公开(公告)号：WO1985002901A1

公开(公告)日：1985-07-04

申请号：PCT/US1984002027

申请日：1984-12-07

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  BASIULIS, Algerd

IPC: F28D15/02

CPC classification number: F28D15/0233

Abstract: A heat pipe (10) has a large area vapor tube for radiant heat loss and has connected thereto a subcooled liquid return tube (14) for a return of the condensed liquid to the evaporator portion of the vapor tube. Wicking material plugs (28, 30) return the liquid and provide equilibrium along the length of the system. The separate return of the liquid through liquid tube (14) permits a long heat pipe which may have several thermal connections.

公开(公告)号：WO1989011071A1

公开(公告)日：1989-11-16

申请号：PCT/US1989001138

申请日：1989-03-21

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  BASIULIS, Algerd

IPC: F25B15/14

CPC classification number: F25B15/14 ,  Y02A30/277 ,  Y02B30/62

Abstract: A thermal engine is disclosed which is operable as a heat pump, refrigerator, or air conditioner. Vaporized working fluid from a first evaporator, which extracts heat from elements desired to be cooled, is fed to a first region of an osmotic pump which also has a second region containing a solution of the working fluid and a preselected solute, the second region being separated from the first region by a membrane permeable to the vaporized working fluid but not to the solute. A second evaporator, which may be driven by waste heat, is operatively coupled to the second region of the osmotic pump by means of a counterflow heat exchanger having a first path for conveying relatively dilute solution from the second region of the osmotic pump to the second evaporator and a second path for conveying relatively concentrated solution from the second evaporator to the second region of the osmotic pump. Output heat from the thermal engine is obtained from a condenser which condenses vaporized working fluid from the second evaporator. The condensed working fluid undergoes constant enthalpy expansion, after which it is returned to the first evaporator.

公开(公告)号：WO1983003945A1

公开(公告)日：1983-11-10

申请号：PCT/US1983000626

申请日：1983-04-27

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  BASIULIS, Algerd

IPC: H05K07/20

CPC classification number: H05K7/20336 ,  F28D15/0233 ,  F28D15/04 ,  G12B15/02

Abstract: A heat pipe cooling module assembly (20) for cooling electronic components (28) includes a plurality of heat pipe modules (22) comprising condenser and evaporator sections (24, 26) and working fluid therein. In a preferred embodiment, each evaporator section comprises a sandwich construction of a pair of flat outer plates (34), a pair of wick pads (36) and a separator plate (38) comprising channels extending from the evaporator section into the condenser section.

Abstract translation: 用于冷却电子部件（28）的热管冷却模块组件（20）包括多个热管模块（22），其包括冷凝器和蒸发器部分（24,26）以及其中的工作流体。 在一个优选实施例中，每个蒸发器部分包括一对平坦外板（34），一对芯焊盘（36）和分隔板（38）的夹层结构，该隔板包括从蒸发器部分延伸到冷凝器部分的通道。

公开(公告)号：EP0107706A1

公开(公告)日：1984-05-09

申请号：EP83901685.0

申请日：1983-04-27

Applicant: Hughes Aircraft Company

Inventor： BASIULIS, Algerd

IPC: F28D15 ,  G12B15 ,  H05K7

CPC classification number: H05K7/20336 ,  F28D15/0233 ,  F28D15/04 ,  G12B15/02

Abstract: Un assemblage de modules de refroidissement par tubes de dissipation de chaleur (20) pour refroidir des composants électroniques (28) comprend une pluralité de modules à tubes de dissipation de chaleur (22) comprenant des sections à condenseur et évaporateur (24, 26) et un fluide de travail à l'intérieur. Dans un mode préférentiel de réalisation, chaque section d'évaporateur comprend une construction en sandwich d'une paire de plaques externes plates (34), une paire de tampons amortisseurs en forme de mèches (36) et une plaque de séparation (38) comprenant des canaux s'étendant depuis la section d'évaporation dans la section de condensation.

