WO2023161713 - SYSTEM FOR RETENTION AND DEPLOYMENT OF SPACE VEHICLES
National phase entry:
Publication Number
WO/2023/161713
Publication Date
31.08.2023
International Application No.
PCT/IB2023/000091
International Filing Date
24.02.2023
Title **
[English]
SYSTEM FOR RETENTION AND DEPLOYMENT OF SPACE VEHICLES
[French]
SYSTÈME DE RÉTENTION ET DE DÉPLOIEMENT DE VÉHICULES SPATIAUX
Applicants **
NETWORK ACCESS ASSOCIATES
Inventors
PONCET, Dominique
NAGI, Manraj
Priority Data
2201682
25.02.2022
FR
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
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| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
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| Pages of Specification | * |
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| Number of Office Actions | * |
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International Searching Authority |
EPO
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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 |
Legal Entity
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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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| 译文 |
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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 | 1967 | |
| EPO | Filing, Examination, Granting | 8113 | |
| Japan | Filing, Examination, Granting | 2091 | |
| South Korea | Filing, Examination, Granting | 1945 | |
| USA | Filing, Examination, Granting | 4740 |
Total:
18,856
The term for entry into the National Phase has expired. This quotation is for informational purposes only
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Abstract[English]
A space vehicle includes a body; a stacking pillar (200a) coupled to an exterior of the body and defining a longitudinal axis, wherein the stacking pillar (200a) is configured to be removably coupled to a stacking pillar (200b) of an adjacent space vehicle; and an engagement mechanism including: a pivot point within the stacking pillar (200a, 200b) defining a pivot axis perpendicular to the longitudinal axis; and a mounting post (300a) positioned within the stacking pillar (200a) and pivotably engaged with the pivot point so as to be pivotable about the pivot axis between a locked position and an unlocked position, wherein the mounting post (300a) is spring-biased to the unlocked position, and wherein the mounting post is configured to restrain the space vehicle from movement away from the adjacent space vehicle when the mounting post (300a) is positioned in the locked position and a mounting post (300b) of the adjacent space vehicle is positioned in a locked position.[French]
Un véhicule spatial comprend un corps; un pilier d'empilement(200a) accouplé à une partie extérieure du corps et définissant un axe longitudinal, le pilier d'empilement (200a) étant conçu pour être accouplé amovible à un pilier d'empilement (200b) d'un véhicule spatial adjacent; et un mécanisme de mise en prise comprenant : un point de pivotement à l'intérieur du pilier d'empilement (200a, 200b) définissant un axe de pivotement perpendiculaire à l'axe longitudinal; et un montant (300a) positionné à l'intérieur du pilier d'empilement (200a) et en prise pivotante avec le point de pivotement de façon à pouvoir pivoter autour de l'axe de pivotement entre une position verrouillée et une position déverrouillée, le montant (300a) étant sollicité par ressort vers la position déverrouillée, et le montant étant conçu pour empêcher le véhicule spatial de se déplacer à l'opposé du véhicule spatial adjacent lorsque le montant (300a) est positionné dans la position verrouillée et un montant (300b) du véhicule spatial adjacent est positionné dans une position verrouillée.