JP2018511522A - 結合された補強材/ヒートパイプを有する人工衛星放熱パネル - Google Patents
結合された補強材/ヒートパイプを有する人工衛星放熱パネル Download PDFInfo
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- JP2018511522A JP2018511522A JP2017551262A JP2017551262A JP2018511522A JP 2018511522 A JP2018511522 A JP 2018511522A JP 2017551262 A JP2017551262 A JP 2017551262A JP 2017551262 A JP2017551262 A JP 2017551262A JP 2018511522 A JP2018511522 A JP 2018511522A
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- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 7
- 239000012530 fluid Substances 0.000 description 7
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- 239000004593 Epoxy Substances 0.000 description 2
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- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- 239000012790 adhesive layer Substances 0.000 description 1
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- 230000005611 electricity Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- QQONPFPTGQHPMA-UHFFFAOYSA-N propylene Natural products CC=C QQONPFPTGQHPMA-UHFFFAOYSA-N 0.000 description 1
- 125000004805 propylene group Chemical group [H]C([H])([H])C([H])([*:1])C([H])([H])[*:2] 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
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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
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
- B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
- B64G1/503—Radiator panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
-
- 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
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
- B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
- B64G1/506—Heat pipes
-
- 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
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
- F28D15/0233—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes the conduits having a particular shape, e.g. non-circular cross-section, annular
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
- F28D15/0275—Arrangements for coupling heat-pipes together or with other structures, e.g. with base blocks; Heat pipe cores
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/14—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally
- F28F1/16—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally the means being integral with the element, e.g. formed by extrusion
-
- 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
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- 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
- B64G1/40—Arrangements or adaptations of propulsion systems
-
- 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
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
-
- 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
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
- B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
- F28F2013/005—Thermal joints
- F28F2013/006—Heat conductive materials
