Double inlets exhaust system for unmanned aerial vehicle
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United States of America Patent
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Nov 1, 2022
Grant Date -
Nov 26, 2020
app pub date -
May 8, 2020
filing date -
May 24, 2019
priority date (Note) -
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Abstract
The dual inlet exhaust design for the flying device incorporates easy-to-assemble designs with low number of components, suitable for limited space and small volume requirements, good performance. The exhaust is designed as a three-chamber cylinder with two coaxial inlet pipes running through the two chambers on both sides, extending into the middle compartment. The width of the two inlet tubes in the middle compartment is different. The inlet pipe at the two compartments on both sides has a bore. The outlet tube is located in the middle compartment, deviating to the side with a smaller expansion inlet, with the longitudinal axis of the outlet tube passing through the inlet tube.
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