Pratik Mishra

Pratik Mishra
The present invention describes a comprehensive plant growing system to provide the favourable conditions to grow more variety of plants with improved sustainability. The regenerative moisture content within the plant growing unit makes apparatus and mechanism of the present invention unique and helps in diversified crop cultivation.
It is already known that fuel cells are utilized to regenerate water. In one of the embodiments of the present invention, placement of the MEMS fuel cells and the design of the stacks is such that it’s been incorporated within the plant growing unit to deliver the regenerative moisture. It also helps gas exchange process within the stomata which is the essential feature for transpiration. This facilitates to maintain balance of ecosystem without human efforts.

Patent Application Number: 202021020210

Cerafiber reinforced metal matrix composite

Pratik Mishra & Dr. Rupendra M Anklekar
(Patent Application number:202121006528): This invention was created because currently the composites for the applications such as satellite structures, payloads, extra-terrestrial vehicles etc. are mostly ceramic or carbon fiber reinforced in metal matrix or polymer matrix composites. So, in our present invention we are combining the reinforcements of both the carbon fibers and titanium diboride dispersion/particulates to achieve the bulk properties like enhancing the load bearing capabilities and have also chosen the aluminium 6061 alloy as metal matrix to obtain enhanced mechanical properties such as high tensile strength, high strength-to-weight ratio, high temperature strength, high impact strength and other properties by proper selection of alloying elements and optimal heat treatment/ ageing treatments for improving the strength by solid solution strengthening and precipitation hardening mechanisms/effects . This novel methodology to obtain advanced state-of-the-art hybrid composites would help to design longer space missions and also to improve the
dynamic stability of the spacecraft structures for different mission-based applications such as for both defense and meteorological purposes.

Design of Fluid Plates

Pratik Mishra
This project is about design, fabrication and installation of waste to energy conversion set-up by integrating fuel cell modules using the biomethanation process. Fuel cells use hydrogen at the anode and oxygen at the cathode to produce electricity, some amount of heat and potable water as a by-product. This is also aimed to reduce the damage to the environment, produce energy and reuse the water apart from use of the remaining slurry as fertiliser as is being done in the existing biomethanation plants. The latest design of the bipolar plates used in fuel cell / fluid plates is applied for patent. (Application Number-202021035822) As an add-on invention, the same fluid plates are aimed to be used for the flow of gases in the stack.

Cerafiber Reinforced Metal Matrix Composite

Mr. Pratik Mishra & Dr. Rupendra M Anklekar
(Patent Application number:202121006528): This invention was created because currently the composites for the applications such as satellite structures, payloads, extra-terrestrial vehicles etc. are mostly ceramic or carbon fiber reinforced in metal matrix or polymer matrix composites. So, in our present invention we are combining the reinforcements of both the carbon fibers and titanium diboride dispersion/particulates to achieve the bulk properties like enhancing the load bearing capabilities and have also chosen the aluminium 6061 alloy as metal matrix to obtain enhanced mechanical properties such as high tensile strength, high strength-to-weight ratio, high temperature strength, high impact strength and other properties by proper selection of alloying elements and optimal heat treatment/ ageing treatments for improving the strength by solid solution strengthening and precipitation hardening mechanisms/effects . This novel methodology to obtain advanced state-of-the-art hybrid composites would help to design longer space missions and also to improve the
dynamic stability of the spacecraft structures for different mission-based applications such as for both defense and meteorological purposes.