JP7386032B2 - 断面が一定でない、テープスプリング展開可能なデバイス - Google Patents
断面が一定でない、テープスプリング展開可能なデバイス Download PDFInfo
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- JP7386032B2 JP7386032B2 JP2019183467A JP2019183467A JP7386032B2 JP 7386032 B2 JP7386032 B2 JP 7386032B2 JP 2019183467 A JP2019183467 A JP 2019183467A JP 2019183467 A JP2019183467 A JP 2019183467A JP 7386032 B2 JP7386032 B2 JP 7386032B2
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- tape spring
- axis
- deployable device
- along
- tape
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- 230000002787 reinforcement Effects 0.000 claims description 12
- 230000007423 decrease Effects 0.000 claims description 6
- 230000003247 decreasing effect Effects 0.000 claims description 2
- 238000005457 optimization Methods 0.000 description 5
- 238000004804 winding Methods 0.000 description 5
- 239000000835 fiber Substances 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000739 chaotic effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
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- 230000003014 reinforcing effect Effects 0.000 description 1
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- 238000004513 sizing Methods 0.000 description 1
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Images
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
- 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
- B64G1/2225—Rolling or unfurling
-
- 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
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tape Measures (AREA)
- Springs (AREA)
- Aerials With Secondary Devices (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
Description
2 テープスプリング
3 幅
4 心棒
10 展開可能なデバイス
11 テープスプリング
13 第1の特性寸法
14 第2の特性寸法
16 自由端部
17 点線
20 展開可能なデバイス
21 テープスプリング
22 端部
23 第1の部分
24 第2の部分
25 点線
31 テープスプリング
32 局所的な補強
41 テープスプリング
42 局所的な補強
60 衛星
X 第2の軸
Y 第3の軸
Z 第1の軸
Claims (5)
- 展開可能なデバイス(10、20)であって、第1の軸Zを中心に巻回された構成から、前記第1の軸Zに実質的に垂直な第2の軸Xに沿って、展開された構成に移ることができるテープスプリング(11、21、31、41)であって、2つの特性寸法、すなわち、前記第1の軸Zに沿った前記テープスプリング(11、21、31、41)の幅(13)である第1の特性寸法、前記第1の軸Z、及び前記第2の軸Xに実質的に垂直な第3の軸Yに沿った前記テープスプリング(11、21、31、41)の厚さ(14)である第2の特性寸法、を有する前記テープスプリング(11、21、31、41)を備え、
前記2つの特性寸法のうちの少なくとも1つが、前記第2の軸Xに沿って不定値を有する展開可能なデバイスにおいて、
前記テープスプリング(21)は、第1の端部及び第2の端部を有し、テープスプリングの第1の端部は、第1の軸Zを中心に巻回されており、テープスプリングの第2の端部は、埋め込まれた端部であり、及び、前記2つの特性寸法のうちの前記少なくとも1つが、前記第2の軸Xに沿って、前記テープスプリング(21)の第1の部分(23)にわたって増加、及び減少し、且つ、前記埋め込まれた端部(22)に向かって前記テープスプリング(21)の第2の部分(24)にわたって増加する不定値を有することを特徴とする、展開可能なデバイス。 - 前記テープスプリング(11)が自由端部を有すること、及び、前記2つの特性寸法のうちの前記少なくとも1つが、前記第2の軸Xに沿って、前記自由端部に向かって減少する不定値を有することを特徴とする、請求項1に記載の展開可能なデバイス(10)。
- 前記テープスプリング(31、41)に位置決めされた、少なくとも部分的に前記第1の軸Zに沿って延在し、且つ/又は、優先的に少なくとも部分的に前記第2の軸Xに沿って延在する少なくとも1つの局所的な補強(32、42)を含むことを特徴とする、請求項1又は2に記載の展開可能なデバイス(10、20)。
- 前記テープスプリング(11、21、31、41)のYZ平面を通る断面が、展開された構成において、円筒形状の、U字形の、又は、大文字の「オメガ文字」形の断面であることを特徴とする、請求項1~3のいずれか一項に記載の展開可能なデバイス(10、20)。
- 少なくとも1つの、請求項1~4のいずれか一項に記載の展開可能なデバイス(10、20)を備えることを特徴とする衛星(60)。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1801096A FR3087426B1 (fr) | 2018-10-18 | 2018-10-18 | Dispositif deployable a metre-ruban a section non constante |
FR1801096 | 2018-10-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2020063034A JP2020063034A (ja) | 2020-04-23 |
JP7386032B2 true JP7386032B2 (ja) | 2023-11-24 |
Family
ID=65443884
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2019183467A Active JP7386032B2 (ja) | 2018-10-18 | 2019-10-04 | 断面が一定でない、テープスプリング展開可能なデバイス |
Country Status (7)
Country | Link |
---|---|
US (1) | US11597538B2 (ja) |
