Tow Assembly Attitude Adjustment for Airborne Geophysical Surveying

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Solution Overview

Problem

Existing airborne geophysical surveying systems face challenges in maintaining the level orientation of surveying equipment during varying flight velocities and wind conditions, leading to noise interference and reduced measurement accuracy due to fixed suspension rigging geometry.

Innovation Solution

A dynamic attitude adjustment system using adjustable suspension ropes and winches to maintain a target attitude of the geophysical surveying platform, incorporating pitch and roll sensors and a control system to adjust rope lengths in real-time, ensuring the transmitter loop remains substantially horizontal across different flight conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If fixed suspension rigging geometry is used, then the structure is simple and easy to manufacture, but the attitude of the surveying equipment cannot be maintained during varying flight conditions

Engineering Contradiction:
Improveattitude stabilityVSAvoidsuspension system complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The patent applies the dynamics principle by making the suspension ropes adjustable in length rather than fixed. The system includes winches that can dynamically change the length of each suspension rope to compensate for varying aerodynamic forces during flight, maintaining a substantially horizontal attitude of the transmitter loop across different flight velocities and wind conditions.

Inventive Principle:
Principle #15Dynamics

2Measurement precision

If adjustable suspension ropes with winches are used, then the attitude stability is improved, but the device complexity increases

Engineering Contradiction:
Improvemeasurement accuracyVSAvoidsuspension system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent implements feedback control by using sensors to detect the actual attitude of the transmitter loop and comparing it to the desired horizontal attitude. The control system processes this information and automatically adjusts the winch motor operations to correct any attitude deviations, ensuring accurate and stable measurements throughout the survey.

Inventive Principle:
Principle #23Feedback

3Object-affected harmful factors

If fixed suspension rigging is used, then the system is easier to operate, but noise interference increases and measurement accuracy decreases

Engineering Contradiction:
Improvenoise interferenceVSAvoidsystem operation simplicity
Core Design Contradiction:
Object-affected harmful factorsVSEase of operation

Solution Approach 1:

The patent applies the dynamics principle by making the suspension ropes adjustable in length rather than fixed. The system includes winches that can dynamically change the length of each suspension rope to compensate for varying aerodynamic forces during flight, maintaining a substantially horizontal attitude of the transmitter loop across different flight velocities and wind conditions.

Inventive Principle:
Principle #15Dynamics

4Adaptability or versatility

If attitude adjustment system is implemented, then the adaptability to varying flight conditions is improved, but the device complexity increases

Engineering Contradiction:
Improveadaptability to flight conditionsVSAvoidsuspension system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent applies parameter changes by adjusting the length of individual suspension ropes to adapt to varying flight conditions. The control system modifies the physical parameters (rope lengths) in response to changes in flight velocity, wind conditions, and aerodynamic forces, enabling the system to maintain optimal attitude across a wide range of operating conditions.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS10252801B2Electromagnetic survey system having tow assembly with attitude adjustment
Publication Date: 2019.04.09 GEOTECH LTD
  • US10252801B2 patent drawing
  • US10252801B2 patent drawing
  • US10252801B2 patent drawing

AI summary

A tow assembly for airborne geophysical surveying that comprises a frame incorporating geophysical surveying equipment; and a suspension assembly for suspending the frame from an aircraft. The suspension assembly has a plurality of suspension ropes connected to the frame at spaced apart connection points for suspending the frame from an aircraft. Lengths of the suspension ropes are adjustable with respect to at least four of the connection points to adjust an attitude of the frame during flight.