FR3098651B1 - THREE-DIMENSIONAL DEPLOYMENT DEVICE - Google Patents

THREE-DIMENSIONAL DEPLOYMENT DEVICE Download PDF

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Publication number
FR3098651B1
FR3098651B1 FR1907785A FR1907785A FR3098651B1 FR 3098651 B1 FR3098651 B1 FR 3098651B1 FR 1907785 A FR1907785 A FR 1907785A FR 1907785 A FR1907785 A FR 1907785A FR 3098651 B1 FR3098651 B1 FR 3098651B1
Authority
FR
France
Prior art keywords
deployment device
configuration
intended
closed configuration
mandrel
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
Application number
FR1907785A
Other languages
French (fr)
Other versions
FR3098651A1 (en
Inventor
Yannick Baudasse
François Guinot
Valentin Bouchet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
Original Assignee
Thales SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Thales SA filed Critical Thales SA
Priority to FR1907785A priority Critical patent/FR3098651B1/en
Publication of FR3098651A1 publication Critical patent/FR3098651A1/en
Application granted granted Critical
Publication of FR3098651B1 publication Critical patent/FR3098651B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
    • B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
    • B65H75/18—Constructional details
    • B65H75/28—Arrangements for positively securing ends of material
    • B65H75/285—Holding devices to prevent the wound material from unwinding
    • 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
    • H01Q1/085—Flexible aerials; Whip aerials with a resilient base
    • H01Q1/087—Extensible roll- up aerials
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/20—Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a curvilinear path
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/30—Resonant antennas with feed to end of elongated active element, e.g. unipole
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00—Handled material; Storage means
    • B65H2701/30—Handled filamentary material
    • B65H2701/37—Tapes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Details Of Aerials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Air Bags (AREA)

Abstract

L’invention concerne un dispositif de déploiement (10) apte à être en configuration fermée ou en configuration ouverte, caractérisé en ce qu’il comprend : un mandrin (11) autour duquel au moins un mètre-ruban (12) est destiné à être en configuration enroulée autour d’un premier axe Z en configuration fermée du dispositif de déploiement (10), une attache (13) configurée pour maintenir en configuration fermée le au moins un mètre-ruban (12), un dispositif de libération (14) de l’attache (13) destiné à faire passer le dispositif de déploiement (10) de la configuration fermée à la configuration ouverte dans laquelle le au moins un mètre-ruban (12) est destiné à être dans une configuration déployée selon un deuxième axe X tangent au mandrin (11). Figure pour l’abrégé : Fig. 1The invention relates to a deployment device (10) adapted to be in a closed configuration or in an open configuration, characterized in that it comprises: a mandrel (11) around which at least one measuring tape (12) is intended to be in a configuration wound around a first axis Z in a closed configuration of the deployment device (10), a clip (13) configured to hold the at least one measuring tape (12) in a closed configuration, a release device (14) of the clip (13) intended to change the deployment device (10) from the closed configuration to the open configuration in which the at least one tape measure (12) is intended to be in a deployed configuration along a second axis X tangent to the mandrel (11). Figure for the abstract: Fig. 1

FR1907785A 2019-07-11 2019-07-11 THREE-DIMENSIONAL DEPLOYMENT DEVICE Active FR3098651B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1907785A FR3098651B1 (en) 2019-07-11 2019-07-11 THREE-DIMENSIONAL DEPLOYMENT DEVICE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1907785A FR3098651B1 (en) 2019-07-11 2019-07-11 THREE-DIMENSIONAL DEPLOYMENT DEVICE
FR1907785 2019-07-11

Publications (2)

Publication Number Publication Date
FR3098651A1 FR3098651A1 (en) 2021-01-15
FR3098651B1 true FR3098651B1 (en) 2022-07-08

Family

ID=69190838

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1907785A Active FR3098651B1 (en) 2019-07-11 2019-07-11 THREE-DIMENSIONAL DEPLOYMENT DEVICE

Country Status (1)

Country Link
FR (1) FR3098651B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6762722B2 (en) * 2001-05-18 2004-07-13 Ipr Licensing, Inc. Directional antenna
FR3024227B1 (en) * 2014-07-25 2018-02-09 Thales RECOVERABLE METER-RIBBON RECESSING METHOD FOR DEPLOYABLE STRUCTURE AND DEPLOYABLE METER-RIBBON STRUCTURE
FR3024228B1 (en) * 2014-07-25 2018-02-09 Thales DEPLOYABLE STRUCTURE WITH METER-RIBBON
US10347974B1 (en) * 2018-01-26 2019-07-09 Eagle Technology, Llc Deployable biconical radio frequency (RF) satellite antenna and related methods

Also Published As

Publication number Publication date
FR3098651A1 (en) 2021-01-15

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