US2316273A - Heater - Google Patents
Heater Download PDFInfo
- Publication number
- US2316273A US2316273A US357175A US35717540A US2316273A US 2316273 A US2316273 A US 2316273A US 357175 A US357175 A US 357175A US 35717540 A US35717540 A US 35717540A US 2316273 A US2316273 A US 2316273A
- Authority
- US
- United States
- Prior art keywords
- chamber
- pipe
- exhaust pipe
- heater
- air
- 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.)
- Expired - Lifetime
Links
- 239000007789 gas Substances 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 230000004075 alteration Effects 0.000 description 2
- 238000011109 contamination Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000005336 cracking Methods 0.000 description 1
- 239000003517 fume Substances 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000002574 poison Substances 0.000 description 1
- 231100000614 poison Toxicity 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
-
- 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
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/10—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically
- F28D7/103—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically consisting of more than two coaxial conduits or modules of more than two coaxial conduits
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Definitions
- This invention relates to improvements in heaters, and refers particularly to heaters primarily intended for use on airplanes.
- Heaters operated by the heat generated by an engine'are in common use consist usually either of air heaters, or steam or hot water heaters.
- Many heaters of the formertype are open to the grave objection that exhaust fumes are liable to mixwith and poison the air being heated, which is particularly dangerous in airplane installations; and heaters of the latter type are not satisfactorycn airplanes for the reason that they are liable to freeze up.
- Another object of the invention is to provide such a heater centrally through which the exhaust pipe extends, and to provide anair cham her around this pipe which is spaced therefrom by an annular arrangement of tubes 'so disposed that a plurality of connected walls extend continuously around the pipe and amply protect theair chamber from contamination by exhaust ases in the event even of cracking of the pipe itself.
- a further :object of the invention is to provide such a heater wherein the tubes, preferably rectangular in cross section, extend contiguous to one another parallel with the. exhaust pipe,
- haust pipe preferably provided with a plurality of small indentations 20 therein to increase its radiating capacity.
- a second pipe 2! Spaced concentrically around the pipe is. is a second pipe 2! which forms the inner annular wall of an air chamber i2-the outer encircling wall of which is shown at [2a.
- Closing the ends of the heater are two annular walls 18 the margins of central openings of which are .brazed, welded or otherwise suitably secured around the exhaust pipe 19:
- eachwall [8 consists of two separate annular portions, the outer periphery of the inner portion being secured-tothe pipe 2i, and the outer sections I 8b being formed of flexed extremities of the outer chamber wall I2a.
- Yet another object of the invention is to provide a heater which is light in weight, compact, efficient in operation, relatively easy tomanufacture. and easy to install.
- Figure 1 illustrates a longitudinal section of the invention
- Figure 2 is a section on the line 2-2 of Figure 1.
- annularly arranged spacing members or tubes 22 preferably substantially rectangular in cross section, extending parallel with the exhaust pipe l9, have their adjacent walls brazed or welded to the latter, and their opposite walls similarly secured to the pipe 2
- the contiguous, substantially radial sides of the tubes 22 are also welded or brazed to one another throughout their entire length, so that the tubes thus united to one another form an annular arrangement of radial walls between pipes I9 and 2
- the tubes; 22 open at their extremities into an nular chambers 23a and -24a closed at their outer ends by the walls l8,'and projecting from these chambers and open to the outside air are pipes.
- a heater comprising an annular chamber having an inlet and an outlet pipe extending therefrom, an exhaust pipe projecting through the annular chamber and spaced therefrom, the chamber having annular end walls which project inwardly and are secured around the exhaust pipe, tubular spacing members annularly arranged around the exhaust pipe and welded or brazed thereto and to said chamber, said spacing members being contiguous and brazed or welded to one another to form an encircling gasproo'f joint between the exhaust pipe and chamber, said members actingas a heat transfer medium between the exhaust pipe and the chember,and radiating-fins projecting partway across the interior of the chamber from its inner wall.
- a heater comprising the combination set ing from the compartments to permit passage of air through said members.
