GB2123895B - Controller for controlling turbine inlet vanes for varying the inlet nozzle area to the turbine of a turbo-compressor - Google Patents

Controller for controlling turbine inlet vanes for varying the inlet nozzle area to the turbine of a turbo-compressor

Info

Publication number
GB2123895B
GB2123895B GB08310185A GB8310185A GB2123895B GB 2123895 B GB2123895 B GB 2123895B GB 08310185 A GB08310185 A GB 08310185A GB 8310185 A GB8310185 A GB 8310185A GB 2123895 B GB2123895 B GB 2123895B
Authority
GB
United Kingdom
Prior art keywords
turbine
inlet
turbo
compressor
varying
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
GB08310185A
Other versions
GB2123895A (en
GB8310185D0 (en
Inventor
Norbert Lewis Osborn
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.)
Individual
Original Assignee
Individual
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
Priority claimed from PCT/US1979/000317 external-priority patent/WO1980002585A1/en
Application filed by Individual filed Critical Individual
Priority to GB08310185A priority Critical patent/GB2123895B/en
Publication of GB8310185D0 publication Critical patent/GB8310185D0/en
Publication of GB2123895A publication Critical patent/GB2123895A/en
Application granted granted Critical
Publication of GB2123895B publication Critical patent/GB2123895B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/24—Control of the pumps by using pumps or turbines with adjustable guide vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies
GB08310185A 1979-05-14 1983-04-14 Controller for controlling turbine inlet vanes for varying the inlet nozzle area to the turbine of a turbo-compressor Expired GB2123895B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08310185A GB2123895B (en) 1979-05-14 1983-04-14 Controller for controlling turbine inlet vanes for varying the inlet nozzle area to the turbine of a turbo-compressor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/US1979/000317 WO1980002585A1 (en) 1979-05-14 1979-05-14 Turbocharger and adaptations thereof
GB08310185A GB2123895B (en) 1979-05-14 1983-04-14 Controller for controlling turbine inlet vanes for varying the inlet nozzle area to the turbine of a turbo-compressor

Publications (3)

Publication Number Publication Date
GB8310185D0 GB8310185D0 (en) 1983-05-18
GB2123895A GB2123895A (en) 1984-02-08
GB2123895B true GB2123895B (en) 1984-08-01

Family

ID=10541126

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08310185A Expired GB2123895B (en) 1979-05-14 1983-04-14 Controller for controlling turbine inlet vanes for varying the inlet nozzle area to the turbine of a turbo-compressor

Country Status (1)

Country Link
GB (1) GB2123895B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3438175A1 (en) * 1984-10-18 1986-04-24 Robert Bosch Gmbh, 7000 Stuttgart DEVICE FOR CONTROLLING THE CHARGE PRESSURE OF AN INTERNAL COMBUSTION ENGINE
DE19719630C2 (en) * 1997-05-09 1999-02-25 Daimler Benz Ag Method for regulating a supercharged internal combustion engine and device for carrying out the method
FR2987874B1 (en) * 2012-03-09 2015-10-09 Snecma COVER FOR COMPRESSOR, COMPRESSOR AND ASSOCIATED TURBOREACTORS
US9103304B2 (en) * 2012-05-30 2015-08-11 GM Global Technology Operations LLC Integrated intake manifold and compressor

Also Published As

Publication number Publication date
GB2123895A (en) 1984-02-08
GB8310185D0 (en) 1983-05-18

Similar Documents

Publication Publication Date Title
IL54223A (en) Variable outlet area exhaust nozzle particularly of a gas turbine
GB2090333B (en) Gas turbine engine shroud/blade tip control
JPS5551990A (en) Controlled flow gas compressor
GB2074655B (en) Particle separator for the inlet of a gas turbine engine
GB2015085B (en) Cooling air control valve for a gas turbine engine
GB2036882A (en) Turbine shroud assembly
GB2019945A (en) Partial span inlet guide vane for crossconnected gas turbine engines
IL57122A (en) System for controlling simulated parameter such as burner pressure for gas turbine engine
JPS5647628A (en) Controller for gas turbine engine
GB2016092A (en) Blade-retainer for the rotor of a turbo machine particularly an axial flow turbine
GB2016597B (en) Controlling guide vane angle of an axial-flow compressor of a gas turbine engine
GB2014249B (en) Steam turbine overspeed protection controller
JPS51146613A (en) Variable area nozzle for gas turbine engine
JPS569607A (en) Turbine controller
JPS5575540A (en) Fuel controller for turbine engine
JPS5560609A (en) Speed controller for steam turbine
JPS5677524A (en) Controller for gas turbine
GB2017229B (en) Guides vanes for gas turbine enginess
ZA782434B (en) Valve assembly for controlling the flow of abrasive material in a duct
GB2025537B (en) Air delivery system for regulating thermal growth of turbine shroud
DE3066075D1 (en) Device for fixing blades to the rotor of the compressor of a turbojet plant
IL58698A0 (en) Pressure controller for dual purpose steam turbine power plant
GB2123895B (en) Controller for controlling turbine inlet vanes for varying the inlet nozzle area to the turbine of a turbo-compressor
GB1503757A (en) Automatic process for the optimum regulation of aircraft fuel flow
GB2057577B (en) Gas turbine fuel flow control

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930514