[go: up one dir, main page]

US20060237180A1 - Air heat exchanger - Google Patents

Air heat exchanger Download PDF

Info

Publication number
US20060237180A1
US20060237180A1 US11/406,817 US40681706A US2006237180A1 US 20060237180 A1 US20060237180 A1 US 20060237180A1 US 40681706 A US40681706 A US 40681706A US 2006237180 A1 US2006237180 A1 US 2006237180A1
Authority
US
United States
Prior art keywords
heat exchanger
air
elements
planar
air heat
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.)
Abandoned
Application number
US11/406,817
Inventor
Norman Anke
Franz Feuerstein
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.)
Liebherr Aerospace Lindenberg GmbH
Original Assignee
Liebherr Aerospace Lindenberg GmbH
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 Liebherr Aerospace Lindenberg GmbH filed Critical Liebherr Aerospace Lindenberg GmbH
Assigned to LIEBHERR-AEROSPACE LINDENBERG GMBH reassignment LIEBHERR-AEROSPACE LINDENBERG GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ANKE, NORMAN, FEUERSTEIN, FRANZ
Publication of US20060237180A1 publication Critical patent/US20060237180A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/10Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor
    • H05B3/16Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor the conductor being mounted on an insulating base
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24HFLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
    • F24H3/00Air heaters
    • F24H3/02Air heaters with forced circulation
    • F24H3/04Air heaters with forced circulation the air being in direct contact with the heating medium, e.g. electric heating element
    • F24H3/0405Air heaters with forced circulation the air being in direct contact with the heating medium, e.g. electric heating element using electric energy supply, e.g. the heating medium being a resistive element; Heating by direct contact, i.e. with resistive elements, electrodes and fins being bonded together without additional element in-between
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2255/00Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes
    • F28F2255/02Flexible elements

Definitions

  • the present disclosure relates to an air heat exchanger in air diffuser systems with flexible planar heat exchanger elements, in particular for use in aircraft.
  • heaters are incorporated in air diffuser systems.
  • heating elements with high surface temperatures are undesirable in the aircraft industry. Therefore, so-called panel heating elements are being used. Due to their large surface area, the same are capable of transferring a high thermal power despite low temperatures.
  • the objective is to install a rather large surface area on a small space, in order to be able to transfer as much heat as possible.
  • Output of the thermal power should be effected in a controlled way, and inadmissible excess temperatures should be avoided. This is ensured by the use of sensors and fuses. Therefore, the elements should be producible at low cost and should achieve a rather high performance with a low weight and a small size.
  • Air heaters with a structure as shown in the attached FIG. 1 are known already.
  • flexible panel heating elements 10 are inserted, which in the illustrated embodiment are arranged parallel to each other.
  • the panel heating elements constitute free-standing plates.
  • the panel heating elements can also consist of coaxially arranged tubes.
  • heat-dissipating cooling bodies for instance in the form of heat exchanger lamellae.
  • an air heat exchanger in an air diffuser system comprising flexible planar heat exchanger elements, in particular for use in aircraft, wherein the individual planar heat exchanger elements are connected with each other by means of webs.
  • these webs themselves are unheated. Inside these webs, conductors are disposed, which connect the individual heat exchanger conductors in the individual surfaces with each other. The webs only serve the mechanical connection of the planar heat exchanger elements.
