CA2644938A1 - System for generating power in a pipeline - Google Patents

System for generating power in a pipeline Download PDF

Info

Publication number
CA2644938A1
CA2644938A1 CA 2644938 CA2644938A CA2644938A1 CA 2644938 A1 CA2644938 A1 CA 2644938A1 CA 2644938 CA2644938 CA 2644938 CA 2644938 A CA2644938 A CA 2644938A CA 2644938 A1 CA2644938 A1 CA 2644938A1
Authority
CA
Canada
Prior art keywords
rotary turbine
gas
bypass line
inline
flow control
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.)
Abandoned
Application number
CA 2644938
Other languages
French (fr)
Inventor
Del Borle
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
Application filed by Individual filed Critical Individual
Priority to CA 2644938 priority Critical patent/CA2644938A1/en
Publication of CA2644938A1 publication Critical patent/CA2644938A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B13/00Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17DPIPE-LINE SYSTEMS; PIPE-LINES
    • F17D1/00Pipe-line systems
    • F17D1/02Pipe-line systems for gases or vapours
    • F17D1/04Pipe-line systems for gases or vapours for distribution of gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2220/00Application
    • F05B2220/60Application making use of surplus or waste energy
    • F05B2220/602Application making use of surplus or waste energy with energy recovery turbines
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B10/00Integration of renewable energy sources in buildings
    • Y02B10/50Hydropower in dwellings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Control Of Turbines (AREA)

Abstract

A system for generating power includes an inline rotary turbine having an input and an output connected to a gas pipeline, such that gas flowing through the gas pipeline rotates the rotary turbine. A generator is connected to the inline rotary turbine for generating power.
A bypass line has an input connected to the input of the rotary turbine and an output connected to the output of the rotary turbine. The bypass line has at least one of an electronically controlled flow control valve and a manually controlled flow control valve.

Description

TITLE
[0001] System for generating power in a pipeline FIELD
[0002] Power generation for a pipeline .
BACKGROUND
[0003] U.S. patent no. 6,537,018 describes a rotational power transfer device.
SUMMARY
[0004] There is provided a system for generating power, comprising an inline rotary turbine having an input and an output connected to a gas pipeline, such that gas flowing through the gas pipeline rotates the rotary turbine. A generator is connected to the inline rotary turbine for generating power. A bypass line has an input connected to the input of the rotary turbine and an output connected to the output of the rotary turbine.
The bypass line has at least one of an electronically controlled flow control valve and a manually controlled flow control valve.
[0005] These and other features will become more apparent from the following description in which reference is made to the appended drawings, the drawings are for the purpose of illustration only and are not intended to be in any way limiting, wherein:
FIG. 1 is a schematic view of a system for generating power.
FIG. 2 is a side elevation view in section of an inline rotary turbine.
I)ETAILED DESCRIPTION
[0006] A system for generating power generally identified by reference numeral 10, will now be described with reference to FIG. 1 and 2.
[0007] Referring to FIG. 1, system for generating power 10 includes an inline rotary turbine 12 having, referring to FIG. 2, an input 14 and an output 16 connected to a gas pipeline 18 as shown in FIG. 1, such that gas flowing through gas pipeline 18 rotates the rotary turbine about an axis that is offset from the axis of gas pipeline 18.
Referring to FIG.

2, rotary turbine 12 includes a rotor 20 and spring-loaded vanes 21 that are movable between an extended position and a retracted position. Radial vanes 21 are biased by springs 23 toward the extended position.
[0008] Referring to FIG. 1, a generator 22 is connected to inline rotary turbine 12 for generating power. There is a bypass line 24 that has an input 26 connected to input 14 of rotary turbine 12 and an output 28 connected to output 16 of rotary turbine 12. Bypass line is connected to gas pipeline 18 and is used to divert a portion of gas flow so that the portion of the gas flow bypasses inline rotary turbine 12. Bypass line 24 has a flow control valve, such as two manually controlled flow control valves 30 and an electronically controlled flow control valve 32 to selectively control the portion of gas flow passing through bypass line 24 and thus control the speed of turbine 12. Either one or both of generator 22 and turbine 12 rnay have a rotation sensor 34 to determine whether the optimal operating speed for turbine 12 is being achieved. Rotation sensor 34 is preferably positioned on one of the inline rotary turbine 12 as shown in FIG. 1 or generator 22. Flow control valve 32 is electronically actuated, and a controller 36 is provided that receives data from rotation sensor 34 and electronically actuates flow control valve 32 to divert gas flow through bypass line 24 in accordance with a flow control strategy that keeps the rotations per minute of the inline rotary turbine within a preselected range. In addition to the embodiment described above, these readings may also be displayed for manual control, or both.
[0009] The system is connected to the outlet of a gas well in order to use the pressure and flow of the gas to drive the vane-type motor. This motion is used to drive a generator to generate power. The speed of the motor is controlled with a bypass control valve, which may be controlled either manually or electronically. The power generated can be used on site, and any remaining power can be sold into the power grid without consuming any gas.
[0010] In this patent document, the word "comprising" is used in its non-limiting sense to rnean that items following the word are included, but items not specifically mentioned are not excluded. A reference to an element by the indefinite article "a" does not exclude the possibility that more than one of the element is present, unless the context clearly requires that there be one and only one of the elements.
[0011] The following claims are to be understood to include what is specifically illustrated and described above, what is conceptually equivalent, and what can be obviously substituted. Those skilled in the art will appreciate that various adaptations and modifications of the described embodiments can be configured without departing from the scope of the claims. The illustrated embodiments have been set forth only as examples and should not be taken as limiting the invention. It is to be understood that, within the scope of the following claims, the invention may be practiced other than as specifically illustrated and described.

