GB698783A - Compressor apparatus - Google Patents

Compressor apparatus

Info

Publication number
GB698783A
GB698783A GB2982051A GB2982051A GB698783A GB 698783 A GB698783 A GB 698783A GB 2982051 A GB2982051 A GB 2982051A GB 2982051 A GB2982051 A GB 2982051A GB 698783 A GB698783 A GB 698783A
Authority
GB
United Kingdom
Prior art keywords
stages
stage
ratio
equal
gas turbine
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
GB2982051A
Inventor
Max Adolf Mueller
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.)
INCONEX HANDELSGESELLSCHAFT M
Original Assignee
INCONEX HANDELSGESELLSCHAFT M
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 INCONEX HANDELSGESELLSCHAFT M filed Critical INCONEX HANDELSGESELLSCHAFT M
Priority to GB2982051A priority Critical patent/GB698783A/en
Publication of GB698783A publication Critical patent/GB698783A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
    • F04D25/163—Combinations of two or more pumps ; Producing two or more separate gas flows driven by a common gearing arrangement

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

698,783. Gas turbine plant; axial-flow compressors. INCONEX HANDELSGES. FOR INDUSTRIELLE PRODUKTE-KONSTRUKTIONENEXPORT. Dec. 20, 1951, No. 29820/51. Classes 110(i) and 110(iii) A compressor supplying air to the combustion chambers of a gas turbine 5 comprises two identical L.P. stages 1, 2 and an H.P. stage 3 of the same construction, the H.P. stage being directly driven by the turbine, and the L.P. stages, which are arranged .one at each side of the H.P. stage, being driven through gearing 6, 7. The H.P. and L.P. stages are of identical dimensions. The ratio between the rotational speeds of the H.P. and L.P. stages is equal to #T 2 /T 1 , and the ratio of the intake volume of the H.P. stage to that of the L.P. stages is equal to ¢#T 2 /T 1 , where T 1 and T 2 are the respective intake temperatures of the L.P. and H.P. stages.
GB2982051A 1951-12-20 1951-12-20 Compressor apparatus Expired GB698783A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2982051A GB698783A (en) 1951-12-20 1951-12-20 Compressor apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2982051A GB698783A (en) 1951-12-20 1951-12-20 Compressor apparatus

Publications (1)

Publication Number Publication Date
GB698783A true GB698783A (en) 1953-10-21

Family

ID=10297706

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2982051A Expired GB698783A (en) 1951-12-20 1951-12-20 Compressor apparatus

Country Status (1)

Country Link
GB (1) GB698783A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3121526A (en) * 1960-08-25 1964-02-18 Rolls Royce Gas turbine engines
US3826587A (en) * 1973-04-10 1974-07-30 Ingersoll Rand Co Centrifugal gas compressor unit
GB2309745A (en) * 1996-02-02 1997-08-06 John Peter Miller Multi-stage compressor
GB2321502A (en) * 1997-01-24 1998-07-29 Europ Gas Turbines Ltd Turbocharger arrangement

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3121526A (en) * 1960-08-25 1964-02-18 Rolls Royce Gas turbine engines
US3826587A (en) * 1973-04-10 1974-07-30 Ingersoll Rand Co Centrifugal gas compressor unit
DE2413674A1 (en) * 1973-04-10 1974-11-07 Ingersoll Rand Co RADIAL TURBO COMPRESSOR
GB2309745A (en) * 1996-02-02 1997-08-06 John Peter Miller Multi-stage compressor
GB2321502A (en) * 1997-01-24 1998-07-29 Europ Gas Turbines Ltd Turbocharger arrangement
GB2321502B (en) * 1997-01-24 2001-02-07 Europ Gas Turbines Ltd Turbocharger arrangement

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