  • the corresponding conductors usually, but not necessarily, are electric conductors.
  • planar heat exchanger elements can have a variable design in terms of shape, size and heat exchanger performance.
  • they can result in a much better utilization of the flow cross-section of the air-conducting conduit.
  • flow can be greater, so that they can provide a greater heat exchanger performance.
  • the same can also be equipped with a variable power density along their length. With a specified maximum temperature, which should not be exceeded, a uniform temperature can thus be adjusted along the length of the tube.
  • additional heat exchanging bodies are provided, for instance plates and/or ribs.
  • the additional heat exchanging bodies can be used both as supports and as spacers for the planar heat exchanger elements.
  • planar heat exchanger elements are manufactured together with the webs connecting the same as an integral element.
  • the sensors or other fuses for monitoring the temperature as well as connecting lines leading to the same can be integrated right during the manufacturing process of the planar heat exchanger elements and the webs connecting the same.
  • planar heat exchanger elements Upon manufacture of the planar heat exchanger elements and the webs of each element, the same is bent into its final shape. As far as the heat exchanger element is incorporated in a pipe conduit, the same will afterwards be inserted into the pipe conduit. In accordance with the herein disclosed aspect of the air heat exchanger, it is no longer necessary to connect each individual planar heat exchanger element separately. Rather, it is sufficient to connect the entire planar heat exchanger element to the heat exchanger fluid conduit.
  • the aforementioned air heat exchanger is used as an air heater, preferably for use in aircraft.
  • FIG. 1 shows a partly sectioned air heat exchanger in accordance with the prior art
  • FIG. 2 shows several views of a part of an air heat exchanger in various structural conditions in accordance with the present invention.
  • FIGS. 2 a to 2 c the various manufacturing steps of an air heat exchanger 20 are shown.
  • the same first of all consists of a number of planar heat exchanger elements 10 , which are each connected with each other by means of webs 14 .
  • the webs 14 substantially have the same structure as the heat exchanger elements 10 , which in the present embodiment constitute panel heating elements. Instead of corresponding panel heating elements, the same can of course also constitute panel cooling elements when used in an air conditioning system.
  • the webs include unheated conductors, which connect the heating conductors of the individual flexible heat exchanger elements 10 .
  • the unheated webs 14 have the same structure as the individual flexible heating elements 10 , whereby they can be manufactured in one and the same work process. This allows simultaneous manufacture of a plurality of flexible heating elements 10 together with the necessary unheated webs 14 in the same process.
  • the heat exchanger elements 10 are bent around the respective webs 14 , as is shown in FIG. 2 b . This results in a stack of planar heat exchanger elements, which can for instance be inserted in a pipe conduit.
  • the planar heat exchanger elements 10 each can have a different width, which is not illustrated here in greater detail. As a result, they are adapted better to the interior of the pipe.
  • the flexible planar heat exchanger elements 10 can be connected with heat exchanging bodies 16 , which dissipate the heat through convection to the surrounding medium, e.g. air.
  • the surrounding medium e.g. air.
  • the cooling bodies in particular in the form of ribs, can at the same time be used as supports for the flexible planar heat exchanger elements. This provides for a very compact construction.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

