SU553944A3 - Регенератор - Google Patents

Регенератор

Info

Publication number
SU553944A3
SU553944A3 SU1745976A SU1745976A SU553944A3 SU 553944 A3 SU553944 A3 SU 553944A3 SU 1745976 A SU1745976 A SU 1745976A SU 1745976 A SU1745976 A SU 1745976A SU 553944 A3 SU553944 A3 SU 553944A3
Authority
SU
USSR - Soviet Union
Prior art keywords
matrix
channels
generator according
regenerator
february
Prior art date
Application number
SU1745976A
Other languages
English (en)
Inventor
Бриль Морис
Original Assignee
Сосьете Аноним Де Веикюль Эндюстриель Эд"Экипман Меканик Савием (Фирма)
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
Priority claimed from FR7104206A external-priority patent/FR2126940A1/fr
Priority claimed from FR7203350A external-priority patent/FR2170815A2/fr
Application filed by Сосьете Аноним Де Веикюль Эндюстриель Эд"Экипман Меканик Савием (Фирма) filed Critical Сосьете Аноним Де Веикюль Эндюстриель Эд"Экипман Меканик Савием (Фирма)
Application granted granted Critical
Publication of SU553944A3 publication Critical patent/SU553944A3/ru

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases
    • F02C7/10Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases
    • F02C7/10Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
    • F02C7/105Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers of the rotary type
    • 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
    • F28D19/00Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04Regenerative 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
    • 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
    • F28D19/00Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04Regenerative 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
    • F28D19/041Regenerative 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
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/009Heat exchange having a solid heat storage mass for absorbing heat from one fluid and releasing it to another, i.e. regenerator
    • Y10S165/013Movable heat storage mass with enclosure
    • Y10S165/014Reciprocated linearly

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

(54) РЕГЕНЕРАТОР
и прижимаетс  к матрице силой давлеии  газа поверхностью 11. Сегмент 9 может быть выполнен из биметаллической ленты, имеющей наружную часть 12 менее расшир ющуюс , чем внутренн   часть 13, что позвол ет достаточно точно отрегулировать степень открыти  сегмента и, соответственно, ликвидировать зазоры между каналами и матрицей, возникающие при температурных деформаци х последних.

Claims (5)

1. Регенератор, например, дл  газотурбинного двигател , содержащий корпус со снабженными уплотнением каналами гор чих и холодных газов, лр-имыкающими к вращающейс , цилиндрической, проницаемой в радиальном и герметичной в осевом направлени х матрице, отличающийс  тем, что, е целью интенсификации теплообмена, отверсти  каналов расположены вдоль оси матрицы , по обе стороны от нее, смежными парами из входного (выходного) отверсти  канала гор чего газа и смежного с ним выходного (входного) отверсти  канала холодного газа, а матрица соединена с механизмом ее осевого перемещени .
2.Регенератор по п. 1, отличающийс  тем, что уплотнение между каналами и матрицей выполнено в виде круглых колец, составленных из сегментов и установленных в
5 выемках стенок каналов.
3.Ренератор по п. 3, отличающийс  тем, что сегменты выполнены в виде концентрических биметаллических пластин.
4.Регенератор по п. 1, отличающийс  0 тем, что, с целью обеспечени  вращени  матрицы , часть подвод щих каналов установлена тангенциально по отношению к ее цилиндрической поверхности.
5.Регенератор по п. 1, отличающийс  5 тем, что механизм осевого перемещени  матрицы выполнен в виде полых камер, расположенных по обоим торцам матрицы и соединенных трубопроводами через реверсивный клапан с источником избыточного давлени .
Приоритет исчисл ть по пп. 1-3 от 9 феврал  1971 г, в соответствии с за вкой № 7104206; .по пп. 4-5 - от 1 феврал  1972 г. в соответствии с за вкой № 7203350, поданными в Патентное Ведомство Франции.
Источник информации, прин тый во внимание при экспертизе:
1. Авторское свидетельство № 182278, F23L 15/02, 1966.
Фиг.
ЧигЗ
SU1745976A 1971-02-09 1972-02-09 Регенератор SU553944A3 (ru)

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
SU553944A3 true SU553944A3 (ru) 1977-04-05

Family

ID=26216196

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1745976A SU553944A3 (ru) 1971-02-09 1972-02-09 Регенератор

Country Status (6)

Country Link
US (1) US3894579A (ru)
JP (1) JPS506653B1 (ru)
DE (1) DE2206109C3 (ru)
GB (1) GB1382876A (ru)
IT (1) IT947434B (ru)
SU (1) SU553944A3 (ru)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0239145U (ru) * 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 (de) * 2017-03-23 2018-09-27 MTU Aero Engines AG Strömungsmaschine mit montageelement
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
DE2206109B2 (de) 1975-02-13
DE2206109A1 (de) 1972-08-17
JPS506653B1 (ru) 1975-03-17
US3894579A (en) 1975-07-15
DE2206109C3 (de) 1975-09-25
GB1382876A (en) 1975-02-05
IT947434B (it) 1973-05-21

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