WO2022175739 - RAMJET OR SCRUM JET AIRCRAFT ENGINE WITH THE CAPABILITY OF MOUNTING TWO FANS BEHIND THE AIRCRAFT'S NOZZLE
National phase entry is expected:
Publication Number
WO/2022/175739
Publication Date
25.08.2022
International Application No.
PCT/IB2021/060846
International Filing Date
23.11.2021
Title **
[English]
RAMJET OR SCRUM JET AIRCRAFT ENGINE WITH THE CAPABILITY OF MOUNTING TWO FANS BEHIND THE AIRCRAFT'S NOZZLE
[French]
MOTEUR D'AÉRONEF À STATORÉACTEUR OU SUPERSTATORÉACTEUR AYANT LA CAPACITÉ DE MONTER DEUX SOUFFLANTES APRÈS LA TUYÈRE DE L'AÉRONEF
Applicants **
NEJATI, Mohammadamin
Secretariat section milad hospital hemmat highway Tehran
Tehran, 1449614531, IR
Inventors
NEJATI, Mohammadamin
Secretariat section milad hospital hemmat highway Tehran
Tehran, 1449614531, IR
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
| Number of Priorities | * |
| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
| Pages for Publication | * |
| Number of Pages with Drawings | * |
| Pages of Specification | * |
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International Searching Authority |
IP India
* |
| Applicant's Legal Status |
Natural Person
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| * | |
| * | |
| * | |
| Entry into National Phase under |
Chapter I
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| Translation |
|
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Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing | 900 | |
| EPO | Filing, Examination | 5349 | |
| Japan | Filing | 591 | |
| South Korea | Filing | 482 | |
| USA | Filing, Examination | 2710 |
Total: 10032 USD
The term for entry into the National Phase has expired. This quotation is for informational purposes only
Abstract[English]
Ramjet or Scrum jet aircraft engine with the capability of mounting two fans behind the aircraft's nozzle. This invention installed in the exhaust section of the aircraft (behind the aircraft nozzle). It has two fans, one of which is located in the smoke section of the aircraft (high pressure wind) and one of the fans is installed in the open air and starts to rotate when as these fans begin to rotate, fresh air is blown into the combustion chamber of the engine and the purpose of this design is to reach the top speed of a Mach.[French]
La présente invention concerne un moteur d'aéronef à statoréacteur ou à superstatoréacteur ayant la capacité de monter deux soufflantes après la tuyère de l'aéronef. La présente invention est installée dans la partie échappement de l'aéronef (après la tuyère de l'aéronef). Il comporte deux soufflantes dont l'une est située dans la section de fumée de l'aéronef (vent à haute pression) et l'une des soufflantes est installée à l'air libre et commence à tourner lorsque à mesure que ces soufflantes commencent à tourner, de l'air frais est soufflé dans la chambre de combustion du moteur et l'objectif de cette conception est d'atteindre la vitesse maximale d'un Mach.