Technical Papers
May 8, 2020

Development of a Robust Mating System for Use in the Autonomous Assembly of Planetary Drill Strings

Publication: Journal of Aerospace Engineering
Volume 33, Issue 4

Abstract

Volume-constrained robotic missions seeking to obtain samples from beneath a planetary subsurface may wish to use a rigid drill string consisting of multiple, individual drill bit sections connected together, as opposed to a single, lengthy drill bit. To ensure that drill strings can be assembled and disassembled reliably, it is essential that a robust connection system be used. The authors propose a geometry that seeks to address the requirements of such a mating interface. The proposed solution is based on the bayonet interface, using L- and T-shaped so-called female grooves and male studs connected and disconnected together through a series of clockwise and counterclockwise rotations and single-point clamping events. This routine allows the transfer of both percussion through the drill string and torque in both directions of rotation, while permitting the accurate disconnection of individual drills bits at the required location. Sustained laboratory and field drilling operations suggest that bayonet-style connections offer a reliable solution to the problem of autonomous assembly and disassembly of drill strings in a planetary exploration setting. This paper discusses the development of such a connection system, based on the bayonet connection, which has been implemented in the overall architecture of the Ultrasonic Planetary Core Drill (UPCD). The design trade-off study, which sought to evaluate the use of the bayonet system in comparison with the more conventional screw thread interface, will be discussed, alongside experimental results from percussion transmission testing and drill string assembly testing.

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Data Availability Statement

All data, models, and code generated or used during the study appear in the published article.

Acknowledgments

The Ultrasonic Planetary Core Drill consortium would like to acknowledge both the financial support provided under the European Commission Framework 7 scheme and the invaluable feedback provided by reviewers.

References

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Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 33Issue 4July 2020

History

Received: Jun 7, 2019
Accepted: Dec 12, 2019
Published online: May 8, 2020
Published in print: Jul 1, 2020
Discussion open until: Oct 8, 2020

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Authors

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Research Associate, School of Engineering, Univ. of Glasgow, Glasgow G128QQ, Scotland, UK (corresponding author). Email: [email protected]
Lecturer, School of Engineering, Univ. of Glasgow, Glasgow G128QQ, Scotland, UK. ORCID: https://orcid.org/0000-0001-9762-5274
X. Li
Research Associate, School of Engineering, Univ. of Glasgow, Glasgow G128QQ, Scotland, UK.
D. Firstbrook
Research Assistant, School of Engineering, Univ. of Glasgow, Glasgow G128QQ, Scotland, UK.
P. Harkness
Reader, School of Engineering, Univ. of Glasgow, Glasgow G128QQ, Scotland, UK.

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