- a heater compriesing an annular air chamber having an inlet pipe and an outlet pipe connected thereto, an exhaust pipe extending through said annular chamber, means directly connected to the exhaust pipe and the inner wall of the chamber spacing the exhaust pipe inwardly from the chamber comprising tub'ular spacing members of substantially rectangular cross section, the sides of contiguous members being secured to each other throughout their height to form an encirclingv gasproof wall between the exhaust pipe and the chamber and to serve as means for transferring heat from the exhaust pipe to the chamber.
- a heater comprising an annular air chamber having an inlet pipe and an outlet pipe connected thereto, an exhaust pipe extending through said annular chamber sealed therefrom and spaced from the inner wall thereof to provide an annular intermediate chamber, and
- spacing members directly connected to the exforth in claim 1, wherein the spacing members' are substantially rectangular in cross section and terminate a short distance from both end walls thereby forming compartments into which the tubes open, and pipes open to the air extendhaust pipe and to the inner wall of the chamber constituting heat transfer means from the former to the latter, said spacing members comprising a plurality of tubes annularly arranged around the exhaust pipe and having juxtaposed flat walls connected to one another to form an encircling gas-proof wall between the exhaust pipe and the chamber.
Landscapes
- Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Description
April 13, 1943. L. MEYER ETAL HEATER Filed Sept. 17, 1940 L I m w i 5/ m v0 0 a mZ/fi a M 2 Patented Apr. 13, 1943 2,316,273 imArEa Ludwig Meyer and Friedrich Klein, Dessau, Getmy; vested in the Alien Property Custodian Application September 17,1940, Serial No. 357,175
In Germany July 13,1939
4 Claims. (01. 257-441) This invention relates to improvements in heaters, and refers particularly to heaters primarily intended for use on airplanes.
Heaters operated by the heat generated by an engine'are in common use, and consist usually either of air heaters, or steam or hot water heaters. Many heaters of the formertype are open to the grave objection that exhaust fumes are liable to mixwith and poison the air being heated, which is particularly dangerous in airplane installations; and heaters of the latter type are not satisfactorycn airplanes for the reason that they are liable to freeze up.
It is an object of this invention to, provide a heater of the air type wherein the pipe through which the exhaust gases flow is spaced from the chamber through which the air to be heated passes by tubes through which air also travels; and .to utilize these tubes as a. heat transfer medium between the exhaust pipe and the air chamber so that a high ratio of heat exchange is provided.
Another object of the invention is to provide such a heater centrally through which the exhaust pipe extends, and to provide anair cham her around this pipe which is spaced therefrom by an annular arrangement of tubes 'so disposed that a plurality of connected walls extend continuously around the pipe and amply protect theair chamber from contamination by exhaust ases in the event even of cracking of the pipe itself.
A further :object of the invention is to provide such a heater wherein the tubes, preferably rectangular in cross section, extend contiguous to one another parallel with the. exhaust pipe,
haust pipe preferably provided with a plurality of small indentations 20 therein to increase its radiating capacity. Spaced concentrically around the pipe is. is a second pipe 2! which forms the inner annular wall of an air chamber i2-the outer encircling wall of which is shown at [2a. Closing the ends of the heater are two annular walls 18 the margins of central openings of which are .brazed, welded or otherwise suitably secured around the exhaust pipe 19: In this instance eachwall [8 consists of two separate annular portions, the outer periphery of the inner portion being secured-tothe pipe 2i, and the outer sections I 8b being formed of flexed extremities of the outer chamber wall I2a.
' which are brazed or welded at their margins to the pipe 2|, as a safety precaution to prevent the entry of exhaust gases into the chamber i2; 2! denotes radiating fins which project part way across the chamber l2 from the pipe 2| which forms the inner wall of such chamber.
and are brazed or welded to the outer periphery of the latter, to the inner wall of the air chamber and to' one another, so that eiiicient heat transfer is obtained fromthe pipe to the cham ber,
Yet another object of the invention is to provide a heater which is light in weight, compact, efficient in operation, relatively easy tomanufacture. and easy to install.
Having thus briefly enumerated some of the obiects and advanta es of the invention, I will now proceed to describe a preferred embodiment thereof, with the aid of the accompanying drawing, in which: 1
Figure 1 illustrates a longitudinal section of the invention, and
Figure 2 is a section on the line 2-2 of Figure 1.
