GB745905A - Improvements in or relating to pressure-ratio sensitive mechanisms - Google Patents

Improvements in or relating to pressure-ratio sensitive mechanisms

Info

Publication number
GB745905A
GB745905A GB23284/52A GB2328452A GB745905A GB 745905 A GB745905 A GB 745905A GB 23284/52 A GB23284/52 A GB 23284/52A GB 2328452 A GB2328452 A GB 2328452A GB 745905 A GB745905 A GB 745905A
Authority
GB
United Kingdom
Prior art keywords
pressure
orifice
orifices
area
responsive device
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
GB23284/52A
Inventor
Richard Harvey Webb
Christopher Linley Johnson
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 GB23284/52A priority Critical patent/GB745905A/en
Publication of GB745905A publication Critical patent/GB745905A/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
    • F04D27/0246Surge control by varying geometry within the pumps, e.g. by adjusting vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Abstract

745,905. Fluid-pressure servomotor-control systems. ROLLS-ROYCE, Ltd. Nov. 30, 1953 [Sept. 16, 1952], No. 23284/52. Class 135. A mechanism responsive to the ratio between the pressure at two sources of gaseous pressure comprises a conduit connected to one of the sources having two restrictive orifices in series of which at least the downstream orifice is choked and one of the orifices is of variable area and a pressure-responsive device having a first area subjected to the pressure at the higher source, a second area subjected to the pressure at the lower source or the pressure between the orifices, whichever is the lower, and a third area subjected to the pressure at the lower source or the pressure between the orifices, whichever is the higher, the pressure load on the first and second areas being in the same sense and opposite to that on the third area, and the pressure-responsive device being connected to the variable area orifice so that on movement of the pressure-responsive device due to out-ofbalance pressure loads thereon the variable area orifice is adjusted to restore the pressureresponsive device to a state of balance. As shown, the invention is applied to adjust the angle of guide vanes 23 of a compressor 2 in accordance with the ratio between its inlet and outlet pressures. The outlet pressure passing through a conduit 1 having a fixed restrictive orifice 3 in series with a variable choked orifice 4 opening to the atmosphere and controlled by a needle valve 5 connected to the piston 16 of a servomotor 17 supplied with operating fluid directly to its left-hand space 18 through a pipe 19 and indirectly to its right-hand space 20 through a restriction 21. Exhaust from the space 20 is controlled by a leak-off valve 15 carried by a lever 14 connected to the rod 12 of a pressure-responsive device 13 comprising a pair of diaphragms 6, 9. Compressor outlet pressure acts on the outer face of the diaphragm 6, the pressure between the orifices 3, 4 on the outer face of the diaphragm 9 and compressor inlet pressure, i.e. atmospheric pressure, on the inner faces of the diaphragms. Should, e.g., compressor outlet pressure increase, the pressure between the orifices will also increase and acting on the larger area diaphragm will open the leakoff valve 15 to relieve pressure in the space 20 to permit rightward movement of the piston 16 to increase the opening of the orifice 4 and at the same time adjust the angle of the guide vanes 23 through a mechanical linkage 24. The increased opening of the orifice 4 reduces the pressure beneath the diaphragm 9 and restores the pressure-responsive device to a state of balance. The diaphragms may be replaced by a pair of interconnected pistons or by a differential piston. Specification 736,003 is referred to.
GB23284/52A 1952-09-16 1952-09-16 Improvements in or relating to pressure-ratio sensitive mechanisms Expired GB745905A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB23284/52A GB745905A (en) 1952-09-16 1952-09-16 Improvements in or relating to pressure-ratio sensitive mechanisms

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB23284/52A GB745905A (en) 1952-09-16 1952-09-16 Improvements in or relating to pressure-ratio sensitive mechanisms

Publications (1)

Publication Number Publication Date
GB745905A true GB745905A (en) 1956-03-07

Family

ID=10193169

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23284/52A Expired GB745905A (en) 1952-09-16 1952-09-16 Improvements in or relating to pressure-ratio sensitive mechanisms

Country Status (1)

Country Link
GB (1) GB745905A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1046352B (en) * 1953-12-30 1958-12-11 Thueringisches Kunstfaserwerk Flow regulator
US3058695A (en) * 1956-09-03 1962-10-16 Havilland Engine Co Ltd Auxiliary gas supply from gas turbine engine and aircraft fitted therewith
US3083892A (en) * 1956-11-01 1963-04-02 Havilland Engine Co Ltd Control of variable pitch stator blades or vanes in axial flow machines

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1046352B (en) * 1953-12-30 1958-12-11 Thueringisches Kunstfaserwerk Flow regulator
US3058695A (en) * 1956-09-03 1962-10-16 Havilland Engine Co Ltd Auxiliary gas supply from gas turbine engine and aircraft fitted therewith
US3083892A (en) * 1956-11-01 1963-04-02 Havilland Engine Co Ltd Control of variable pitch stator blades or vanes in axial flow machines

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