TY - GEN
T1 - Design, Simulation and Experiment of a High-Power Waterjet Thruster for AquaUAV
AU - Ding, Yi
AU - Zhou, Ming
AU - Chang, Min
AU - Hui, Zhe
AU - Bai, Junqiang
N1 - Publisher Copyright:
© Press of Acta Aeronautica et Astronautica Sinica 2026.
PY - 2026
Y1 - 2026
N2 - Aquatic Unmanned Aerial Vehicles (AquaUAVs) hold extensive application prospects and significant potential value. Inspired by flying squids, water jet propulsion effectively addresses the challenge of underwater launches for AquaUAVs, enabling rapid and efficient takeoff. A novel high-power waterjet thruster using a gas generator as the high-pressure source is proposed. A mathematical model of thrust characteristics was established for this thruster to analyze parameter variations within the thruster during propulsion. CFD simulations of the waterjet process were conducted, and thrust characteristic experiments were performed. Discrepancies among the mathematical model predictions, CFD simulation results, and experimental data were analyzed to validate the correctness of the mathematical model. The thruster achieved a maximum thrust of 1,492 N and a total impulse of 219.1 N·s in testing, leading among water jet thrusters using the same principle. In the future, an improved prototype with multiple gas generators and optimized structure is expected to provide a solution for underwater launches of larger AquaUAVs.
AB - Aquatic Unmanned Aerial Vehicles (AquaUAVs) hold extensive application prospects and significant potential value. Inspired by flying squids, water jet propulsion effectively addresses the challenge of underwater launches for AquaUAVs, enabling rapid and efficient takeoff. A novel high-power waterjet thruster using a gas generator as the high-pressure source is proposed. A mathematical model of thrust characteristics was established for this thruster to analyze parameter variations within the thruster during propulsion. CFD simulations of the waterjet process were conducted, and thrust characteristic experiments were performed. Discrepancies among the mathematical model predictions, CFD simulation results, and experimental data were analyzed to validate the correctness of the mathematical model. The thruster achieved a maximum thrust of 1,492 N and a total impulse of 219.1 N·s in testing, leading among water jet thrusters using the same principle. In the future, an improved prototype with multiple gas generators and optimized structure is expected to provide a solution for underwater launches of larger AquaUAVs.
KW - AquaUAVs
KW - Computational fluid dynamics simulation
KW - Jet propulsion
KW - Waterjet thruster
UR - https://www.scopus.com/pages/publications/105043344926
U2 - 10.1007/978-981-95-3034-2_39
DO - 10.1007/978-981-95-3034-2_39
M3 - 会议稿件
AN - SCOPUS:105043344926
SN - 9789819530335
T3 - Lecture Notes in Mechanical Engineering
SP - 649
EP - 659
BT - Proceedings of the 2nd Aerospace Frontiers Conference, AFC 2025 - Volume 1
PB - Springer Science and Business Media Deutschland GmbH
T2 - 2nd Aerospace Frontiers Conference, AFC 2025
Y2 - 11 April 2025 through 14 April 2025
ER -