WO2024229270 - "G" LOAD SUPRESSING AIRCRAFT
National phase entry is expected:
Publication Number
WO/2024/229270
Publication Date
07.11.2024
International Application No.
PCT/US2024/027508
International Filing Date
02.05.2024
Title **
[English]
"G" LOAD SUPRESSING AIRCRAFT
[French]
AÉRONEF À PRESSION DE CHARGE "G"
Applicants **
WRIGHT, Harold
Inventors
WRIGHT, Harold
Priority Data
18/654,441
05.02.2024
US
18/211,379
19.06.2023
US
63/464,093
04.05.2023
US
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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| Number of Office Actions | * |
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International Searching Authority |
USPTO
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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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| * | |
| * | |
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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 | 2220 | |
| EPO | Filing, Examination, Granting | 8806 | |
| Japan | Filing, Examination, Granting | 2108 | |
| South Korea | Filing, Examination, Granting | 2049 | |
| USA | Filing, Examination, Granting | 4310 |
Total:
19,493
The term for entry into the National Phase has expired. This quotation is for informational purposes only
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Abstract[English]
A "G" load suppressing aircraft incorporating a fuselage having a nose end; a cavity, extending downwardly into the fuselage, the cavity opening upwardly at the fuselage's nose end; a cockpit capsule fitted for receipt within the cavity; explosive bolts for releasably attaching the cockpit capsule to the fuselage, the explosive bolts holding the cockpit capsule within the cavity; a liquid supply line for filling the cockpit capsule with a transparent liquid, the liquid supply line being connected operatively to the cockpit capsule; and rocket engines for ejecting the cockpit capsule from the cavity, the rocket engines being connected operatively to the cockpit.[French]
Aéronef à suppression de charge " G " comprenant : un fuselage présentant un nez; une cavité s'étendant vers le bas dans le fuselage, la cavité s'ouvrant vers le haut au niveau du nez du fuselage; une capsule de cockpit conçue pour être reçue dans la cavité; des boulons explosifs pour fixer de manière amovible la capsule de cockpit au fuselage, les boulons explosifs maintenant la capsule de cockpit à l'intérieur de la cavité; une conduite d'alimentation en liquide pour remplir la capsule du cockpit avec un liquide transparent, la conduite d'alimentation en liquide étant connectée de manière fonctionnelle à la capsule du cockpit; et des moteurs-fusées pour éjecter la capsule du cockpit de la cavité, les moteurs-fusées étant connectés de manière fonctionnelle au cockpit.