FR3083216B1 - STRUCTURE THAT CAN BE ASSEMBLED AND ADJUSTED IN SPACE - Google Patents
STRUCTURE THAT CAN BE ASSEMBLED AND ADJUSTED IN SPACE Download PDFInfo
- Publication number
- FR3083216B1 FR3083216B1 FR1855849A FR1855849A FR3083216B1 FR 3083216 B1 FR3083216 B1 FR 3083216B1 FR 1855849 A FR1855849 A FR 1855849A FR 1855849 A FR1855849 A FR 1855849A FR 3083216 B1 FR3083216 B1 FR 3083216B1
- Authority
- FR
- France
- Prior art keywords
- assembled
- trellis
- adjusted
- space
- functional tile
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000002184 metal Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B7/00—Pliers; Other hand-held gripping tools with jaws on pivoted limbs; Details applicable generally to pivoted-limb hand tools
- B25B7/02—Jaws
- B25B7/04—Jaws adjustable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
- B64G1/2229—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the deployment actuating mechanism
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G4/00—Tools specially adapted for use in space
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/16—Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal
- H01Q15/161—Collapsible reflectors
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Aerials With Secondary Devices (AREA)
- Finishing Walls (AREA)
Abstract
L'invention propose une structure spatiale (1) comprenant un treillis métallique (10) et au moins une tuile fonctionnelle (20) fixée au treillis, caractérisée en ce que chaque tuile fonctionnelle est assemblée au treillis par une pluralité de lames (30) de longueur réglable, lesdites lames étant configurées pour permettre un réglage de la position relative de la tuile fonctionnelle par rapport au treillis et de l'orientation de la tuile fonctionnelle.The invention provides a spatial structure (1) comprising a metal trellis (10) and at least one functional tile (20) fixed to the trellis, characterized in that each functional tile is assembled to the trellis by a plurality of blades (30) of adjustable length, said blades being configured to allow adjustment of the relative position of the functional tile relative to the lattice and of the orientation of the functional tile.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1855849A FR3083216B1 (en) | 2018-06-28 | 2018-06-28 | STRUCTURE THAT CAN BE ASSEMBLED AND ADJUSTED IN SPACE |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1855849A FR3083216B1 (en) | 2018-06-28 | 2018-06-28 | STRUCTURE THAT CAN BE ASSEMBLED AND ADJUSTED IN SPACE |
FR1855849 | 2018-06-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3083216A1 FR3083216A1 (en) | 2020-01-03 |
FR3083216B1 true FR3083216B1 (en) | 2020-05-29 |
Family
ID=63963144
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1855849A Active FR3083216B1 (en) | 2018-06-28 | 2018-06-28 | STRUCTURE THAT CAN BE ASSEMBLED AND ADJUSTED IN SPACE |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3083216B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3122410A1 (en) | 2021-04-30 | 2022-11-04 | Airbus Defence And Space Sas | Reflector satellite and satellite assembly comprising such a satellite |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1084130A (en) * | 1912-11-12 | 1914-01-13 | George H Cargin | Adjustable brazing-clamp. |
US6327944B1 (en) * | 2000-12-27 | 2001-12-11 | Wan Yi Liao | Structure of pliers with variable nose |
DE602004018360D1 (en) * | 2004-12-28 | 2009-01-22 | Alcatel Lucent | Connecting device for space equipment elements with flexible deployable blades |
US8042305B2 (en) * | 2005-03-15 | 2011-10-25 | Alliant Techsystems Inc. | Deployable structural assemblies, systems for deploying such structural assemblies |
US20140232052A1 (en) * | 2013-02-19 | 2014-08-21 | Frank Mendez | Multi-use adjustable vise |
CN203636665U (en) * | 2013-12-25 | 2014-06-11 | 陈钦炀 | Tea pliers |
ITUB20159411A1 (en) * | 2015-12-28 | 2017-06-28 | Stellar Project S R L | COMPACT STABILIZED AIMING SYSTEM |
-
2018
- 2018-06-28 FR FR1855849A patent/FR3083216B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3083216A1 (en) | 2020-01-03 |
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