Referring to the drawing, is denotes an ex- A plurality of annularly arranged spacing members or tubes 22, preferably substantially rectangular in cross section, extending parallel with the exhaust pipe l9, have their adjacent walls brazed or welded to the latter, and their opposite walls similarly secured to the pipe 2| which forms the inner wall of the chamber l2. The contiguous, substantially radial sides of the tubes 22 are also welded or brazed to one another throughout their entire length, so that the tubes thus united to one another form an annular arrangement of radial walls between pipes I9 and 2| so that should'the former crack ample protection is afforded for preventing contamination of the air flowing through the chamber I2 by the exhaust gases, and at the same time the sides or radial walls of the tubes 22 constituteexcellent heat transfer means for the passage of heat from the exhaust pipe I 9 to the chamber i 2.
The tubes; 22 open at their extremities into an nular chambers 23a and -24a closed at their outer ends by the walls l8,'and projecting from these chambers and open to the outside air are pipes.
23 and 26 respectively. Connected to one exemity of the chamber I2 is an air inlet pipe 25. and projecting from its opposite extremity is a second pipe 26 through which heated air flows to a suitable register or outlet (not shown).
From the foregoing it will be clearly seen that hi h heat transfer is obtained from the exhaust p pe l9 to the air chamber I 2, mainly through the walls of the tubes 22; that the continuous annular arrangement of the connected tubes and th joints formed between them constitute additional protection against leakage of gas from the pipe I! into the chamber l2; and that the end wall construction further assists in preventing such leakage. Also that, due to the tubular construction of the heater, it is light in weight and therefore specially suited for use in airplanes.
While the preferred construction has been described and shown, it is understood that alterations and modifications may be made thereto provided the said alterations and modifications fall within the scope of the appended claims.
What we claim is:
1. A heater comprising an annular chamber having an inlet and an outlet pipe extending therefrom, an exhaust pipe projecting through the annular chamber and spaced therefrom, the chamber having annular end walls which project inwardly and are secured around the exhaust pipe, tubular spacing members annularly arranged around the exhaust pipe and welded or brazed thereto and to said chamber, said spacing members being contiguous and brazed or welded to one another to form an encircling gasproo'f joint between the exhaust pipe and chamber, said members actingas a heat transfer medium between the exhaust pipe and the chember,and radiating-fins projecting partway across the interior of the chamber from its inner wall.
2. A heater comprising the combination set ing from the compartments to permit passage of air through said members.
3. A heater compriesing an annular air chamber having an inlet pipe and an outlet pipe connected thereto, an exhaust pipe extending through said annular chamber, means directly connected to the exhaust pipe and the inner wall of the chamber spacing the exhaust pipe inwardly from the chamber comprising tub'ular spacing members of substantially rectangular cross section, the sides of contiguous members being secured to each other throughout their height to form an encirclingv gasproof wall between the exhaust pipe and the chamber and to serve as means for transferring heat from the exhaust pipe to the chamber.
4. A heater comprising an annular air chamber having an inlet pipe and an outlet pipe connected thereto, an exhaust pipe extending through said annular chamber sealed therefrom and spaced from the inner wall thereof to provide an annular intermediate chamber, and
' spacing members directly connected to the exforth in claim 1, wherein the spacing members' are substantially rectangular in cross section and terminate a short distance from both end walls thereby forming compartments into which the tubes open, and pipes open to the air extendhaust pipe and to the inner wall of the chamber constituting heat transfer means from the former to the latter, said spacing members comprising a plurality of tubes annularly arranged around the exhaust pipe and having juxtaposed flat walls connected to one another to form an encircling gas-proof wall between the exhaust pipe and the chamber.
' LUDWIG MEYER.