Abstract translation: 用于冷却电子部件（28）的热管冷却模块组件（20）包括多个热管模块（22），其包括冷凝器和蒸发器部分（24,26）以及其中的工作流体。 在一个优选实施例中，每个蒸发器部分包括一对平坦的外板（34），一对芯焊盘（36）和分隔板（38）的夹层结构，该隔板包括从蒸发器部分延伸到冷凝器部分的通道。

公开(公告)号：EP0107706B1

公开(公告)日：1987-08-05

申请号：EP83901685.4

申请日：1983-04-27

Applicant: Hughes Aircraft Company

Inventor： BASIULIS, Algerd

IPC: H05K7/20 ,  G12B15/02

CPC classification number: H05K7/20336 ,  F28D15/0233 ,  F28D15/04 ,  G12B15/02

Abstract: A heat pipe cooling module assembly (20) for cooling electronic components (28) includes a plurality of heat pipe modules (22) comprising condenser and evaporator sections (24, 26) and working fluid therein. In a preferred embodiment, each evaporator section comprises a sandwich construction of a pair of flat outer plates (34), a pair of wick pads (36) and a separator plate (38) comprising channels extending from the evaporator section into the condenser section.

Abstract translation: 用于冷却电子部件（28）的热管冷却模块组件（20）包括多个热管模块（22），其包括冷凝器和蒸发器部分（24,26）以及其中的工作流体。 在一个优选实施例中，每个蒸发器部分包括一对平坦的外板（34），一对芯焊盘（36）和分隔板（38）的夹层结构，该隔板包括从蒸发器部分延伸到冷凝器部分的通道。

公开(公告)号：EP0165974A1

公开(公告)日：1986-01-02

申请号：EP85900401.0

申请日：1984-12-07

Applicant: Hughes Aircraft Company

Inventor： BASIULIS, Algerd

IPC: F28D15

CPC classification number: F28D15/0233

Abstract: Un tuyau thermique (10) possède un tube de vapeur de grande superficie pour une perte de chaleur rayonnante et est connecté à un tube de retour de liquide sous-refroidi (14) destiné à retourner le liquide condensé dans la partie d'évaporation du tube de vapeur. Des bouchons de matériau de mèche (28, 30) retournent le liquide et permettent l'équilibre sur toute la longueur du système. Le retour séparé du liquide par le tube de liquide (14) permet d'avoir un long tuyau thermique pouvant comporter plusieurs connexions thermiques.

公开(公告)号：EP0366776A1

公开(公告)日：1990-05-09

申请号：EP89905984.0

申请日：1989-03-21

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： BASIULIS, Algerd

IPC: F25B15

CPC classification number: F25B15/14 ,  Y02A30/277 ,  Y02B30/62

Abstract: A thermal engine is disclosed which is operable as a heat pump, refrigerator, or air conditioner. Vaporized working fluid from a first evaporator, which extracts heat from elements desired to be cooled, is fed to a first region of an osmotic pump which also has a second region containing a solution of the working fluid and a preselected solute, the second region being separated from the first region by a membrane permeable to the vaporized working fluid but not to the solute. A second evaporator, which may be driven by waste heat, is operatively coupled to the second region of the osmotic pump by means of a counterflow heat exchanger having a first path for conveying relatively dilute solution from the second region of the osmotic pump to the second evaporator and a second path for conveying relatively concentrated solution from the second evaporator to the second region of the osmotic pump. Output heat from the thermal engine is obtained from a condenser which condenses vaporized working fluid from the second evaporator. The condensed working fluid undergoes constant enthalpy expansion, after which it is returned to the first evaporator.

公开(公告)号：EP0165974B1

公开(公告)日：1988-06-01

申请号：EP85900401.2

申请日：1984-12-07

Applicant: Hughes Aircraft Company

Inventor： BASIULIS, Algerd

IPC: F28D15/02

CPC classification number: F28D15/0233

Abstract: A heat pipe (10) has a large area vapor tube for radiant heat loss and has connected thereto a subcooled liquid return tube (14) for a return of the condensed liquid to the evaporator portion of the vapor tube. Wicking material plugs (28, 30) return the liquid and provide equilibrium along the length of the system. The separate return of the liquid through liquid tube (14) permits a long heat pipe which may have several thermal connections.