The present disclosure relates to an air heat exchanger in air diffuser systems with flexible planar heat exchanger elements, in particular for use in aircraft. In accordance with the present disclosure, the individual planar heat exchanger elements are connected with each other by means of webs. The present disclosure furthermore relates to a method for manufacturing air heat exchangers as well as to a use thereof.

Description

    CROSS-REFERENCE TO RELATED APPLICATION
  • This application claims priority to German Patent Application Serial No. 10 2005 018 050.7 filed Apr. 19, 2005, which is hereby incorporated by reference in its entirety for all purposes.
  • FIELD
  • The present disclosure relates to an air heat exchanger in air diffuser systems with flexible planar heat exchanger elements, in particular for use in aircraft.
  • BACKGROUND AND SUMMARY
  • For heating the air, heaters are incorporated in air diffuser systems. For safety reasons, heating elements with high surface temperatures are undesirable in the aircraft industry. Therefore, so-called panel heating elements are being used. Due to their large surface area, the same are capable of transferring a high thermal power despite low temperatures. The objective is to install a rather large surface area on a small space, in order to be able to transfer as much heat as possible. Output of the thermal power should be effected in a controlled way, and inadmissible excess temperatures should be avoided. This is ensured by the use of sensors and fuses. Therefore, the elements should be producible at low cost and should achieve a rather high performance with a low weight and a small size.
  • Air heaters with a structure as shown in the attached FIG. 1 are known already. In an air-conducting tube 12 to be heated, flexible panel heating elements 10 are inserted, which in the illustrated embodiment are arranged parallel to each other. In this case, the panel heating elements constitute free-standing plates. As an alternative to the illustrated embodiment, the panel heating elements can also consist of coaxially arranged tubes. There can also be provided heat-dissipating cooling bodies, for instance in the form of heat exchanger lamellae.
  • These prior art systems involve a very high contacting effort, as the individual panel heating elements must be connected with each other via soldering points, plug-in connections and the like. As a result, the risk of defects is substantially increased during the manufacture of such elements. In particular the manufacture of coaxial panel heating elements involves a substantially higher mounting effort as compared to plate-shaped elements.
  • It is the object of the present disclosure to create an air heat exchanger which is comparatively easier to manufacture and to install.
  • In accordance with the present disclosure, this object is solved by an air heat exchanger in an air diffuser system comprising flexible planar heat exchanger elements, in particular for use in aircraft, wherein the individual planar heat exchanger elements are connected with each other by means of webs.
  • In one example, these webs themselves are unheated. Inside these webs, conductors are disposed, which connect the individual heat exchanger conductors in the individual surfaces with each other. The webs only serve the mechanical connection of the planar heat exchanger elements. The corresponding conductors usually, but not necessarily, are electric conductors.
  • Accordingly, the planar heat exchanger elements can have a variable design in terms of shape, size and heat exchanger performance. Thus, they can result in a much better utilization of the flow cross-section of the air-conducting conduit. In certain portions of round tubes, for instance, flow can be greater, so that they can provide a greater heat exchanger performance.
  • To effect a uniform surface temperature of the flexible heat exchanger elements in the direction of the traversed length, the same can also be equipped with a variable power density along their length. With a specified maximum temperature, which should not be exceeded, a uniform temperature can thus be adjusted along the length of the tube.
  • Particularly advantageously, additional heat exchanging bodies are provided, for instance plates and/or ribs. The additional heat exchanging bodies can be used both as supports and as spacers for the planar heat exchanger elements.
  • The above-mentioned object of the present disclosure is solved in particular by a method wherein, the planar heat exchanger elements are manufactured together with the webs connecting the same as an integral element.
  • Accordingly, the sensors or other fuses for monitoring the temperature as well as connecting lines leading to the same can be integrated right during the manufacturing process of the planar heat exchanger elements and the webs connecting the same.
  • Upon manufacture of the planar heat exchanger elements and the webs of each element, the same is bent into its final shape. As far as the heat exchanger element is incorporated in a pipe conduit, the same will afterwards be inserted into the pipe conduit. In accordance with the herein disclosed aspect of the air heat exchanger, it is no longer necessary to connect each individual planar heat exchanger element separately. Rather, it is sufficient to connect the entire planar heat exchanger element to the heat exchanger fluid conduit.
  • Particularly advantageously, the aforementioned air heat exchanger is used as an air heater, preferably for use in aircraft.
  • Further details, features and advantages of the present disclosure will be illustrated with reference to an embodiment shown in the figures.
  • BRIEF DESCRIPTION OF THE FIGURES
  • FIG. 1 shows a partly sectioned air heat exchanger in accordance with the prior art; and
  • FIG. 2 shows several views of a part of an air heat exchanger in various structural conditions in accordance with the present invention.
  • DETAILED DESCRIPTION
  • In FIGS. 2 a to 2 c, the various manufacturing steps of an air heat exchanger 20 are shown. The same first of all consists of a number of planar heat exchanger elements 10, which are each connected with each other by means of webs 14. The webs 14 substantially have the same structure as the heat exchanger elements 10, which in the present embodiment constitute panel heating elements. Instead of corresponding panel heating elements, the same can of course also constitute panel cooling elements when used in an air conditioning system.
  • In a manner not illustrated here, the webs include unheated conductors, which connect the heating conductors of the individual flexible heat exchanger elements 10. In principle, the unheated webs 14 have the same structure as the individual flexible heating elements 10, whereby they can be manufactured in one and the same work process. This allows simultaneous manufacture of a plurality of flexible heating elements 10 together with the necessary unheated webs 14 in the same process. After the manufacturing process in flat position, as shown in FIG. 2 a, the heat exchanger elements 10 are bent around the respective webs 14, as is shown in FIG. 2 b. This results in a stack of planar heat exchanger elements, which can for instance be inserted in a pipe conduit.
  • Advantageously, the planar heat exchanger elements 10 each can have a different width, which is not illustrated here in greater detail. As a result, they are adapted better to the interior of the pipe. As is for instance indicated in FIG. 2 c, the flexible planar heat exchanger elements 10 can be connected with heat exchanging bodies 16, which dissipate the heat through convection to the surrounding medium, e.g. air. In addition, there can also be provided heat exchanging ribs, which cannot be seen in FIG. 2 c. The cooling bodies, in particular in the form of ribs, can at the same time be used as supports for the flexible planar heat exchanger elements. This provides for a very compact construction.

