Flying Apparatus With Flexible Shell and Coanda-effect

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Aerospace & Defense

FLYING APPARATUS WITH FLEXBILE SHELL AND COANDA -EFFECT
Based on the Invention Patent No. 00121196, CLASA B63H9/04 from 06.12.2006 and Patent application(pending) A/00878/2017 from 26/10/2017

The technical solution is based on a flight apparatus with flexible outer shell, powered by the pressure effect described as the Coandă-Effect, apparatus built as an experimental model for functional tests.

Lenticular vehicles with Coandă Effect are an innovative solution for all flying apparatus with vertical take-off, high-speed flying apparatus, or the ones which require a robust and compact body – reentry body – at high altitudes and high speeds, but also are suitable for water (under water), using the same propulsion.
As a military “vehicle”, it offers a greater tolerance from direct hits.
As a drone it is almost indestructible.

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  • About the Entrant

  • Name:
    Danut Sobol
  • Type of entry:
    individual
  • Patent status:
    pending