FR3015955B1 - Structure segmentee, en particulier pour reflecteur d'antenne de satellite, pourvue d'au moins un dispositif de deploiement a rotation et translation - Google Patents
Structure segmentee, en particulier pour reflecteur d'antenne de satellite, pourvue d'au moins un dispositif de deploiement a rotation et translationInfo
- Publication number
- FR3015955B1 FR3015955B1 FR1303110A FR1303110A FR3015955B1 FR 3015955 B1 FR3015955 B1 FR 3015955B1 FR 1303110 A FR1303110 A FR 1303110A FR 1303110 A FR1303110 A FR 1303110A FR 3015955 B1 FR3015955 B1 FR 3015955B1
- Authority
- FR
- France
- Prior art keywords
- translation
- rotation
- deployment device
- satellite antenna
- antenna reflector
- 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.)
- Expired - Fee Related
Links
Classifications
-
- 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
- H01Q15/162—Collapsible reflectors composed of a plurality of rigid panels
-
- 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
-
- 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
- B64G1/2221—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 manner of deployment
- B64G1/2222—Folding
- B64G1/2224—Folding about multiple axes
-
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/08—Means for collapsing antennas or parts thereof
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/288—Satellite antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/12—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems
- H01Q3/16—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aerials With Secondary Devices (AREA)
- Details Of Aerials (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1303110A FR3015955B1 (fr) | 2013-12-30 | 2013-12-30 | Structure segmentee, en particulier pour reflecteur d'antenne de satellite, pourvue d'au moins un dispositif de deploiement a rotation et translation |
US15/102,491 US20160322710A1 (en) | 2013-12-30 | 2014-12-10 | Segmented structure, in particular for a satellite antenna reflector, provided with at least one rotational and translational deployment device |
EP14824038.5A EP3089913A1 (fr) | 2013-12-30 | 2014-12-10 | Structure segmentée, en particulier pour réflecteur d'antenne de satellite, pourvue d'au moins un dispositif de déploiement à rotation et translation |
CA2931924A CA2931924A1 (fr) | 2013-12-30 | 2014-12-10 | Structure segmentee, en particulier pour reflecteur d'antenne de satellite, pourvue d'au moins un dispositif de deploiement a rotation et translation |
PCT/FR2014/000268 WO2015101723A1 (fr) | 2013-12-30 | 2014-12-10 | Structure segmentée, en particulier pour réflecteur d'antenne de satellite, pourvue d'au moins un dispositif de déploiement à rotation et translation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1303110A FR3015955B1 (fr) | 2013-12-30 | 2013-12-30 | Structure segmentee, en particulier pour reflecteur d'antenne de satellite, pourvue d'au moins un dispositif de deploiement a rotation et translation |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3015955A1 FR3015955A1 (fr) | 2015-07-03 |
FR3015955B1 true FR3015955B1 (fr) | 2016-12-30 |
Family
ID=50780521
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1303110A Expired - Fee Related FR3015955B1 (fr) | 2013-12-30 | 2013-12-30 | Structure segmentee, en particulier pour reflecteur d'antenne de satellite, pourvue d'au moins un dispositif de deploiement a rotation et translation |
Country Status (5)
Country | Link |
---|---|
US (1) | US20160322710A1 (fr) |
EP (1) | EP3089913A1 (fr) |
CA (1) | CA2931924A1 (fr) |
FR (1) | FR3015955B1 (fr) |
WO (1) | WO2015101723A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10661918B2 (en) * | 2016-10-04 | 2020-05-26 | Space Systems/Loral, Llc | Self-assembling persistent space platform |
US10957986B2 (en) * | 2017-08-04 | 2021-03-23 | Space Systems/Loral, Llc | Reconfigurable spacecraft with a hold-down assembly for a rigid reflector |
CN108945523B (zh) * | 2018-09-04 | 2023-07-25 | 燕山大学 | 四棱柱可展单元以及基于四棱柱可展单元的空间伸展机构 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4811034A (en) * | 1987-07-31 | 1989-03-07 | Trw Inc. | Stowable reflector |
JPH06253476A (ja) * | 1993-02-25 | 1994-09-09 | Rocket Syst:Kk | 太陽発電の受電装置 |
US6191757B1 (en) * | 1999-04-08 | 2001-02-20 | Hughes Electronics Corporation | System for compact stowage of segmented dish reflectors |
US6859188B1 (en) * | 2003-03-27 | 2005-02-22 | Lockheed Martin Corporation | Rotationally configurable offset reflector antenna |
SE0402167L (sv) * | 2004-09-10 | 2006-01-10 | Ayen Technology Ab | Hopfällbar parabolreflektor |
US9331394B2 (en) * | 2011-09-21 | 2016-05-03 | Harris Corporation | Reflector systems having stowable rigid panels |
-
2013
- 2013-12-30 FR FR1303110A patent/FR3015955B1/fr not_active Expired - Fee Related
-
2014
- 2014-12-10 EP EP14824038.5A patent/EP3089913A1/fr not_active Withdrawn
- 2014-12-10 CA CA2931924A patent/CA2931924A1/fr not_active Abandoned
- 2014-12-10 WO PCT/FR2014/000268 patent/WO2015101723A1/fr active Application Filing
- 2014-12-10 US US15/102,491 patent/US20160322710A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
FR3015955A1 (fr) | 2015-07-03 |
US20160322710A1 (en) | 2016-11-03 |
EP3089913A1 (fr) | 2016-11-09 |
WO2015101723A1 (fr) | 2015-07-09 |
CA2931924A1 (fr) | 2015-07-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 3 |
|
CA | Change of address |
Effective date: 20151224 |
|
CD | Change of name or company name |
Owner name: AIRBUS DEFENCE AND SPACE SAS, FR Effective date: 20151224 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
ST | Notification of lapse |
Effective date: 20180831 |