WO2023161719 - SPACE VEHICLE AND METHOD FOR MANUFACTURE THEREOF

National phase entry:
Publication Number WO/2023/161719
Publication Date 31.08.2023
International Application No. PCT/IB2023/000105
International Filing Date 24.02.2023
Title **
[English] SPACE VEHICLE AND METHOD FOR MANUFACTURE THEREOF
[French] VÉHICULE SPATIAL ET SON PROCÉDÉ DE FABRICATION
Applicants **
NETWORK ACCESS ASSOCIATES LIMITED
Inventors
COLAS, Victor
NAGI, Manraj
Priority Data
2201688   25.02.2022   FR
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 *
*
Number of Office Actions *
*
International Searching Authority
*
Recordal of a Change of the Applicant's Name/Address
*
Type of Assignment
*
Applicant's Legal Status
*
*
*
*
*
*
Entry into National Phase under
*
Patent Delivery
*
Translation

* 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 StagesTotal
China Filing, Examination, Granting1965
EPO Filing, Examination, Granting8141
Japan Filing, Examination, Granting2108
South Korea Filing, Examination, Granting1935
USA Filing, Examination, Granting4740
MasterCard Visa
Total: 18,889

The term for entry into the National Phase has expired. This quotation is for informational purposes only

Contact Us
Abstract[English] Ae methhod includes providing a quantity of sheet metal, press-forming a first panel from the sheet metal to form a first stamped panel, press-forming a second panel from the sheet metal to form a second stamped panel, fixing at least one stiffener to the first stamped panel such that the stiffener extends across a width of the first panel, where a first end of the stiffener is attached to the first stamped panel at a first fixation location, and where a second end of the stiffener is attached to the first stamped panel at a second fixation location, fixing at least one onboard equipment component to the first stamped panel, where at least one of the at least one onboard equipment component is fixed to the stiffener, sealing the first panel to the second panel to form a space vehicle.[French] Un procédé consiste à fournir une quantité de tôle, à former sous pression un premier panneau à partir de la tôle pour former un premier panneau estampé, à former sous pression un second panneau à partir de la tôle pour former un second panneau estampé, à fixer au moins un raidisseur sur le premier panneau estampé de telle sorte que le raidisseur s'étend dans la largeur du premier panneau, une première extrémité du raidisseur étant fixée sur le premier panneau estampé à un premier emplacement de fixation, et une seconde extrémité du raidisseur étant fixée sur le premier panneau estampé à un second emplacement de fixation, à fixer au moins un composant d'équipement embarqué sur le premier panneau estampé, au moins composant dudit composant d'équipement embarqué étant fixé sur le raidisseur, et à étanchéifier le premier panneau avec le second panneau pour former un véhicule spatial.

Rejoining the server...