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Thermal Sciences (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Environmental & Geological Engineering (AREA)
- Toxicology (AREA)
- Environmental Sciences (AREA)
- Biodiversity & Conservation Biology (AREA)
- Sustainable Development (AREA)
- Critical Care (AREA)
- Geometry (AREA)
- Emergency Medicine (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
Description
・(取得データ):要求されたデータは、ゲートウェイステーションでインターネットから取得される。
・(アップリンク):データ信号は、大型の地上ベースのアンテナを介して人工衛星のゲートウェイアンテナ160に送信される(Kaバンド)。
・(ペイロード):データ信号が増幅され、ダウンリンク(Ku)バンドへの変換のために変換モジュール110に送られ、次に再び増幅される。
・ペイロード信号は、ペイロードアンテナ124に送られる。
・(ダウンリンク):アンテナ124は、増幅され周波数変換された信号をユーザ端末に送信する。
ユーザが電子メールなどのデータを(要求ではなく)送信する場合、信号は、逆方向だが同じ経路を辿る。
(i)直線状ではない(湾曲しているなど)、または
(ii)直線状であるが、放熱パネルの表面上で互いに平行ではない、または
(iii)直線状でなく、放熱パネルの表面上で互いに平行でない。
102 統合ペイロードモジュール
104,106,108,112,126 パネル
109 ブレース
110 変換モジュール
114 推進モジュール
116 燃料タンク
118 推進制御システム
120 支持ウェブ
122 ペイロードアンテナモジュール
124 ペイロードアンテナ
128 バッテリーモジュール
130 パネル
132 バスコンポーネントモジュール
134 メインソーラーアレイモーター
136 リアクションホイール
138 駆動モーター
140 ソーラーアレイシステム
142A,142B ソーラーパネル
144 モーター
146 受動回転ベアリング
148A,148B yバー
150 部材
152 開口部
154 ロック・リリース部材
156 開口部
158 無指向性アンテナ
160 ゲートウェイアンテナ
162 可動マウント
164 メイン制御プロセッサ
300,400,500,600,700,800 受動的熱システム
370 未改変ヒートパイプ
372 ボア
374 本体
376 フランジ
470,570,670,770,870 構造ヒートパイプ
480 直線垂直フィン
580 L字型フィン
680 二重フィン
780 水平プレート
880 垂直フィン
882 水平プレート
Claims (16)
- 人工衛星に収容された電子機器によって生成された熱を外部環境へ放射するための複数の中実の放熱パネルを有する人工衛星であって、前記人工衛星は、受動的熱システムを含み、前記受動的熱システムは、
前記中実の放熱パネルの少なくとも1つと、
前記少なくとも1つの放熱パネルに配置された複数のヒートパイプと、
を備え、前記放熱パネルの表面には他の構造的な補強材が配置されていない、人工衛星。 - 受動的熱システムを備える装置であって、前記受動的熱システムは、
中実の放熱パネルと、
前記中実の放熱パネルの表面に配置された少なくとも1つの構造ヒートパイプと、
を備える、装置。 - 前記構造ヒートパイプが、前記中実の放熱パネルから離れるように、前記構造ヒートパイプの本体の上部に近い位置から延在する2つ以内の直線フィンを有する、請求項2に記載の装置。
- 前記構造ヒートパイプが、1つ以内の直線フィンを有する、請求項3に記載の装置。
- 2つの前記フィンが共同してv字形を形成する、請求項3に記載の装置。
- 前記構造ヒートパイプがL字形部材を備え、前記L字形部材は、前記中実の放熱パネルから離れるように、前記構造ヒートパイプの本体の上部に近い位置から延在する第1部分を有する、請求項2に記載の装置。
- 前記L字形部材の前記第1部分が前記中実の放熱パネルに対して直交して配向される、請求項6に記載の装置。
- 前記L字形部材の第2部分が前記中実の放熱パネルに対して平行に配向される、請求項6に記載の装置。
- 前記構造ヒートパイプがt字形部材を備え、前記t字形部材は、前記中実の放熱パネルから離れるように、前記構造ヒートパイプの本体の上部に近い位置から延在する第1部分を有する、請求項2に記載の装置。
- 前記t字形部材の前記第1部分が前記中実の放熱パネルに対して直交して配向される、請求項9に記載の装置。
- 前記t字形部材の第2部分が前記中実の放熱パネルに対して平行に配向される、請求項9に記載の装置。
- 前記装置が人工衛星である、請求項2に記載の装置。
- 少なくとも2つの構造ヒートパイプが前記放熱パネルの表面に配置され、前記少なくとも2つの構造ヒートパイプが互いに対して平行ではない、請求項2に記載の装置。
- 前記少なくとも1つの構造ヒートパイプが直線ではない、請求項2に記載の装置。
- 複数の中実の放熱パネルを備える人工衛星であって、前記放熱パネルの少なくとも1つは、1または複数の構造ヒートパイプが前記中実の放熱パネルの表面に配置されている受動的熱システムとして構成されている、人工衛星。
- 前記放熱パネルの少なくとも2つは、1または複数の構造ヒートパイプが前記少なくとも2つの放熱パネルのそれぞれに配置されている受動的熱システムとして構成されている、請求項15に記載の人工衛星。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/673,215 US10392135B2 (en) | 2015-03-30 | 2015-03-30 | Satellite radiator panels with combined stiffener/heat pipe |
US14/673,215 | 2015-03-30 | ||
PCT/US2016/024916 WO2016160924A1 (en) | 2015-03-30 | 2016-03-30 | Satellite radiator panels with combined stiffener/heat pipe |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2018511522A true JP2018511522A (ja) | 2018-04-26 |
JP6763875B2 JP6763875B2 (ja) | 2020-09-30 |
Family
ID=57007537
