A laser-microfabricated electrohydrodynamic thruster for centimeter-scale aerial robots

Hari Krishna Hari Prasad, Ravi Sankar Vaddi, Yogesh M. Chukewad, Elma Dedic, Igor Novosselov, Sawyer B. Fuller

PLoS ONE · 2020 · 23 citations · 31 references

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Concepts

TL;DR

Insect‑scale robots have traditionally relied on flapping wings, but electrohydrodynamic (EHD) thrust offers a simpler, moving‑part‑free alternative that generates lift by accelerating ions in a corona discharge. The authors present a laser‑micromachining fabrication process for EHD thrusters that enables the use of fiber‑based composites beyond what semiconductor lithography allows. They built a 1.8 × 2.5 cm four‑thruster device with steel emitters and a lightweight carbon‑fiber mesh, and measured its current and thrust, confirming agreement with the Townsend relation. The device achieved a peak thrust of 363 µN—over three times its 37 mg mass—at 5.2 kV and demonstrated liftoff in free flight at 4.6 kV.

Abstract

To date, insect scale robots capable of controlled flight have used flapping-wings for generating lift, but this requires a complex and failure-prone mechanism. A simpler alternative is electrohydrodynamic (EHD) thrust, which requires no moving mechanical parts. In EHD, corona discharge generates a flow of ions in an electric field between two electrodes; the high-velocity ions transfer their kinetic energy to neutral air molecules through collisions, accelerating the gas and creating thrust. We introduce a fabrication process for EHD thruster based on 355 nm laser micromachining, which potentially allows for greater materials selection, such as fiber-based composites, than is possible with semiconductor-based lithographic processing. Our four-thruster device measures 1.8 × 2.5 cm and is composed of steel emitters and a lightweight carbon fiber mesh. We measured the electrical current and thrust of each thruster of our four-thruster design, showing agreement with the Townsend relation. The peak thrust of our device, at 5.2 kV, was measured to be 3.03 times its 37 mg (363.0 μN) mass using a precision balance. In free flight, we demonstrated liftoff at 4.6 kV.

References

31