Claims (20)

1. An air heat exchanger in air diffuser systems, comprising flexible planar heat exchanger elements, wherein the individual planar heat exchanger elements are connected with each other by means of webs.
2. The air heat exchanger as claimed in claim 1, wherein the air heat exchanger is coupled in an aircraft.
3. The air heat exchanger as claimed in claim 1, wherein the webs are made of a flexible, bendable material.
4. The air heat exchanger as claimed in claim 1, wherein the webs have a structure that is the same as the planar heat exchanger elements.
5. The air heat exchanger as claimed in claim 1, wherein the planar heat exchanger elements have a variable design in terms of shape, size and heat exchanger performance.
6. The air heat exchanger as claimed in claim 1, wherein the planar heat exchanger elements have a variable heat exchanger performance along their length, in order to achieve a uniform surface temperature in the direction of the traversed length.
7. The air heat exchanger as claimed in claim 1, wherein the planar heat exchanger elements are connected with additional heat exchanging bodies.
8. The air heat exchanger as claimed in claim 7, wherein the additional heat exchanging bodies are shaped in a form of plates and/or ribs.
9. The air heat exchanger as claimed in claim 1, wherein the planar heat exchanger elements constitute plates.
10. The air heat exchanger as claimed in claim 1, wherein the additional heat exchanging bodies are used as supports and as spacers for the planar heat exchanger elements.
11. A method for manufacturing an air heat exchanger in air diffuser systems comprising fabricating a plurality of individual planar heat exchanger elements and a plurality of webs connecting the individual planar heat exchanger elements as an integral element.
12. The method as claimed in claim 11, wherein sensors for monitoring the temperature as well as their connecting lines are integrated into the planar heat exchanger elements during the fabricating process.
13. The method as claimed in claim 11, wherein the planar heat exchanger elements are first manufactured in a flat position together with the webs connecting the same and are then bent into a final shape and possibly inserted into a pipe conduit.
14. The method as claimed in claim 11, further comprising using said air heat exchanger as an air heater to heat air in an aircraft.
15. The method as claimed in claim 11, wherein said individual planar elements are flexible.
16. An air heat exchanger in air diffuser systems, comprising:
a plurality of flexible planar heat exchanger elements, and
a plurality of webs connecting the individual planar heat exchanger elements, wherein the air heat exchanged is coupled in an aircraft.
17. The air heat exchanger as claimed in claim 16, wherein the webs are made of a flexible and bendable material, and wherein the webs have a structure that is the same as the planar heat exchanger elements.
18. The air heat exchanger as claimed in claim 16, wherein at least two planar heat exchanger elements have a variable shape, size and heat exchanger performance.
19. The air heat exchanger as claimed in claim 18, wherein at least two planar heat exchanger elements have a variable heat exchanger performance along their respective lengths, in order to achieve a uniform surface temperature in the direction of the traversed length.
20. The air heat exchanger as claimed in claim 19, wherein at least one planar heat exchanger element and one web are integrally formed, the exchanger further comprising a plurality of sensors for monitoring the temperature as well as corresponding connecting lines, said sensors further being integrally formed into the planar heat exchanger elements.
US11/406,817 2005-04-19 2006-04-18 Air heat exchanger Abandoned US20060237180A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005018050.7 2005-04-19
DE102005018050A DE102005018050A1 (en) 2005-04-19 2005-04-19 Air heat exchanger

Publications (1)

Publication Number Publication Date
US20060237180A1 true US20060237180A1 (en) 2006-10-26

Family

ID=36685986

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/406,817 Abandoned US20060237180A1 (en) 2005-04-19 2006-04-18 Air heat exchanger

Country Status (4)

Country Link
US (1) US20060237180A1 (en)
EP (1) EP1715272A1 (en)
CA (1) CA2543382A1 (en)
DE (1) DE102005018050A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11371782B2 (en) 2018-07-26 2022-06-28 Dana Canada Corporation Heat exchanger with parallel flow features to enhance heat conduction

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12017806B2 (en) * 2022-01-21 2024-06-25 Maxar Space Llc Satellite with modular radiator panels

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3341925A (en) * 1963-06-26 1967-09-19 Gen Motors Corp Method of making sheet metal heat exchangers with air centers
US3508607A (en) * 1967-04-19 1970-04-28 Motoren Turbinen Union Heat exchanger
US4075091A (en) * 1972-06-28 1978-02-21 National Research Development Corporation Method for effecting heat or mass transfer
US4258785A (en) * 1980-02-08 1981-03-31 Borg-Warner Corporation Heat exchanger interplate fitting
US5507338A (en) * 1995-08-30 1996-04-16 Ford Motor Company Tab for an automotive heat exchanger
US5855240A (en) * 1998-06-03 1999-01-05 Ford Motor Company Automotive heat exchanger
US6244333B1 (en) * 1998-08-27 2001-06-12 Zeks Air Drier Corporation Corrugated folded plate heat exchanger
US6742578B2 (en) * 2001-04-11 2004-06-01 Toyo Radiator Co., Ltd Heat exchanger core

