IP Library Granted Patent US 8,166,774
Granted Patent B2
US 8,166,774 · App. 11/656,799 · Granted May 1, 2012

Heat exchanger with an expansion stage

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Quick Facts
Patent No.
US 8,166,774
App. No.
11/656,799
Granted
May 1, 2012
Kind
B2
Abstract

In a heat exchanger unit for conditioning a first fluid, particularly a refrigerant in an air conditioning system, including a heat exchanger, the heat exchanger includes first and second tube element units for heat exchange between a first fluid flowing through the tube elements and a second fluid flowing over the tube elements, wherein the first fluid is supplied first to the first tube element unit so as to flow upwardly therethrough and via an intermediate outlet connector to a compressor stage from where it is transferred to the top of the second tube element unit which is disposed above the first tube element unit and flows downwardly through the second tube element unit to an expansion stage wherein the energy released during expansion in the expansion stage is utilized for the compression of the first fluid in the compressor stage.

Claims (5)

1. A heat transfer system including a first fluid-air heat exchanger unit ( 3 ) with a first tube element ( 3 a ) and a second tube element ( 3 b ) connected in series with the first tube element ( 3 a ), a main compressor (K) connected to the first tube element ( 3 a ) for compressing a refrigerant supplied to the first tube element ( 3 a ) to system operating pressure and thereby increasing its temperature to an operating temperature at which the refrigerant is supplied to said first tube element ( 3 a ), a compressor-expansion stage unit ( 2 ) arranged between the first and second tube elements ( 3 a , 3 b ) and including a compression stage ( 14 ) connected to the first tube element ( 3 a ) for re-compressing the refrigerant from the first tube element ( 3 a ) in which the refrigerant has been cooled and lost pressure, before the refrigerant re-pressurized and reheated is supplied to the second tube element ( 3 b ), and an expansion stage ( 15 ) connected to the second tube element ( 3 b ) for receiving the refrigerant which has been cooled in the second tube unit ( 3 b ) and decompressing it to a low system pressure while recuperating expansion energy therefrom, the expansion stage ( 15 ) being operatively connected to the compression stage ( 14 ) for transferring the energy recuperated in the expansion stage ( 15 ) to the compression stage ( 14 ) for operating the compression stage and for efficient cooling of the refrigerant, the expansion stage ( 15 ) being connected to a second heat exchanger unit (W 2 ) in which the refrigerant is heated again before being supplied directly, that is without intermediate heat exchanger to the main compressor (K), the compression stage ( 14 ) and the expansion stage ( 15 ) being arranged in a common housing ( 16 ) including a compression stage wheel arrangement ( 14 a , 14 b ) and an expansion stage wheel arrangement ( 15 a , 15 b ) and an insulating separation wall ( 21 ) slidably supported in the housing ( 16 ) between the compression stage wheel arrangement ( 14 a , 14 b ) and the expansion stage wheel arrangement ( 15 a , 15 b ) and in contact with the compressor and expansion stage wheel arrangements ( 14 a , 14 b ; 15 a , 15 b ); wherein the compression stage ( 14 ) and the expansion stage ( 15 ) bare a common shaft ( 17 ) carrying a compression stage wheel ( 14 a ) and an expansion stage wheel ( 15 a ), and one of the compression stage wheel ( 14 a ) and the expansion stage wheel ( 15 a ) is axially slidably supported on the common shaft ( 17 ); and a support element ( 23 ) provided axially in contact with the shaft ( 17 ) and the compressor wheels ( 14 a 14 b ) by a compression spring ( 25 ) disposed between the support element ( 23 ) and the housing lid ( 16 d ) supported in the housing ( 16 ) and biased toward the compression stage wheel ( 14 a , 14 b ).

2. The heat transfer system unit as claimed in claim 1 , wherein the compression stage ( 14 ) and the expansion stage ( 15 ) are arranged directly adjacent to each other and are mechanically coupled for transferring the energy released in the expansion stage ( 15 ) to the compression stage ( 14 ) for the recompression of the refrigerant entering the compression stage ( 14 ) from the first tube element unit ( 3 a ).

3. The heat transfer circuit as claimed in claim 1 , wherein, in a vertical installation orientation of the fluid-air heat exchanger ( 3 ), the first tube element ( 3 a ) is arranged below the second tube element ( 3 b ).

4. The heat transfer system as claimed in claim 1 , wherein the expansion stage ( 15 ) includes a variable expansion volume in which an inner expansion of the first fluid takes place whereby energy is released and transmitted via the common shaft ( 17 ) to the compression stage ( 14 ), which also includes a variable volume in which an inner compression of the first fluid takes place using the energy released in the expansion stage ( 15 ).

5. The heat transfer system as claimed in claim 1 , wherein each of the compression stage ( 14 ) and the expansion stage ( 15 ) includes an inner wheel ( 14 a , 15 a ) supported on the common shaft ( 17 ) and an outer wheel ( 14 b , 15 b ) rotatably supported in the common housing ( 16 ) and surrounding the respective inner wheels ( 14 a , 15 a ), and the inner wheels ( 14 a , 15 a ) have a circumferential outer tooth structure and the outer wheels ( 14 b , 15 b ) have an inner tooth structure engaging the outer tooth structure of the inner wheels ( 14 a , 14 b ), the axes of rotation of the inner wheel and the outer wheel being spaced from each other such that, at one side, the inner and outer wheels are in fitting engagement.

Assignments (6)
CHANGE OF NAME Recorded Oct 30, 2015
From: HALLA VISTEON CLIMATE CONTROL CORPORATION
To: HANON SYSTEMS
Reel/Frame 037007/0103 →
RELEASE OF SECURITY INTEREST IN INTELLECTUAL PROPERTY Recorded Jun 9, 2014
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDINGS, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
Reel/Frame 033107/0717 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 2, 2013
From: VISTEON GLOBAL TECHNOLOGIES, INC.
To: HALLA VISTEON CLIMATE CONTROL CORPORATION
Reel/Frame 030935/0958 →
RELEASE BY SECURED PARTY AGAINST SECURITY INTEREST IN PATENTS ON REEL 025241 FRAME 0317 Recorded Apr 26, 2011
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDING, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
Reel/Frame 026178/0412 →
SECURITY AGREEMENT (REVOLVER) Recorded Oct 19, 2010
From: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDINGS, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC., AS AGENT
Reel/Frame 025238/0298 →
SECURITY AGREEMENT Recorded Oct 19, 2010
From: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDING, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC., AS AGENT
Reel/Frame 025241/0317 →