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2017551262A Expired - Fee Related JP6763875B2 (ja) | 2015-03-30 | 2016-03-30 | 結合された補強材/ヒートパイプを有する人工衛星放熱パネル |
Country Status (10)
Country | Link |
---|---|
US (1) | US10392135B2 (ja) |
EP (1) | EP3277587B1 (ja) |
JP (1) | JP6763875B2 (ja) |
KR (1) | KR102124242B1 (ja) |
CN (1) | CN107848635B (ja) |
CA (1) | CA2981169C (ja) |
ES (1) | ES2878080T3 (ja) |
IL (1) | IL254741B (ja) |
SG (1) | SG11201708018RA (ja) |
WO (1) | WO2016160924A1 (ja) |
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FR3030458B1 (fr) * | 2014-12-18 | 2017-01-27 | Airbus Defence & Space Sas | Engin spatial |
US9745083B2 (en) * | 2015-04-01 | 2017-08-29 | Worldvu Satellites Limited | Method for thermal stabilization of a communications satellite |
FR3052443B1 (fr) * | 2016-06-10 | 2018-07-06 | Airbus Defence And Space Sas | Engin spatial |
CN106455450B (zh) * | 2016-11-22 | 2019-01-25 | 上海卫星工程研究所 | 星用热管的高等温性轻量化应用方法 |
US10780998B1 (en) * | 2017-03-22 | 2020-09-22 | Space Systems/Loral, Llc | Spacecraft design with multiple thermal zones |
CN107985630A (zh) * | 2017-11-02 | 2018-05-04 | 银河航天(北京)科技有限公司 | 一种多功能结构板 |
FR3089957B1 (fr) * | 2018-12-18 | 2020-12-18 | Airbus Defence & Space Sas | Procédé de fixation d’un équipement dissipatif, mur de véhicule spatial et véhicule spatial |
CN109606745B (zh) * | 2019-01-09 | 2021-10-26 | 中国科学院长春光学精密机械与物理研究所 | 一种空间热管辐射器 |
US11794927B2 (en) | 2019-08-28 | 2023-10-24 | The Boeing Company | Additively manufactured spacecraft panel |
US11802606B2 (en) | 2020-05-18 | 2023-10-31 | The Boeing Company | Planate dynamic isolator |
US11827389B2 (en) * | 2020-05-18 | 2023-11-28 | The Boeing Company | Additively manufactured satellite |
US11542041B2 (en) * | 2020-05-18 | 2023-01-03 | The Boeing Company | Additively manufactured satellite panel with damping |
US11909110B2 (en) * | 2020-09-30 | 2024-02-20 | The Boeing Company | Additively manufactured mesh horn antenna |
AU2021273575A1 (en) | 2020-12-17 | 2022-07-07 | The Boeing Company | Satellite thermal enclosure |
US12024318B1 (en) * | 2021-09-03 | 2024-07-02 | Blue Origin, Llc | Heat fins for heat dissipation of rocket components |
US11930622B2 (en) | 2022-01-07 | 2024-03-12 | Dell Products Lp | System and method for a 5G cooling module that directs heat into a thermal loop associated with a processing device |
US20230322419A1 (en) * | 2022-04-11 | 2023-10-12 | Maxar Space Llc | Radiating coupling heat pipe |
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EP3277587A4 (en) | 2018-09-05 |
KR102124242B1 (ko) | 2020-06-17 |
US20160288926A1 (en) | 2016-10-06 |
US10392135B2 (en) | 2019-08-27 |
IL254741B (en) | 2022-05-01 |
KR20170134537A (ko) | 2017-12-06 |
CN107848635B (zh) | 2021-02-26 |
ES2878080T3 (es) | 2021-11-18 |
SG11201708018RA (en) | 2017-10-30 |
CA2981169A1 (en) | 2016-10-06 |
EP3277587A1 (en) | 2018-02-07 |
EP3277587B1 (en) | 2021-06-16 |
JP6763875B2 (ja) | 2020-09-30 |
CA2981169C (en) | 2020-12-29 |
IL254741A0 (en) | 2017-11-30 |
CN107848635A (zh) | 2018-03-27 |
WO2016160924A1 (en) | 2016-10-06 |
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