GB807071A - Improvements in or relating to gas compressing plant - Google Patents

Improvements in or relating to gas compressing plant

Info

Publication number
GB807071A
GB807071A GB2455255A GB2455255A GB807071A GB 807071 A GB807071 A GB 807071A GB 2455255 A GB2455255 A GB 2455255A GB 2455255 A GB2455255 A GB 2455255A GB 807071 A GB807071 A GB 807071A
Authority
GB
United Kingdom
Prior art keywords
pressure
compressor
pressure compressor
valve
pass valve
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
GB2455255A
Inventor
Neil Milligan Clark
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB2455255A priority Critical patent/GB807071A/en
Publication of GB807071A publication Critical patent/GB807071A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0207Surge control by bleeding, bypassing or recycling fluids

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Abstract

807,071. Centrifugal compressors; gas turbine plant POWER JETS (RESEARCH & DEVELOPMENT) Ltd. Aug. 3, 1956 [Aug. 26, 1955], No. 24552/55. Addition to 774,391. Classes 110 (1) and 110 (3). [Also in Group XXIX] A compressor plant comprises separate low and high-pressure compressors connected in series and driven by separate turbines, the low-pressure compressor also supplying gas to the turbines by way of a heating system, and surging is prevented by a by-pass at the outlet of the high-pressure compressor, the by-pass valve being controlled by a pneumatic differential relay responsive to two gas pressures sensed by tappings at the high-pressure compressor. In the gas turbine plant described in the parent Specification, wherein the output from a lowpressure centrifugal air compressor is divided, part of it going through a two-stage highpressure centrifugal air compressor to the output and part directly to the combustion chamber and from there to the two separate turbines which separately drive the compressors; the surge-preventing by-pass valve 17, Fig. 4, is actuated pneumatically instead of hydraulically. The high-pressure compressor runs at a constant governor-controlled speed. Pressure tappings 28, 29 at the inlet and throat of a venturi flow meter situated at the intake or delivery of the high-pressure compressor communicate with corrugated diaphragms or, as shown, bellows 32, 33 of differing diameters, connected in opposition to a lever 40 pivoted about a fulcrum 41. A valve 37 carried by the lever 40 throttles the escape of air through a nozzle at the end of a pipe 38. Variations in the leak-off result in corresponding variations in the pressure in an air supply pipe 21 downstream of a restriction 39. This pressure is applied to a diaphragm 44 to operate the by-pass valve 17. A device 35 can alter the pressure to provide compensation for temperature variations sensed at 36. At normal rates of flow, the venturi is partly bypassed by a valve 31 which lifts at a load value just above the operating range of the surgepreventing control. The pipe 21 is connected to the outlet of the low-pressure compressor, and may incorporate a cooler. The venturi may be omitted, the flow measuring tappings then being taken from static points in an outlet duct wall or from a yawmeter. The yawmeter tapping points may comprise sensing holes 26, 27, Fig. 2, in small diameter tubes 25 in the leading edges of separate diffuser vanes 24 of the second-stage high-pressure compressor. The tubes 25 are adjustable to bring the holes 26, 27 to the required positions. A number of such pairs of holes may be disposed around the circumference of the compressor. A second and larger pneumatic relay may be interposed between the pneumatic relay and the by-pass valve 17. Mechanical or pneumatic feedback may be used.
GB2455255A 1955-08-26 1955-08-26 Improvements in or relating to gas compressing plant Expired GB807071A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2455255A GB807071A (en) 1955-08-26 1955-08-26 Improvements in or relating to gas compressing plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2455255A GB807071A (en) 1955-08-26 1955-08-26 Improvements in or relating to gas compressing plant

Publications (1)

Publication Number Publication Date
GB807071A true GB807071A (en) 1959-01-07

Family

ID=10213415

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2455255A Expired GB807071A (en) 1955-08-26 1955-08-26 Improvements in or relating to gas compressing plant

Country Status (1)

Country Link
GB (1) GB807071A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044683A (en) * 1960-01-18 1962-07-17 Schwitzer Corp Pressure control for turbochargers
FR2389785A1 (en) * 1977-05-06 1978-12-01 Alsthom Atlantique Centrifugal compressor control system - has anti-pumping valve actuated by signal from flow direction sensing probe in outlet
CN112664326A (en) * 2020-12-11 2021-04-16 中国航空工业集团公司金城南京机电液压工程研究中心 High-low pressure bleed air system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044683A (en) * 1960-01-18 1962-07-17 Schwitzer Corp Pressure control for turbochargers
FR2389785A1 (en) * 1977-05-06 1978-12-01 Alsthom Atlantique Centrifugal compressor control system - has anti-pumping valve actuated by signal from flow direction sensing probe in outlet
CN112664326A (en) * 2020-12-11 2021-04-16 中国航空工业集团公司金城南京机电液压工程研究中心 High-low pressure bleed air system
CN112664326B (en) * 2020-12-11 2022-09-06 中国航空工业集团公司金城南京机电液压工程研究中心 High-low pressure bleed air system

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