GB811434A - Improvements in or relating to regenerative heat exchangers - Google Patents

Improvements in or relating to regenerative heat exchangers

Info

Publication number
GB811434A
GB811434A GB1067655A GB1067655A GB811434A GB 811434 A GB811434 A GB 811434A GB 1067655 A GB1067655 A GB 1067655A GB 1067655 A GB1067655 A GB 1067655A GB 811434 A GB811434 A GB 811434A
Authority
GB
United Kingdom
Prior art keywords
chamber
compressor
regenerator
air
thence
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
Application number
GB1067655A
Inventor
George John Huebner Jr
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.)
Old Carco LLC
Original Assignee
Chrysler Corp
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 Chrysler Corp filed Critical Chrysler Corp
Priority to GB1067655A priority Critical patent/GB811434A/en
Publication of GB811434A publication Critical patent/GB811434A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

811,434. Gas turbine plant. CHRYSLER CORPORATION. April 13, 1955, No. 10676/55. Class 110 (3). [Also in Group XIII] In a gas turbine plant in which combustion air is preheated in a rotary regenerator (see Group XIII) having a glass matrix 13, air is drawn through a converging inlet 11 of a centrifugal type compressor 10 and is forced by the rotor vanes 25 to a diffuser 29 leading to a chamber 31 and thence through the regenerator matrix in which it is preheated before being mixed with fuel and burned. Combustion gases from the combustion chambers (not shown) flow into a passage 36 and thence through a turbine 43 driving the compressor and a turbine 45 driving the power output shaft 48, before flowing into a chamber 42, the gases giving up heat to the regenerator matrix in passing therethrough to an exhaust chamber 51. Intake air after passing through the compressor rotor vanes 25 flows additionally to a radially extending portion 26 having a peripheral discharge opening 30 for creating a centrifugal head.
GB1067655A 1955-04-13 1955-04-13 Improvements in or relating to regenerative heat exchangers Expired GB811434A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1067655A GB811434A (en) 1955-04-13 1955-04-13 Improvements in or relating to regenerative heat exchangers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1067655A GB811434A (en) 1955-04-13 1955-04-13 Improvements in or relating to regenerative heat exchangers

Publications (1)

Publication Number Publication Date
GB811434A true GB811434A (en) 1959-04-08

Family

ID=9972223

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1067655A Expired GB811434A (en) 1955-04-13 1955-04-13 Improvements in or relating to regenerative heat exchangers

Country Status (1)

Country Link
GB (1) GB811434A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3251403A (en) * 1962-01-05 1966-05-17 Corning Glass Works Ceramic heat exchanger structures
US3407866A (en) * 1966-09-01 1968-10-29 Corning Glass Works Ceramic seals and bearing members

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3251403A (en) * 1962-01-05 1966-05-17 Corning Glass Works Ceramic heat exchanger structures
US3407866A (en) * 1966-09-01 1968-10-29 Corning Glass Works Ceramic seals and bearing members

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