AU1177092A - Device for unfolding a stack of elements - Google Patents
Device for unfolding a stack of elementsInfo
- 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
Links
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
- 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
- B64G1/222—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
- B64G1/2226—Telescoping
-
- 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
- B64G1/2228—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 hold-down or release mechanisms
-
- 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
- B64G1/2229—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 deployment actuating mechanism
-
- 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
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements 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)
- Photovoltaic Devices (AREA)
- Handcart (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.
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 |
DE4125704 | 1991-08-02 | ||
DE19914125704 DE4125704A1 (en) | 1991-08-02 | 1991-08-02 | Component stack unfolding mechanism |
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)
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)
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 |
-
1992
- 1992-01-20 WO PCT/DE1992/000032 patent/WO1992012898A1/en active IP Right Grant
- 1992-01-20 AT AT92902934T patent/ATE122631T1/en not_active IP Right Cessation
- 1992-01-20 EP EP92902934A patent/EP0521124B1/en not_active Expired - Lifetime
- 1992-01-20 AU AU11770/92A patent/AU1177092A/en not_active Abandoned
- 1992-01-20 DE DE59202202T patent/DE59202202D1/en not_active Expired - Fee Related
- 1992-01-20 ES ES92902934T patent/ES2075678T3/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0521124A1 (en) | 1993-01-07 |
DE59202202D1 (en) | 1995-06-22 |
EP0521124B1 (en) | 1995-05-17 |
ATE122631T1 (en) | 1995-06-15 |
ES2075678T3 (en) | 1995-10-01 |
WO1992012898A1 (en) | 1992-08-06 |
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