FR3094974B1 - Dispositif et procédé pour déployer un corps creux de forme allongée se trouvant à l’état enroulé - Google Patents
Dispositif et procédé pour déployer un corps creux de forme allongée se trouvant à l’état enroulé Download PDFInfo
- Publication number
- FR3094974B1 FR3094974B1 FR2003508A FR2003508A FR3094974B1 FR 3094974 B1 FR3094974 B1 FR 3094974B1 FR 2003508 A FR2003508 A FR 2003508A FR 2003508 A FR2003508 A FR 2003508A FR 3094974 B1 FR3094974 B1 FR 3094974B1
- Authority
- FR
- France
- Prior art keywords
- hollow body
- elongated hollow
- state
- deploying
- rolled
- 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.)
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Classifications
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- 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
- B64G1/2227—Inflating
-
- 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
- B64G1/223—Modular spacecraft systems
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Storage Of Web-Like Or Filamentary Materials (AREA)
- Tents Or Canopies (AREA)
- Unwinding Of Filamentary Materials (AREA)
Abstract
L’invention concerne un dispositif de déploiement d’un corps creux de forme allongée présentant : au moins un corps creux allongé comportant deux demi-corps de coque allongés (2a, 2b) et pour première extrémité une racine, un mandrin (13) monté rotatif, sur lequel l’au moins un corps creux allongé est, dans un premier état, enroulé et comprimé, et dans un deuxième état, déroulé et déployé, de sorte qu’une cavité allongée (4) se forme entre les deux demi-corps, le premier demi-corps est fixé au mandrin rotatif dans la zone de la racine, un mécanisme d’expansion étant en prise avec le second demi-corps dans la zone de la racine, et écarte le second demi-corps du mandrin rotatif, afin d’assurer l’expansion de la section transversale de l’au moins un corps creux allongé dans ladite zone, quand ce dernier est déroulé du mandrin rotatif. Figure pour l’abrégé : Fig. 2
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102019109810.6A DE102019109810B4 (de) | 2019-04-12 | 2019-04-12 | Vorrichtung und Verfahren zum Entfalten eines aufgerollten länglichen Hohlkörpers |
DE102019109810.6 | 2019-04-12 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3094974A1 FR3094974A1 (fr) | 2020-10-16 |
FR3094974B1 true FR3094974B1 (fr) | 2023-06-16 |
Family
ID=72613512
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2003508A Active FR3094974B1 (fr) | 2019-04-12 | 2020-04-08 | Dispositif et procédé pour déployer un corps creux de forme allongée se trouvant à l’état enroulé |
Country Status (3)
Country | Link |
---|---|
US (1) | US11772827B2 (fr) |
DE (1) | DE102019109810B4 (fr) |
FR (1) | FR3094974B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11142350B2 (en) * | 2018-10-24 | 2021-10-12 | Purdue Research Foundation | Compact scalable drag sail deployment assembly |
DE102019109810B4 (de) | 2019-04-12 | 2023-01-19 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung und Verfahren zum Entfalten eines aufgerollten länglichen Hohlkörpers |
WO2024057287A1 (fr) * | 2022-09-16 | 2024-03-21 | Auckland Uniservices Limited | Mécanisme de mât déployable et ses applications |
Family Cites Families (42)
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US3361377A (en) * | 1965-12-30 | 1968-01-02 | Melpar Inc | Extendible-retractable boom |
US3434674A (en) * | 1967-05-01 | 1969-03-25 | Dehavilland Aircraft Canada | Storable tubular extensible member device |
US3589632A (en) * | 1969-04-30 | 1971-06-29 | Westinghouse Electric Corp | Self-forming-boom storing and deploying apparatus |
US3862528A (en) * | 1970-05-04 | 1975-01-28 | Trw Inc | Deployable boom |
US4195804A (en) * | 1978-03-30 | 1980-04-01 | General Dynamics Corporation | Space platform docking device |
US5094410A (en) * | 1989-10-31 | 1992-03-10 | Space Industries, Inc. | Capture/berthing system for spacecraft |
US6126115A (en) * | 1997-01-21 | 2000-10-03 | Lockheed Martin Corporation | Apparatus for retaining and releasing a payload |
DE19825785C2 (de) * | 1998-06-10 | 2000-04-27 | Deutsch Zentr Luft & Raumfahrt | Solarsegler mit Segelfolie und Faltrohren |
AU6046000A (en) * | 1999-03-22 | 2000-10-16 | Ilc Dover, Inc. | Method of linear actuation by inflation and apparatus therefor |
US7857261B2 (en) * | 2001-11-01 | 2010-12-28 | Michigan Aerospace Corporation | Docking system |
US7828249B2 (en) * | 2004-03-18 | 2010-11-09 | Michigan Aerospace Corporation | Docking system |
DE102004021569A1 (de) | 2004-05-03 | 2005-12-01 | Hts - Hoch Technologie Systeme Gmbh | Vorrichtung, Verfahren und dünnwandiger Hohlprofilstrang zum Ausfahren und/oder Abstützen flexibler Solarzellenmodule |
