AU1177092A - Device for unfolding a stack of elements - Google Patents

Device for unfolding a stack of elements

Info

Publication number
AU1177092A
AU1177092A AU11770/92A AU1177092A AU1177092A AU 1177092 A AU1177092 A AU 1177092A AU 11770/92 A AU11770/92 A AU 11770/92A AU 1177092 A AU1177092 A AU 1177092A AU 1177092 A AU1177092 A AU 1177092A
Authority
AU
Australia
Prior art keywords
elements
stack
unfolding
rotation
axes
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.)
Abandoned
Application number
AU11770/92A
Inventor
F. W. Adolf Berger
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.)
F W ADOLF BERGER
Original Assignee
F W ADOLF BERGER
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
Priority claimed from DE19914101637 external-priority patent/DE4101637A1/en
Priority claimed from DE19914125704 external-priority patent/DE4125704A1/en
Application filed by F W ADOLF BERGER filed Critical F W ADOLF BERGER
Publication of AU1177092A publication Critical patent/AU1177092A/en
Abandoned legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2221Parts 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
    • B64G1/2222Folding
    • B64G1/2224Folding about multiple axes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2221Parts 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
    • B64G1/2226Telescoping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2228Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the hold-down or release mechanisms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2229Parts 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/44Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerials With Secondary Devices (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Packages (AREA)
  • Cartons (AREA)
  • Tents Or Canopies (AREA)
  • Handcart (AREA)
  • Photovoltaic Devices (AREA)

Abstract

Each element (A1, A2, A3, A4 ... An) in a stack of elements is connected to the adjacent element by two crossways-running hinge joints (G12, H12; G23; G34, H34 ...) in such a way that, between each two elements, two axes of rotation (e1 or c2 and f1 or d2; e2 or c3 and f2 or d3; ...) are defined along opposite edges of the elements. Each element can thus be turned optionally with respect to the neighbouring element about either one of the two mutually opposite axes of rotation so that the stack can be unfolded in two alternative ways.
AU11770/92A 1991-01-21 1992-01-20 Device for unfolding a stack of elements Abandoned AU1177092A (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE4101637 1991-01-21
DE19914101637 DE4101637A1 (en) 1991-01-21 1991-01-21 Flap device for parallel components arranged in sequence - allows them to be folded together accordion-fashion i.e. joined by strips on flap link
DE19914125704 DE4125704A1 (en) 1991-08-02 1991-08-02 Component stack unfolding mechanism
DE4125704 1991-08-02

Publications (1)

Publication Number Publication Date
AU1177092A true AU1177092A (en) 1992-08-27

Family

ID=25900389

Family Applications (1)

Application Number Title Priority Date Filing Date
AU11770/92A Abandoned AU1177092A (en) 1991-01-21 1992-01-20 Device for unfolding a stack of elements

Country Status (6)

Country Link
EP (1) EP0521124B1 (en)
AT (1) ATE122631T1 (en)
AU (1) AU1177092A (en)
DE (1) DE59202202D1 (en)
ES (1) ES2075678T3 (en)
WO (1) WO1992012898A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113562198B (en) * 2021-08-26 2023-04-07 哈尔滨工业大学 Hinge mechanism, solar sailboard and micro-nano satellite

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2310711A (en) * 1942-10-14 1943-02-09 Edward S Savage Mystery toy
DE1285337B (en) * 1965-10-26 1968-12-12 Boelkow Gmbh Drum-shaped, especially spin-stabilized satellite
FR2354925A1 (en) * 1976-06-18 1978-01-13 Aerospatiale SYNCHRONIZING MECHANISM FOR THE DEPLOYMENT OF CARRIER ELEMENTS OF SOLAR CELLS
DE3907063A1 (en) * 1989-03-04 1990-09-13 Messerschmitt Boelkow Blohm SOLAR GENERATOR ARRANGEMENT FOR PARTIAL AND FULL DEVELOPMENT

Also Published As

Publication number Publication date
ATE122631T1 (en) 1995-06-15
EP0521124A1 (en) 1993-01-07
ES2075678T3 (en) 1995-10-01
EP0521124B1 (en) 1995-05-17
WO1992012898A1 (en) 1992-08-06
DE59202202D1 (en) 1995-06-22

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