FRIEDRICH KLEIN.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2316273X | 1939-07-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2316273A true US2316273A (en) | 1943-04-13 |
Family
ID=7994581
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US357175A Expired - Lifetime US2316273A (en) | 1939-07-13 | 1940-09-17 | Heater |
Country Status (1)
Country | Link |
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US (1) | US2316273A (en) |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2650073A (en) * | 1949-06-25 | 1953-08-25 | Air Preheater | Combined regenerator and precooler for gas turbine cycles |
US2703921A (en) * | 1949-04-14 | 1955-03-15 | Brown Fintube Co | Method of making internally finned tubes |
US2726681A (en) * | 1950-09-18 | 1955-12-13 | Brown Fintube Co | Internally finned tube |
US2756032A (en) * | 1952-11-17 | 1956-07-24 | Heater | |
DE1089787B (en) * | 1955-10-28 | 1960-09-29 | Robert James Swinton Smith | Heat exchange device in which heat is transferred from a medium to be cooled with the interposition of an evaporating transfer fluid to a coolant |
US3002729A (en) * | 1955-06-20 | 1961-10-03 | Brown Fintube Co | Tube with external fins |
US3154141A (en) * | 1959-04-28 | 1964-10-27 | Huet Andre | Roughened heat exchanger tube |
DK100385C (en) * | 1956-09-05 | 1964-11-23 | English Electric Co Ltd | Fuel element tank for nuclear reactor. |
US3374833A (en) * | 1965-05-12 | 1968-03-26 | Equipment De La Blanchisserie | Heating still |
US3584682A (en) * | 1968-07-29 | 1971-06-15 | Borg Warner | Tubular heat transfer device |
US4228848A (en) * | 1979-01-23 | 1980-10-21 | Grumman Energy Systems, Inc. | Leak detection for coaxial heat exchange system |
DE3025075A1 (en) * | 1980-07-02 | 1982-01-21 | Grumman Energy Systems, Inc., Ronkonkoma, N.Y. | Leak detection for coaxial heat exchange - has outer, intermediate and inner coaxial tubes with longitudinal fins projecting radially inwards |
EP0086470A1 (en) * | 1982-02-15 | 1983-08-24 | Wilhelm Dr.-Ing. Vox | Heat pump condensor with three specifically co-axial tubular elements |
US5385299A (en) * | 1992-03-02 | 1995-01-31 | Zawada; Michael E. | Fresh air intake system for a dwelling having central forced warm air heating |
US20040134649A1 (en) * | 2003-01-14 | 2004-07-15 | Paul Richardson | Carpet cleaning system |
US20050274499A1 (en) * | 2004-05-29 | 2005-12-15 | Rule David D | Systems, devices and methods for regulating temperatures of tanks, containers and contents therein |
EP1496327A3 (en) * | 2003-07-11 | 2007-11-14 | Bayerische Motoren Werke Aktiengesellschaft | Heat exchanger |
US20070264389A1 (en) * | 2006-05-11 | 2007-11-15 | Rule David D | Systems, apparatuses and methods for processing the contents of containers and tanks, and methods for modifying the processing capabilities of tanks and containers |
US20080175951A1 (en) * | 2007-01-23 | 2008-07-24 | Rule David D | Methods, apparatuses and systems of fermentation |
US20110011069A1 (en) * | 2009-07-16 | 2011-01-20 | Honda Motor Co., Ltd. | Cogeneration apparatus |
US20110094492A1 (en) * | 2008-04-11 | 2011-04-28 | Eduard Alper Bolkan | Device for feeding water steam via a heat exchanger in a combustion chamber and a method |
US20140245768A1 (en) * | 2013-03-04 | 2014-09-04 | Rocky Research | Co-fired absorption system generator |
US10935321B2 (en) | 2015-02-04 | 2021-03-02 | Kilr-Chilr, Llc | Energy transfer systems and energy transfer methods |
-
1940
- 1940-09-17 US US357175A patent/US2316273A/en not_active Expired - Lifetime
Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2703921A (en) * | 1949-04-14 | 1955-03-15 | Brown Fintube Co | Method of making internally finned tubes |
US2650073A (en) * | 1949-06-25 | 1953-08-25 | Air Preheater | Combined regenerator and precooler for gas turbine cycles |
US2726681A (en) * | 1950-09-18 | 1955-12-13 | Brown Fintube Co | Internally finned tube |
