CH313856A - Erwärmungseinheit für Brennkraftturbinen - Google Patents

Erwärmungseinheit für Brennkraftturbinen

Info

Publication number
CH313856A
CH313856A CH313856DA CH313856A CH 313856 A CH313856 A CH 313856A CH 313856D A CH313856D A CH 313856DA CH 313856 A CH313856 A CH 313856A
Authority
CH
Switzerland
Prior art keywords
internal combustion
heating unit
combustion turbines
turbines
heating
Prior art date
Application number
Other languages
English (en)
Inventor
Hryniszak Waldemar
Original Assignee
Parsons & Co Ltd C A
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 Parsons & Co Ltd C A filed Critical Parsons & Co Ltd C A
Publication of CH313856A publication Critical patent/CH313856A/de

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • 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

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)
  • Solid-Fuel Combustion (AREA)
  • Air Supply (AREA)
  • Air-Conditioning For Vehicles (AREA)
CH313856D 1952-06-23 1952-12-23 Erwärmungseinheit für Brennkraftturbinen CH313856A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB15784/52A GB749904A (en) 1952-06-23 1952-06-23 Improvements in and relating to heating units for combustion turbines

Publications (1)

Publication Number Publication Date
CH313856A true CH313856A (de) 1956-05-15

Family

ID=10065401

Family Applications (1)

Application Number Title Priority Date Filing Date
CH313856D CH313856A (de) 1952-06-23 1952-12-23 Erwärmungseinheit für Brennkraftturbinen

Country Status (5)

Country Link
US (1) US2795109A (de)
CH (1) CH313856A (de)
DE (1) DE952951C (de)
FR (1) FR1078870A (de)
GB (1) GB749904A (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3220183A (en) * 1954-03-22 1965-11-30 Garrett Corp Engine
DE1064296B (de) * 1957-09-17 1959-08-27 George Royce Hoffmann Strahltriebwerk fuer Flugzeuge, Geschosse od. dgl.
DE1147803B (de) * 1959-05-22 1963-04-25 Bmw Triebwerkbau Ges M B H Kraftstoffoerderung innerhalb der Laeuferwelle von Rotationszerstaeubern fuer Brennkammern, insbesondere fuer Gasturbinen
US3143166A (en) * 1960-01-20 1964-08-04 Williams Res Corp Heat exchanger for gas turbines
GB1039677A (en) * 1963-07-10 1966-08-17 Rolls Royce Combustion chamber for a gas turbine engine
GB1055956A (en) * 1964-10-23 1967-01-25 Rolls Royce Gas turbine engine
US4767656A (en) * 1984-01-09 1988-08-30 The Boeing Company Composite material structure with integral fire protection
AU2002951688A0 (en) * 2002-09-25 2002-10-17 Dbt Diesel Pty Limited Turbocharged compression ignition engine
GB2428465A (en) * 2005-07-19 2007-01-31 Thomas Tsoi Hei Ma A system for dispensing EGR in a reciprocating internal combustion engine
GB201801165D0 (en) * 2018-01-24 2018-03-07 Rolls Royce Plc Oil pipe assembly

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US981978A (en) * 1901-02-18 1911-01-17 Rockaway Automobile Company Internal-combustion motor.
US1516108A (en) * 1922-08-21 1924-11-18 Ljungstroms Angturbin Ab Regenerative air preheater
US2399394A (en) * 1940-12-07 1946-04-30 Bbc Brown Boveri & Cie Pressure exchanger
US2667034A (en) * 1946-04-01 1954-01-26 Power Jets Res & Dev Ltd Air turbine power plant having rotary regenerator to transfer heat from an afterburner to the motive fluid
US2551112A (en) * 1946-09-05 1951-05-01 Daniel And Florence Guggenheim Premixing combustion chamber
US2630678A (en) * 1947-08-18 1953-03-10 United Aircraft Corp Gas turbine power plant with fuel injection between compressor stages

Also Published As

Publication number Publication date
FR1078870A (fr) 1954-11-24
US2795109A (en) 1957-06-11
DE952951C (de) 1956-11-22
GB749904A (en) 1956-06-06

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