Description:Specific details of the invention and its intended design are provided below:
Field
The present disclosure (100) relates to the field of unmanned aerial vehicle, and more particularly relates to optimized hybrid unmanned aerial system.
Background
The present disclosure relates to the field of unmanned aerial vehicle, and more particularly relates to the optimized hybrid unmanned aerial system.
Drones, also known as unmanned aerial vehicles (UAVs), are aircraft that operate without a human pilot onboard. They are controlled remotely by a human operator or can fly autonomously through pre-programmed flight paths and automated systems. Drones come in various sizes and configurations, ranging from small, handheld models to large, military grade aircraft.
The concept of drone dates back several decades, but their use and technological advancements have significantly increased in recent years. Initially developed for military purposes, drones were primarily used for surveillance and reconnaissance missions. However, their applications have expanded to various industries, including agriculture, photography, filmmaking, delivery services, infrastructure inspection, disaster management, and scientific research.
In existing period the drones have not gained any pleasant welcome in the daily life of society, they are only acceptable in special events and functions because of just of two reasons that are due to high noise of propellers and due to breach of privacy.
Objective
Some of the objects of the present disclosure, which at least one embodiment here in satisfies, are as follows:
• It is an object of the present disclosure to ameliorate one or more problems of the prior art or to at least provide a useful alternative.
• An object of the present disclosure is to reduce the noise of the drones below the 50db.
• Another object of the present disclosure is to build a system that can be able to fly in the sky of the society without any breach of privacy and safely.
• Still another object of the present disclosure is to provide a system that minimizes vitality maintenance and recovering energy in any kind of worst case scenario.
Other objects and advantages of the present disclosure will be more apparent from the following description, which is not intended to limit the scope of the present disclosure.
Summary
The present subject matter relates to an unmanned aerial system comprising an optimized hybrid unmanned aerial system utilizing the ion propulsion technology along with toroidal propeller to reduce the noise pollution caused by the existing drone systems.
In the present disclosure, both the ionic propulsion or toroidal propeller are powered with a different energy sources, so in case of failure of any one power source the other will going to provide a safe landing of the unmanned aerial system immediately.
In an embodiment, the system includes an ion propulsion and toroidal propeller along with strain gauges.
Detailed Description
Embodiments, of the present disclosure 100, will now be described with reference to the accompanying drawing.
The present disclosure envisages an optimized hybrid model drone utilizing ionic propulsion technology. The system of the present disclosure is helpful in safe landing of an unmanned aerial vehicle in case of any worst scenario as well provides a very low noise profile in system.
In accordance with one embodiment, the system is utilizing the ion propulsion technology (102) along with a toroidal propeller (101) to generate the thrust (103) and lift towards the flying direction.
As multicopter drones are equipped with tradition propellers which now been substituted by tipless toroidal propellers, which aerodynamically controls the noise emission from drone.
Initially these tipped propellers generate noise signature of 70-85 dB of noise pressure, which later with the substitute of toroidal propellers reduced to 55 dB noise signature maximum. This noise pressure is totally dependent on size of drone. More the size of drone, more this noise signature is. This generic figure is taken for medium size drones
In present system (100) here in this ion propulsion technology (102), various forward-reverse polarity electrodes are set in pattern to generate the ionized atmosphere for lift forces. This ionized atmosphere under and side by side of drone create lift forces which is also known ionic wind (lift force in the form wind) or ionic thrust (thrust developed due to ionization).
In the present disclosure(100) where Ionic Propulsion technology(102) provide silent system with respect to lower noise emissions of toroidal propellers, while toroidal propellers provide lift with size of drone lesser than drone solely made with ionic propulsion technology(102).
TECHNICAL ADVANCES AND ECONOMICAL SIGNIFICANCE
The present disclosure described herein above has several technical advantages including, but not limited to, the realization of a system for detecting humidity and soil texture that:
• provides an very low noise profile aerial vehicle ;
• relevant to fly in sky above the society and;
• Safe landing in case of any worst scenario
The embodiments herein and the various features and advantageous details there of are explained with reference to the non-limiting embodiments in the following description. Descriptions of well-known components and processing techniques are omitted so as to not unnecessarily obscure the embodiments herein. The examples used herein are intended merely to facilitate an understanding of ways in which the embodiments herein may be practiced and to further enable those of skill in the art to practice the embodiments herein. Accordingly, the examples should not be construed as limiting the scope of the embodiments herein.
Any discussion of documents, acts, materials, devices, articles or the like that has 15 been included in this specification is solely for the purpose of providing a context for the disclosure. It is not to be taken as an admission that any or all of these matters form a part of the prior art base or were common general knowledge in the field relevant to the disclosure as it existed anywhere before the priority date of this application.
The numerical values mentioned for the various physical parameters, dimensions or quantities are only approximations and it is envisaged that the values higher/lower than the numerical values assigned to the parameters, dimensions or quantities fall within the scope of the disclosure, unless there is a statement in the specification specific to the contrary.
, Claims:We Claim
1. An optimized hybrid unmanned aerial system utilizing an ion propulsion technology along with toroidal propeller (100) comprising each of the technology ionic propulsion (102) or toroidal propeller (101) are powered with a different source (battery), so in case of failure of one power source (battery) the other will going to provide a safe landing of the aerial system.
2. Optimized hybrid unmanned aerial system utilizing an ion propulsion along with toroidal propeller as claimed in claim 1, wherein the smart controlling system of drone is going to reduce the rate of descent (ROD), i.e. control the fast falling at the initiation of free fall due to any failure.
3. Optimized hybrid unmanned aerial system utilizing an ion propulsion along with toroidal propeller as claimed in claim 1, is a setup of strain gauges is integrated on lower part of landing gear stand to consume the jerk or impact forces from ground and accomplish energy recuperation by energy transduction at strain gauges.
4. Optimized hybrid unmanned aerial system utilizing an ion propulsion along with toroidal propeller as claimed in claim 1, is a compact unmanned aerial system unit is comparatively of smaller size and generates noise signature lesser than 45 dB noise pressure.
5. Optimized hybrid unmanned aerial system utilizing an ion propulsion along with toroidal propeller as claimed in claim 1, An optimized hybrid unmanned aerial system employing ion propulsion technology and toroidal propeller, wherein the power management system is configured to dynamically allocate power from either source (battery) to ensure uninterrupted operation and safe landing in the event of a power source failure.
6. Optimized hybrid unmanned aerial system utilizing an ion propulsion along with toroidal propeller as claimed in claim 1, wherein the power management system incorporates real-time monitoring and predictive algorithms to anticipate potential power source failures and proactively adjust power allocation for optimal performance and safety.