ES3076138T3 - High-length redundant thermal-control device with complex two-phase structures, assembly method and manufacturing method - Google Patents

High-length redundant thermal-control device with complex two-phase structures, assembly method and manufacturing method

Info

Publication number
ES3076138T3
ES3076138T3 ES24758785T ES24758785T ES3076138T3 ES 3076138 T3 ES3076138 T3 ES 3076138T3 ES 24758785 T ES24758785 T ES 24758785T ES 24758785 T ES24758785 T ES 24758785T ES 3076138 T3 ES3076138 T3 ES 3076138T3
Authority
ES
Spain
Prior art keywords
complex
manufacturing
control device
phase structures
assembly method
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
ES24758785T
Other languages
English (en)
Inventor
Matthieu Martinelli
Laura Fourgeaud
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.)
Airbus Defence and Space SAS
Original Assignee
Airbus Defence and Space SAS
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 Airbus Defence and Space SAS filed Critical Airbus Defence and Space SAS
Application granted granted Critical
Publication of ES3076138T3 publication Critical patent/ES3076138T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00—Products made by additive manufacturing
    • 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
    • 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
    • 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
    • F28D15/04—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 with tubes having a capillary structure
    • F28D15/046—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 with tubes having a capillary structure characterised by the material or the construction of the capillary structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00—Fastening; Joining
    • F28F2275/06—Fastening; Joining by welding

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sustainable Development (AREA)
  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Environmental Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Control Of Temperature (AREA)
ES24758785T 2023-08-24 2024-08-20 High-length redundant thermal-control device with complex two-phase structures, assembly method and manufacturing method Active ES3076138T3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2308825A FR3152311B1 (fr) 2023-08-24 2023-08-24 Dispositif de contrôlr thermique redondant de grande longueur à structures diphasiques complexes, procédé d'assemblage et procédé de fabrication
PCT/EP2024/073334 WO2025040672A1 (fr) 2023-08-24 2024-08-20 Dispositif de contrôle thermique redondant de grande longueur à structures diphasiques complexes, procédé d'assemblage et procédé de fabrication

Publications (1)

Publication Number Publication Date
ES3076138T3 true ES3076138T3 (en) 2026-08-12

Family

ID=88838869

Family Applications (1)

Application Number Title Priority Date Filing Date
ES24758785T Active ES3076138T3 (en) 2023-08-24 2024-08-20 High-length redundant thermal-control device with complex two-phase structures, assembly method and manufacturing method

Country Status (4)

Country Link
EP (1) EP4701932B1 (es)
ES (1) ES3076138T3 (es)
FR (1) FR3152311B1 (es)
WO (1) WO2025040672A1 (es)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5649310A (en) * 1994-06-15 1997-07-15 Space Systems/Loral, Inc. Signal translation and amplification system including a thermal radiation panel coupled thereto
JPH0853100A (ja) * 1994-08-10 1996-02-27 Mitsubishi Electric Corp ヒートパイプ埋め込みハニカムサンドイッチパネル
DE19908683C2 (de) 1999-02-26 2001-03-01 Dornier Gmbh Radiatorstruktur eines Satelliten
US10837712B1 (en) * 2015-04-15 2020-11-17 Advanced Cooling Technologies, Inc. Multi-bore constant conductance heat pipe for high heat flux and thermal storage

Also Published As

Publication number Publication date
EP4701932A1 (fr) 2026-03-04
EP4701932C0 (fr) 2026-05-13
FR3152311A1 (fr) 2025-02-28
FR3152311B1 (fr) 2025-08-15
EP4701932B1 (fr) 2026-05-13
WO2025040672A1 (fr) 2025-02-27