US2756032A (en) * | 1952-11-17 | 1956-07-24 | Heater | |
US3002729A (en) * | 1955-06-20 | 1961-10-03 | Brown Fintube Co | Tube with external fins |
DE1089787B (en) * | 1955-10-28 | 1960-09-29 | Robert James Swinton Smith | Heat exchange device in which heat is transferred from a medium to be cooled with the interposition of an evaporating transfer fluid to a coolant |
DK100385C (en) * | 1956-09-05 | 1964-11-23 | English Electric Co Ltd | Fuel element tank for nuclear reactor. |
US3154141A (en) * | 1959-04-28 | 1964-10-27 | Huet Andre | Roughened heat exchanger tube |
US3374833A (en) * | 1965-05-12 | 1968-03-26 | Equipment De La Blanchisserie | Heating still |
US3584682A (en) * | 1968-07-29 | 1971-06-15 | Borg Warner | Tubular heat transfer device |
US4228848A (en) * | 1979-01-23 | 1980-10-21 | Grumman Energy Systems, Inc. | Leak detection for coaxial heat exchange system |
DE3025075A1 (en) * | 1980-07-02 | 1982-01-21 | Grumman Energy Systems, Inc., Ronkonkoma, N.Y. | Leak detection for coaxial heat exchange - has outer, intermediate and inner coaxial tubes with longitudinal fins projecting radially inwards |
EP0086470A1 (en) * | 1982-02-15 | 1983-08-24 | Wilhelm Dr.-Ing. Vox | Heat pump condensor with three specifically co-axial tubular elements |
US5385299A (en) * | 1992-03-02 | 1995-01-31 | Zawada; Michael E. | Fresh air intake system for a dwelling having central forced warm air heating |
US20040134649A1 (en) * | 2003-01-14 | 2004-07-15 | Paul Richardson | Carpet cleaning system |
EP1496327A3 (en) * | 2003-07-11 | 2007-11-14 | Bayerische Motoren Werke Aktiengesellschaft | Heat exchanger |
US7870891B2 (en) * | 2004-05-29 | 2011-01-18 | Kilr-Chilr, Llc | Systems, devices and methods for regulating temperatures of tanks, containers and contents therein |
US8881795B2 (en) | 2004-05-29 | 2014-11-11 | Kilr-Chilr, Llc | Temperature regulating systems |
US20110168349A1 (en) * | 2004-05-29 | 2011-07-14 | Rule David D | Systems, Devices and Methods for Regulating Temperatures of Tanks, Containers and Contents Therein |
US20050274499A1 (en) * | 2004-05-29 | 2005-12-15 | Rule David D | Systems, devices and methods for regulating temperatures of tanks, containers and contents therein |
US7685715B2 (en) | 2006-05-11 | 2010-03-30 | Kilr-Chilr, Llc | Methods for processing the contents of containers and tanks and methods for modifying the processing capabilities of tanks and containers |
US20100212860A1 (en) * | 2006-05-11 | 2010-08-26 | Rule David D | Systems, Apparatuses and Methods for Processing the Contents of Tanks and Containers, and Methods for Modifying the Processing Capabilities of Tanks and Containers |
US20070264389A1 (en) * | 2006-05-11 | 2007-11-15 | Rule David D | Systems, apparatuses and methods for processing the contents of containers and tanks, and methods for modifying the processing capabilities of tanks and containers |
US20080175951A1 (en) * | 2007-01-23 | 2008-07-24 | Rule David D | Methods, apparatuses and systems of fermentation |
US10865369B2 (en) | 2007-01-23 | 2020-12-15 | Kilr-Chilr, Llc | Fermentation methods |
US20110094492A1 (en) * | 2008-04-11 | 2011-04-28 | Eduard Alper Bolkan | Device for feeding water steam via a heat exchanger in a combustion chamber and a method |
US20110011069A1 (en) * | 2009-07-16 | 2011-01-20 | Honda Motor Co., Ltd. | Cogeneration apparatus |
US8739521B2 (en) * | 2009-07-16 | 2014-06-03 | Honda Motor Co., Ltd. | Cogeneration apparatus |
US20140245768A1 (en) * | 2013-03-04 | 2014-09-04 | Rocky Research | Co-fired absorption system generator |
US9664451B2 (en) * | 2013-03-04 | 2017-05-30 | Rocky Research | Co-fired absorption system generator |
US10935321B2 (en) | 2015-02-04 | 2021-03-02 | Kilr-Chilr, Llc | Energy transfer systems and energy transfer methods |
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