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI47141C (en) * 1960-03-16 1973-09-10 Rosenblad Heat exchange system for two heat exchanging media of different pressures.
FR2334932A1 (en) * 1975-12-09 1977-07-08 Ussi Const Usines Separation I Heat exchanger battery using plastics pockets - has pockets clamped between bars on fixed and moving frames to allow expansion
JPH02146497A (en) * 1988-11-26 1990-06-05 Kajima Corp Flexible film type heat exchanger
SE465894B (en) * 1989-09-15 1991-11-11 Sten Zeilon HEAT EXCHANGER WITH TIGHTENING MEMBRANE AND GAS TRANSMISSIBLE DISTANCE BODIES

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3341925A (en) * 1963-06-26 1967-09-19 Gen Motors Corp Method of making sheet metal heat exchangers with air centers
US3508607A (en) * 1967-04-19 1970-04-28 Motoren Turbinen Union Heat exchanger
US4075091A (en) * 1972-06-28 1978-02-21 National Research Development Corporation Method for effecting heat or mass transfer
US4258785A (en) * 1980-02-08 1981-03-31 Borg-Warner Corporation Heat exchanger interplate fitting
US5507338A (en) * 1995-08-30 1996-04-16 Ford Motor Company Tab for an automotive heat exchanger
US5855240A (en) * 1998-06-03 1999-01-05 Ford Motor Company Automotive heat exchanger
US6244333B1 (en) * 1998-08-27 2001-06-12 Zeks Air Drier Corporation Corrugated folded plate heat exchanger
US6742578B2 (en) * 2001-04-11 2004-06-01 Toyo Radiator Co., Ltd Heat exchanger core

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11371782B2 (en) 2018-07-26 2022-06-28 Dana Canada Corporation Heat exchanger with parallel flow features to enhance heat conduction

Also Published As

Publication number Publication date
DE102005018050A1 (en) 2006-10-26
EP1715272A1 (en) 2006-10-25
CA2543382A1 (en) 2006-10-19

Similar Documents

Publication Publication Date Title
CA2682420C (en) Heat absorbing or dissipating device with multi-pipe reversely transported temperature difference fluids
US8622116B2 (en) Heat absorbing or dissipating device with multi-pipe reversely transported temperature difference fluids
US20110094718A1 (en) Heat absorbing or dissipating device with double-scroll piping transmitting temperature difference fluid
CN102085789B (en) Pre-heater apparatus for vehicle
WO2013168526A1 (en) Heat exchanger and vehicle air conditioning device
EP2314968A2 (en) Heat absorbing or dissipating device with piping staggered and uniformly distributed by temperature difference
CN108700330A (en) Fastening system for pipes passing through a plate of an air handling unit, and an air handling unit comprising such a system
CN104540252A (en) PTC electric heating device
US20140217190A1 (en) A tubular section bar for a biphasic radiator and relative biphasic radiator
US20060237180A1 (en) Air heat exchanger
US20160025425A1 (en) Heat exchanger with slotted guard fin
KR20130008437A (en) Substrate for electric heater
EP3137836B1 (en) Improved heat exchanger
CN115768638A (en) Electric fluid heater
JP6111024B2 (en) Heat exchanger
JP6454915B2 (en) Cooling heat transfer device
CN207268481U (en) An air conditioner indoor unit and a PTC heating plate
JP2001116475A (en) Heating radiator and method for manufacturing it
CN114046601B (en) Multifunctional sectional heating and clean gas heat exchange device
RU2328661C1 (en) Heat-exchanger of floor heating convector (options)
CN113396305B (en) PTC heater
RU65188U1 (en) HEAT EXCHANGER OF FLOOR HEATING CONVECTOR (OPTIONS)
KR101821042B1 (en) Heat exchanger using cartridge heater
CN107906648A (en) Radiation recuperator, indoor apparatus of air conditioner and air conditioner
CZ305152B6 (en) Heat-exchange apparatus formed by hollow polymer fibers

Legal Events

Date Code Title Description
AS Assignment

Owner name: LIEBHERR-AEROSPACE LINDENBERG GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:ANKE, NORMAN;FEUERSTEIN, FRANZ;REEL/FRAME:017886/0612

Effective date: 20060502

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION