WO2023068947 - VORTEX GENERATING CANNON SYSTEM
National phase entry is expected:
Publication Number
WO/2023/068947
Publication Date
27.04.2023
International Application No.
PCT/PH2022/050018
International Filing Date
20.10.2022
Title **
[English]
VORTEX GENERATING CANNON SYSTEM
[French]
SYSTÈME DE CANON GÉNÉRATEUR DE TOURBILLON
Applicants **
ELEDIA, El Arby
Inventors
ELEDIA, El Arby
Priority Data
12021050542
23.10.2021
PH
Application details
| Total Number of Claims/PCT | * |
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International Searching Authority |
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| Recordal of a Change of the Applicant's Name/Address |
Change of Applicant's Name and Address
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| Type of Assignment |
The Standard Agent's Assignment
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| Applicant's Legal Status |
Natural Person
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| Entry into National Phase under |
Chapter I
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| Patent Delivery |
Send the Letters Patent by Courier
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| Translation |
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* The data is based on automatic recognition. Please verify and amend if necessary.
** IP-Coster compiles data from publicly available sources. If this data includes your personal information, you can contact us to request its removal.
Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing, Examination, Granting | 2358 | |
| EPO | Filing, Examination, Granting | 11905 | |
| Japan | Filing, Examination, Granting | 2543 | |
| South Korea | Filing, Examination, Granting | 2691 | |
| USA | Filing, Examination, Granting | 5730 |
Total:
25,227
The term for entry into the National Phase has expired. This quotation is for informational purposes only
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Abstract[English]
There is provided a vortex generating cannon system comprising a compression means for creating a fluid flow, a barrel comprising a first fluid inlet, and a fluid outlet; the first fluid inlet and the fluid outlet defining a bore or a tube through which the fluid flow from the compression means enters and exits the barrel. The vortex generating cannon system further comprising a closed loop wing deflector situated within the barrel enhancing a fluid convection initiated by the compression means thereby generating, launching, and propelling a vortex loop of fluid towards a target and a support means to hold the closed loop wing deflector in place within the barrel.[French]
L'invention concerne un système de canon générateur de tourbillon comprenant un moyen de compression pour créer un écoulement de fluide, un cylindre comprenant un premier orifice d'entrée de fluide, ainsi qu'un orifice de sortie de fluide ; le premier orifice d'entrée de fluide et l'orifice de sortie de fluide définissant un alésage ou un tube à travers lequel l'écoulement de fluide provenant du moyen de compression pénètre dans le cylindre et en ressort. Le système de canon générateur de tourbillon selon l'invention comprend également un déflecteur d'aile en boucle fermée situé à l'intérieur du cylindre, améliorant la convection de fluide initiée par le moyen de compression, générant, lançant et propulsant ainsi une boucle tourbillonnaire de fluide vers une cible, ainsi qu'un moyen de support pour maintenir le déflecteur d'aile en boucle fermée en place à l'intérieur du cylindre.