EP (1) | EP3640147B1 (ja) |
JP (1) | JP7386032B2 (ja) |
CN (1) | CN111071485B (ja) |
CA (1) | CA3058738A1 (ja) |
ES (1) | ES2877127T3 (ja) |
FR (1) | FR3087426B1 (ja) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022159476A1 (en) * | 2021-01-21 | 2022-07-28 | Apex Brands, Inc. | Roll-over resistant measuring tape |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3528543A (en) | 1968-08-27 | 1970-09-15 | Eli I Robinsky | Corrugated roll-up structure |
US4991784A (en) | 1987-12-07 | 1991-02-12 | Schmid Hans A | Apparatus for guiding a curved strip |
JP2000138392A (ja) | 1998-10-15 | 2000-05-16 | Space Syst Loral Inc | 階段状テ―パを備えたソ―ラパネルアレイ |
WO2018087538A1 (en) | 2016-11-08 | 2018-05-17 | Oxford Space Systems | Deployable mast structure |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5749121Y2 (ja) * | 1978-03-29 | 1982-10-27 | ||
FR2969984B1 (fr) * | 2010-12-30 | 2013-02-08 | Thales Sa | Générateur solaire deroulable caissonne |
GB2491822B (en) * | 2011-06-09 | 2015-12-02 | Rtl Materials Ltd | Coilable extendible member and methods |
US9352528B1 (en) * | 2014-04-02 | 2016-05-31 | Todd D. Brooks | Self-supporting collapsible and retractable elongate member and method of retracting |
FR3024227B1 (fr) * | 2014-07-25 | 2018-02-09 | Thales | Procede d'encastrement escamotable de metre-ruban pour une structure deployable et structure deployable a metre-ruban |
FR3025498B1 (fr) * | 2014-09-05 | 2017-12-08 | Thales Sa | Mat deployable a deploiement spontane autonome et satellite comportant au moins un tel mat |
FR3028842A1 (fr) * | 2014-11-21 | 2016-05-27 | Thales Sa | Structure deployable escamotable a metre-ruban |
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 |
CN105370713A (zh) * | 2015-11-20 | 2016-03-02 | 北京卫星制造厂 | 一种微小卫星展开机构 |
JP6525272B2 (ja) * | 2016-07-01 | 2019-06-05 | サカセ・アドテック株式会社 | ブーム |
US10611502B2 (en) * | 2016-10-20 | 2020-04-07 | Roccor, Llc | Precision deployment devices, systems, and methods |
CN106864772B (zh) * | 2017-01-24 | 2021-06-01 | 航天东方红卫星有限公司 | 航天器预应力薄壁锥形多杆平行并联式空间展开机构 |
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2018
- 2018-10-18 FR FR1801096A patent/FR3087426B1/fr not_active Expired - Fee Related
-
2019
- 2019-10-04 JP JP2019183467A patent/JP7386032B2/ja active Active
- 2019-10-14 EP EP19203042.7A patent/EP3640147B1/fr active Active
- 2019-10-14 ES ES19203042T patent/ES2877127T3/es active Active
- 2019-10-15 CA CA3058738A patent/CA3058738A1/en active Pending
- 2019-10-16 US US16/655,139 patent/US11597538B2/en active Active
- 2019-10-17 CN CN201910987449.4A patent/CN111071485B/zh active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3528543A (en) | 1968-08-27 | 1970-09-15 | Eli I Robinsky | Corrugated roll-up structure |
US4991784A (en) | 1987-12-07 | 1991-02-12 | Schmid Hans A | Apparatus for guiding a curved strip |
JP2000138392A (ja) | 1998-10-15 | 2000-05-16 | Space Syst Loral Inc | 階段状テ―パを備えたソ―ラパネルアレイ |
WO2018087538A1 (en) | 2016-11-08 | 2018-05-17 | Oxford Space Systems | Deployable mast structure |
Also Published As
Publication number | Publication date |
---|---|
US20200122862A1 (en) | 2020-04-23 |
EP3640147B1 (fr) | 2021-05-05 |
CN111071485B (zh) | 2024-07-26 |
ES2877127T3 (es) | 2021-11-16 |
EP3640147A1 (fr) | 2020-04-22 |
CA3058738A1 (en) | 2020-04-18 |
JP2020063034A (ja) | 2020-04-23 |
US11597538B2 (en) | 2023-03-07 |
FR3087426A1 (fr) | 2020-04-24 |
FR3087426B1 (fr) | 2022-03-11 |
CN111071485A (zh) | 2020-04-28 |
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