JP5276952B2 (ja) * | 2008-11-05 | 2013-08-28 | サカセ・アドテック株式会社 | 伸展構造物 |
US8863369B2 (en) * | 2011-09-13 | 2014-10-21 | Composite Technology Development, Inc. | Slit tube locking longeron |
US9399295B2 (en) * | 2012-03-19 | 2016-07-26 | Macdonald, Dettwiler And Associates Inc. | Spacecraft capture mechanism |
US9151069B2 (en) * | 2012-04-23 | 2015-10-06 | Stephen M. Bobbio | Spool-mounted coiled structural extending member |
US9555904B2 (en) * | 2012-08-09 | 2017-01-31 | Analytical Mechanics Associates, Inc. | Gossamer apparatus and systems for use with spacecraft |
FR2998876B1 (fr) | 2012-12-05 | 2015-07-17 | Thales Sa | Dispositif de deploiement et de reploiement d'une structure flexible, structure deployable flexible et satellite munis d'un tel dispositif |
PL405939A1 (pl) * | 2013-11-06 | 2015-05-11 | Centrum Badań Kosmicznych Polskiej Akademii Nauk | Mechanizm zaciskowy, układ blokujący oraz sposób operowania manipulatorem rekonfigurowalnym |
US9593485B2 (en) * | 2014-03-12 | 2017-03-14 | Roccor, Llc | Deployment system for supported retractable extension of a composite boom |
US10266368B2 (en) * | 2014-06-07 | 2019-04-23 | Composite Technology Development, Inc. | Wedge and mandrel assembly for slit-tube longerons |
FR3025498B1 (fr) * | 2014-09-05 | 2017-12-08 | Thales Sa | Mat deployable a deploiement spontane autonome et satellite comportant au moins un tel mat |
US10160555B2 (en) * | 2015-04-22 | 2018-12-25 | Composite Technology Development, Inc. | Multiple boom deployment |
US9863148B2 (en) * | 2015-08-28 | 2018-01-09 | The United States Of America As Represented By The Administrator Of Nasa | Sheath-based rollable lenticular-shaped and low-stiction composite boom |
US9796488B2 (en) * | 2015-10-02 | 2017-10-24 | The Boeing Company | Dual port payload attach ring compatible satellite |
US10196817B2 (en) * | 2016-04-15 | 2019-02-05 | Composite Technology Development, Inc. | Locking mechanism for deployable booms |
US10611502B2 (en) * | 2016-10-20 | 2020-04-07 | Roccor, Llc | Precision deployment devices, systems, and methods |
SK8501Y1 (sk) * | 2017-02-14 | 2019-08-05 | Zepelin S R O | Nafukovací nosník a použitie tohto nafukovacieho nosníka |
IT201700039763A1 (it) * | 2017-04-11 | 2018-10-11 | Univ Degli Studi Padova | Apparecchiatura automatica per il lancio ed il recupero controllato di una massa tethered in orbita |
FR3071822B1 (fr) * | 2017-10-04 | 2020-11-27 | Arianegroup Sas | Mat deployable de satellite |
DE102018105765A1 (de) * | 2018-03-13 | 2019-09-19 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zum Herstellen eines Faserverbund-Hohlbauteils und Faserverbund-Hohlbauteil |
US11047132B2 (en) * | 2018-05-27 | 2021-06-29 | Roccor, Llc | Boom deployer devices, systems, and methods |
DE102018112690B4 (de) * | 2018-05-28 | 2022-02-17 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung zum Entfalten eines aufgerollten länglichen Hohlkörpers |
DE102018112691B4 (de) * | 2018-05-28 | 2021-07-22 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung zum Entfalten eines aufgerollten länglichen Hohlkörpers |
US10819038B2 (en) * | 2018-06-20 | 2020-10-27 | Eagle Technology, Llc | Mesh reflector satellites antennas with on-orbit extruded or printed supported structure |
US20200002027A1 (en) * | 2018-06-29 | 2020-01-02 | Manuel Victor Borrego Borrego | Hollow structure for creating pressurized space habitats |
JP7164169B2 (ja) * | 2018-10-09 | 2022-11-01 | 株式会社Outsense | 展開構造物 |
EP3912224A4 (fr) * | 2019-01-18 | 2022-10-05 | M.M.A. Design, LLC | Système déployable à membrane souple |
DE102019109810B4 (de) | 2019-04-12 | 2023-01-19 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung und Verfahren zum Entfalten eines aufgerollten länglichen Hohlkörpers |
US11177576B2 (en) * | 2019-06-26 | 2021-11-16 | Eagle Technology, Llc | Antenna having deployable antenna fins and associated methods |
US11958637B2 (en) * | 2020-04-22 | 2024-04-16 | Geoshade Corporal | Gyromesh solar sail spacecraft and sail panel assemblies |
US11643226B1 (en) * | 2020-09-01 | 2023-05-09 | Lockheed Martin Corporation | Spacecraft mating mechanisms |
-
2019
- 2019-04-12 DE DE102019109810.6A patent/DE102019109810B4/de active Active
-
2020
- 2020-04-06 US US16/840,859 patent/US11772827B2/en active Active
- 2020-04-08 FR FR2003508A patent/FR3094974B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
DE102019109810A1 (de) | 2020-10-15 |
DE102019109810B4 (de) | 2023-01-19 |
US20200324921A1 (en) | 2020-10-15 |
FR3094974A1 (fr) | 2020-10-16 |
US11772827B2 (en) | 2023-10-03 |
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PLSC | Publication of the preliminary search report |
Effective date: 20220603 |
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