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 PDF

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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
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France
Prior art keywords
hollow body
elongated hollow
state
deploying
rolled
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FR2003508A
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English (en)
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FR3094974A1 (fr
Inventor
Marco Straubel
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Deutsches Zentrum fuer Luft und Raumfahrt eV
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Deutsches Zentrum fuer Luft und Raumfahrt eV
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Publication of FR3094974A1 publication Critical patent/FR3094974A1/fr
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Classifications

    • 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)
  • Unwinding Of Filamentary Materials (AREA)
  • Tents Or Canopies (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
FR2003508A 2019-04-12 2020-04-08 Dispositif et procédé pour déployer un corps creux de forme allongée se trouvant à l’état enroulé Active FR3094974B1 (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
WO2000057685A2 (fr) * 1999-03-22 2000-10-05 Ilc Dover, Inc. Procede d'actionnement lineaire par gonflement et dispositif correspondant
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
WO2020150735A1 (fr) * 2019-01-18 2020-07-23 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

Also Published As

Publication number Publication date
US11772827B2 (en) 2023-10-03
FR3094974A1 (fr) 2020-10-16
US20200324921A1 (en) 2020-10-15
DE102019109810B4 (de) 2023-01-19
DE102019109810A1 (de) 2020-10-15

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