WO2024201492 - A SYSTEM FOR TRAVERSING THROUGH A FLUIDIC MEDIUM

National phase entry:
Publication Number WO/2024/201492
Publication Date 03.10.2024
International Application No. PCT/IN2024/050249
International Filing Date 11.03.2024
Title **
[English] A SYSTEM FOR TRAVERSING THROUGH A FLUIDIC MEDIUM
[French] SYSTÈME DE TRAVERSÉE D'UN MILIEU FLUIDIQUE
Applicants **
BKSAY WORKS PVT LTD B-18/6, Himalaya Pride, Techzone–IV, Gr. Noida West, Gautam Buddha Nagar, Delhi NCR, Uttar Pradesh, India (Bharat). Gautam Buddha Nagar 201309, IN
Inventors
POTUKUCHI, Kalyan B-18/6, Himalaya Pride, Techzone–IV, Gr. Noida West, Gautam Buddha Nagar, Delhi NCR, Uttar Pradesh, India (Bharat). Gautam Buddha Nagar 201309, IN
J H S D, Anoohya Flat no - 104, Sri Sai Chaitanya Residency, Near Unicent School, Miyapur, Hyderabad, Telangana, India (Bharat). Hyderabad 500049, IN
Priority Data
202311023764   30.03.2023   IN
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Quotation for National Phase entry

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China Filing1511
EPO Filing, Examination8128
Japan Filing531
South Korea Filing575
USA Filing, Examination2635
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Total: 13380

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Abstract[English] A Fluid traversing system disclosed herein. The fluid traversing system, or FTS (116), comprising primarily at least one self-vectoring craft, or SVC (111), wherein each SVC has one or more detachable coupling means, or DC (114). Further, each SVC has a plethora of components in order to, sustain independent stable motion through a fluidic medium, establish wired/wireless communications, generate power and has a plurality of DC that are selectively controlled, in order to couple with another SVC and/or any other type of crafts and/or various payloads. Furthermore, each SVC has a plurality of pivotable/displaceable rotors/stators coupled within the fuselage/hull of the SVC. Further, each rotor/stator has a plurality of blades (112), wherein each blade is selectively pivoted/articulated with respect to the said rotor/stator or other blades.[French] Est divulgué un système de traversée de fluide. Le système de traversée de fluide, ou FTS (116), comprend principalement au moins un engin autonome, ou SVC (111), chaque SVC comportant un ou plusieurs moyens d'accouplement détachables, ou DC (114). En outre, chaque SVC comporte une multitude de composants afin de maintenir un déplacement stable indépendant dans un milieu fluidique, d'établir des communications filaires/sans fil, de générer de l'énergie et comporte une pluralité de DC qui sont commandés sélectivement, afin de s'accoupler à un autre SVC et/ou à tout autre type d'embarcations et/ou à diverses charges utiles. En outre, chaque SVC comporte une pluralité de rotors/stators pivotants/déplaçables accouplés à l'intérieur du fuselage/de la coque du SVC. En outre, chaque rotor/stator comporte une pluralité de pales (112), chaque pale étant pivotée/articulée sélectivement par rapport audit rotor/stator ou à d'autres pales.
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