GB1382876A - Regenerative heat exchanger devices - Google Patents
Regenerative heat exchanger devicesInfo
- Publication number
- GB1382876A GB1382876A GB557172A GB557172A GB1382876A GB 1382876 A GB1382876 A GB 1382876A GB 557172 A GB557172 A GB 557172A GB 557172 A GB557172 A GB 557172A GB 1382876 A GB1382876 A GB 1382876A
- Authority
- GB
- United Kingdom
- Prior art keywords
- block
- turbine
- via ducts
- feb
- heat exchangers
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
- F02C7/10—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
- F02C7/10—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
- F02C7/105—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers of the rotary type
-
- 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
- F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
- F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
-
- 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
- F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
- F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
- F28D19/041—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier with axial flow through the intermediate heat-transfer medium
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S165/00—Heat exchange
- Y10S165/009—Heat exchange having a solid heat storage mass for absorbing heat from one fluid and releasing it to another, i.e. regenerator
- Y10S165/013—Movable heat storage mass with enclosure
- Y10S165/014—Reciprocated linearly
Abstract
1382876 Gas turbine engines SOC ANON DE VEHICULES INDUSTRIELS ET D'EQUIPEMENTS MECANIQUES 7 Feb 1972 [9 Feb 1971 1 Feb 1972] 5571/72 Heading F1G [Also in Division F4] In a vehicle gas turbine engine incorporating a pair of regenerative heat exchangers 38 each comprising a cylindrical regenerator block 5 which is both rotated and axially reciprocated and is made up of a series of circular plates 21 stacked and clamped on a central rod 15, exhaust gases leaving the turbine wheels 32; 33 via ducts 44 are directed through the regenerative heat exchangers 38 by way of a plurality of duct sections 4 which are parallel to and alternate with similar duct sections 3 through which compressed air from a compressor 31 is passed via ducts 37. Heated compressed air leaving exchangers 38 is supplied to a chamber 40 for combustion via ducts 39. Cooled exhaust gases leave via ducts 46. Each cylindrical regenerator block 5 may be rotated through the action of at least one of the fluids passing through the block and serving to generate a torque to rotate the block, this being achieved by offsetting the axial planes of the duct sections 3 and 4 in relation to the central axis (50) Figs. 16, 17 and 19 (not shown) of the block. Mechanical means, as shown, or fluid-pressure see Fig. 5 (not shown) may be used to effect axial reciprocation of the block 5. The two heat exchangers 38 are arranged to have their axial reciprocating movements offset by a half-stroke and are symmetrically disposed in relation to the turbine axis 47. The compressor 31 is driven from the first turbine wheel 32. The second turbine wheel 33 drives a reduction gearing 34 and an output shaft 35. A swivelling distributer 36 is provided between the turbine wheels.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7104206A FR2126940A1 (en) | 1971-02-09 | 1971-02-09 | Gas turbine exhaust cooler - with cylindrical block permeable only radially and oscillating axially |
FR7203350A FR2170815A2 (en) | 1972-02-01 | 1972-02-01 | Regenerative heat exchanger - partic for gas turbine driven vehicles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1382876A true GB1382876A (en) | 1975-02-05 |
Family
ID=26216196
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB557172A Expired GB1382876A (en) | 1971-02-09 | 1972-02-07 | Regenerative heat exchanger devices |
Country Status (6)
Country | Link |
---|---|
US (1) | US3894579A (en) |
JP (1) | JPS506653B1 (en) |
DE (1) | DE2206109C3 (en) |
GB (1) | GB1382876A (en) |
IT (1) | IT947434B (en) |
SU (1) | SU553944A3 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0239145U (en) * | 1988-09-09 | 1990-03-15 | ||
US6983890B2 (en) * | 2002-01-21 | 2006-01-10 | Webasto Thermosysteme International Gmbh | Vehicle heating appliance with a valve in the fuel supply |
US20060054301A1 (en) * | 2004-02-19 | 2006-03-16 | Mcray Richard F | Variable area mass or area and mass species transfer device and method |
US20090101302A1 (en) * | 2007-10-17 | 2009-04-23 | Tupper Myron D | Dynamic heat exchanger |
US9353967B2 (en) * | 2010-02-03 | 2016-05-31 | Farshid Ahmady | Fluid heating apparatus |
US20130105105A1 (en) * | 2011-10-31 | 2013-05-02 | Harlod L. O'Brien | Bimetallic seal for air heaters |
DE102017204954A1 (en) * | 2017-03-23 | 2018-09-27 | MTU Aero Engines AG | FLOW MACHINE WITH ASSEMBLY ELEMENT |
US10502424B2 (en) * | 2017-08-10 | 2019-12-10 | General Electric Company | Volute combustor for gas turbine engine |
CA3050503C (en) | 2019-07-24 | 2020-05-26 | Inline Heat Recovery Inc. | Heat recovery unit |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2210916A (en) * | 1938-04-05 | 1940-08-13 | Sperry Gyroscope Co Inc | Automatic pilot for dirigible craft |
US2769912A (en) * | 1954-04-12 | 1956-11-06 | Phillips Petroleum Co | Shut-off valve |
GB1270797A (en) * | 1968-09-30 | 1972-04-12 | Lucas Industries Ltd | Fluid operated servomechanism |
-
1972
- 1972-02-07 GB GB557172A patent/GB1382876A/en not_active Expired
- 1972-02-08 US US224580A patent/US3894579A/en not_active Expired - Lifetime
- 1972-02-09 DE DE2206109A patent/DE2206109C3/en not_active Expired
- 1972-02-09 SU SU1745976A patent/SU553944A3/en active
- 1972-02-09 IT IT20386/72A patent/IT947434B/en active
- 1972-09-12 JP JP47013385A patent/JPS506653B1/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US3894579A (en) | 1975-07-15 |
IT947434B (en) | 1973-05-21 |
DE2206109B2 (en) | 1975-02-13 |
JPS506653B1 (en) | 1975-03-17 |
SU553944A3 (en) | 1977-04-05 |
DE2206109A1 (en) | 1972-08-17 |
DE2206109C3 (en) | 1975-09-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |