GB713436A - Improvements in or relating to axial-flow compressors - Google Patents

Improvements in or relating to axial-flow compressors

Info

Publication number
GB713436A
GB713436A GB6209/51A GB620951A GB713436A GB 713436 A GB713436 A GB 713436A GB 6209/51 A GB6209/51 A GB 6209/51A GB 620951 A GB620951 A GB 620951A GB 713436 A GB713436 A GB 713436A
Authority
GB
United Kingdom
Prior art keywords
pressure
valve
piston
engine
opening
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
GB6209/51A
Inventor
Adrian Albert Lombard
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB6209/51A priority Critical patent/GB713436A/en
Publication of GB713436A publication Critical patent/GB713436A/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
    • F04D27/0215Arrangements therefor, e.g. bleed or by-pass valves
    • 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
    • F04D27/0223Control schemes therefor
    • 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
    • F04D27/023Details or means for fluid extraction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/522Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps

Landscapes

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

Abstract

713,436. Axial-flow compressors. ROLLSROYCE, Ltd. March 5, 1952 [March 14, 1951] No. 6209/51. Class 110(1) [Also in Group XXIX] In a multi-stage axial-flow compressor, air is bled off from a later stage through a bleed valve, the opening of which is controlled by a pressuresensitive element which is loaded in one sense by a fluid pressure which is a function of the compressor rotational speed, and in the opposite sense by a force which is a function of the opening of the bleed valve. In a compressor forming part of a gas turbine engine, Fig. 3, air is bled from intermediate stages through ports 33 into annular chambers 31 and thence through ports 36 the opening of which is controlled by slide valves 37. The latter are connected by linkage 41 to a hydraulic ram 42. The ram piston 44 has a hollow stem 46 which is in communication with the inside of the ram cylinder 43 to the right of the piston head 47; thus the effective area of the right-hand side of the piston head is greater than that of the left-hand side. The delivery pressure of a swashplate-type fuel pump 13 is applied through a pipe 50 directly to the left-hand side of the head 47 and by way of a restriction 53 to the right hand side. A centrifugal pump formed integrally with the pump 13 develops a pressure which is a function of the rotational speed of the engine (since the pump is driven by the engine), the pressure being, applied through a pipe 60 to one side of a diaphragm 58, the suction pressure of pump 13 being applied to the other side through a pipe 59. The diaphragm 58 is connected by a rod 67 to a half-ball valve 69. Increase of engine speed produces an increase of fluid pressure loading tending to move the diaphragm 58 against the action of a spring 62 and thereby to lift the valve 69 from its seat, so venting the right-hand end of the cylinder 43 to the pump suction through duct 52 and pipe 59. The resultant pressure drop due to the restriction 53 causes the piston 44 to move to the right, thereby increasing the opening of bleed valves 37. until the resultant increase of the force exerted on the diaphragm 58 by the spring 62 due to the increased compression of the latter by the piston 44 returns the valve 69 towards its closed position. A lower limit to the range of engine speeds over which the bleed valves 37 are adjusted is set by a secondary spring 66 which exerts a load on the diaphragm 58 which is independent of the position of the piston 44. Below this lower limit of speed, the bleed valves are maintained fully open. Stator blades 112 of the compressor may be connected to the ram 42 by linkage 110 so that their pitch is adjusted in unison with the bleed valve opening. In the modification shown in Fig. 4, the diaphragm 58 is loaded by the pressure drop across an orifice 100. the area of which is controlled, so as to be proportional to the square root of the engine intake temperature, by a capsule 101 connected to a bulb 108 in the engine intake. The pressure fluid for this purpose is supplied by a positive displacement pump 104 driven by the engine, producing a flow through the orifice 100 which is proportional to the engine speed. Thus the pressure drop across the orifice 100 is proportional to the corrected engine speed, i.e., the actual engine speed divided by the square root of the engine intake temperature, and the bleed valve opening is consequently a function of the corrected speed. In a further embodiment. the bleed valves each comprise a piston valve sliding in a cylinder having ported walls and conveniently forming part of the compressor casing. That part of the cylinder on the side of the piston valve remote from the ports is closed and is connected by way of a restriction to a source of high pressure, for example the delivery duct of the compressor. Downstream of the restriction, a connection is made to a point of low pressure such as the atmosphere through a valve of which the opening is controlled by the hydraulic ram 42. As this valve is progressively opened by the ram, the pressure downstream of the restriction (i.e., the pressure in the closed end of the cylinder tending to keep the piston valve in the closed position) is progressively reduced, so that the bleed valve opening is progressively increased. The piston valve may be lightly spring loaded towards the open position. Specification 704,849 is referred to.
GB6209/51A 1951-03-14 1951-03-14 Improvements in or relating to axial-flow compressors Expired GB713436A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB6209/51A GB713436A (en) 1951-03-14 1951-03-14 Improvements in or relating to axial-flow compressors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB6209/51A GB713436A (en) 1951-03-14 1951-03-14 Improvements in or relating to axial-flow compressors

Publications (1)

Publication Number Publication Date
GB713436A true GB713436A (en) 1954-08-11

Family

ID=9810411

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6209/51A Expired GB713436A (en) 1951-03-14 1951-03-14 Improvements in or relating to axial-flow compressors

Country Status (1)

Country Link
GB (1) GB713436A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3201009A1 (en) * 1981-03-23 1982-09-30 Avco Corp., 06830 Greenwich, Conn. INTEGRATED MULTI-PLANE OPERATING SYSTEM FOR THE ADJUSTABLE BLADES AND THE AIR RELEASE VALVE OF A COMPRESSOR
WO2010078497A1 (en) * 2008-12-31 2010-07-08 Rolls-Royce North American Technologies, Inc. Variable pressure ratio compressor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3201009A1 (en) * 1981-03-23 1982-09-30 Avco Corp., 06830 Greenwich, Conn. INTEGRATED MULTI-PLANE OPERATING SYSTEM FOR THE ADJUSTABLE BLADES AND THE AIR RELEASE VALVE OF A COMPRESSOR
WO2010078497A1 (en) * 2008-12-31 2010-07-08 Rolls-Royce North American Technologies, Inc. Variable pressure ratio compressor
US8863529B2 (en) 2008-12-31 2014-10-21 Rolls-Royce North American Technologies, Inc. Variable pressure ratio compressor

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