and mass of the probe increase

Engineering Contradiction:
Improvecontact stabilityVSAvoidprobe length
Core Design Contradiction:
Stability of the object's compositionVSLength of moving object

Solution Approach 1:

The spring is arranged at an angle (specifically 45 degrees) to the shaft rather than parallel to it. This angular arrangement allows the spring to provide the necessary reaction force while occupying less axial space, thereby reducing the overall probe length while maintaining contact stability.

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

Solution Approach 2:

The invention changes the geometric parameter of the spring arrangement from parallel to angular (45 degrees). This parameter change allows the spring to generate the required reaction force with a shorter axial projection, reducing the probe length while maintaining the stabilizing effect during contact.

Inventive Principle:
Principle #35Parameter changes

2Ease of operation

If the spring constant is set low for gradual force change, then control stability is improved, but the ability to push back the airframe when too close is reduced

Engineering Contradiction:
Improvecontrol stabilityVSAvoidpush back force
Core Design Contradiction:
Ease of operationVSForce

Solution Approach 1:

The system transitions from a static spring constant to a dynamic reaction force system. As the shaft moves forward and the spring compresses, the reaction force increases progressively. The angular arrangement ensures that even with a moderate spring constant, the force component along the shaft axis increases sufficiently to push back the airframe when needed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

By arranging the spring at an angle, the system utilizes the geometric relationship between spring compression and axial force. The angular configuration creates a mechanical advantage where moderate spring compression generates sufficient axial reaction force to push back the airframe while maintaining gradual force increase for control stability.

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

3Device complexity

If the probe is fixed to the drone body, then the structure is simplified, but the airframe becomes unstable due to reaction forces

Engineering Contradiction:
Improvestructure complexityVSAvoidairframe stability
Core Design Contradiction:
Device complexityVSStability of the object's composition

Solution Approach 1:

The shaft is made movable relative to the base member through the spring mechanism, allowing the probe to dynamically adjust its position during contact. This dynamic arrangement isolates the reaction forces to the movable shaft while keeping the base member and airframe stable, solving the stability issue without requiring complex structural modifications.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The probe is segmented into a movable shaft portion and a fixed base member portion. The shaft can move independently along the central axis to absorb contact forces, while the base member remains fixed to the base. This segmentation isolates the reaction forces to the shaft, preventing airframe instability while maintaining structural simplicity.

Inventive Principle:
Principle #1Segmentation

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

Enables stable contact with targets using appropriate pressure, maintaining control and preventing unwanted collisions by adjusting reaction forces nonlinearly, reducing mass and space requirements.

Implementation Method 1

a base member (11) to which one end of a spring (13) is connected; and a shaft (12) to which the other end of the spring is connected, the shaft being configured to move relative to the base member in a direction of a central axis of the shaft when the shaft comes into contact with a target object

Methodology Applied
Scientific EffectSpring: Spring

Data Source

PatentUS20250290596A1Floating moving object and probe mechanism
Publication Date: 2025.09.18 THK CO LTD
  • US20250290596A1 patent drawing
  • US20250290596A1 patent drawing
  • US20250290596A1 patent drawing

AI summary

Provided are a base member 11 to which one end of a spring 13 is connected, and a shaft 12 to which the other end of the spring 13 is connected, and which is configured to move relative to the base member in a direction of a central axis of the shaft when the shaft comes into contact with a target object, wherein the spring 13 is arranged such that a center axis of the spring 13 is at an angle to the center axis of the shaft.