Claims (4)

1. A system for generating power, comprising:
an inline rotary turbine having an input and an output connected to a gas pipeline, such that gas flowing through the gas pipeline rotates the rotary turbine;
a generator connected to the inline rotary turbine for generating power;
a bypass line connected to the gas pipeline for diverting a portion of gas flow so that portion of the gas flow bypasses the inline rotary turbine, the bypass line having a flow control valve, for selectively controlling the portion of gas flow passing through the bypass line.
2. The system of Claim 1, wherein a rotation sensor is positioned on one of the inline rotary turbine or the generator, the flow control valve is electronically actuated, and a controller is provided which receives data from the rotation sensor and electronically actuates the flow control valve to divert gas flow through the bypass line in accordance with a flow control strategy that keeps the rotations per minute of the inline rotary turbine within a preselected range.
3. The system of Claim 1, wherein the gas pipeline has an axis and the inline rotary turbine is axially offset.
4. The system of Claim 3, wherein the inline rotary turbine has radial vanes that are movable between an extended position and a retracted position, the radial vanes being biased by springs toward the extended position.
CA 2644938 2008-11-12 2008-11-12 System for generating power in a pipeline Abandoned CA2644938A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA 2644938 CA2644938A1 (en) 2008-11-12 2008-11-12 System for generating power in a pipeline

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA 2644938 CA2644938A1 (en) 2008-11-12 2008-11-12 System for generating power in a pipeline

Publications (1)

Publication Number Publication Date
CA2644938A1 true CA2644938A1 (en) 2010-05-12

Family

ID=42168162

Family Applications (1)

Application Number Title Priority Date Filing Date
CA 2644938 Abandoned CA2644938A1 (en) 2008-11-12 2008-11-12 System for generating power in a pipeline

Country Status (1)

Country Link
CA (1) CA2644938A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2664786A1 (en) * 2012-05-16 2013-11-20 Energreen AS Fluid regulating valve
ITMO20130051A1 (en) * 2013-02-27 2014-08-28 Lorenzo Ferioli "REGULATION VALVE WITH ENERGY RECOVERY"
WO2015176145A1 (en) * 2014-05-19 2015-11-26 Atlas Copco Airpower, Naamloze Vennootschap Method for expanding a gas flow and device thereby applied
GB2534377A (en) * 2015-01-21 2016-07-27 Zeropex Group Ltd Water treatment apparatus and method
US20220221316A1 (en) * 2019-05-23 2022-07-14 Electro Mechanical Developments Limited Fluid Monitoring Apparatus

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2664786A1 (en) * 2012-05-16 2013-11-20 Energreen AS Fluid regulating valve
WO2013171253A1 (en) * 2012-05-16 2013-11-21 Energreen As Fluid regulating valve
CN104428529A (en) * 2012-05-16 2015-03-18 恩尔格林有限公司 Fluid regulating valve
ITMO20130051A1 (en) * 2013-02-27 2014-08-28 Lorenzo Ferioli "REGULATION VALVE WITH ENERGY RECOVERY"
WO2014132187A3 (en) * 2013-02-27 2015-01-22 Gattavari Claudio Angelo Adjustment valve with energy recovery
US10458554B2 (en) 2013-02-27 2019-10-29 Loclain S.R.L. Adjustment valve with energy recovery
KR20170008282A (en) * 2014-05-19 2017-01-23 아틀라스 캅코 에어파워, 남로체 벤누트삽 Method for expanding a gas flow and device thereby applied
BE1021896B1 (en) * 2014-05-19 2016-01-25 Atlas Copco Airpower Naamloze Vennootschap METHOD FOR LETTING A GAS RATE EXPANDED AND A DEVICE APPLIED THEREOF
CN106414915A (en) * 2014-05-19 2017-02-15 阿特拉斯·科普柯空气动力股份有限公司 Method for expanding a gas flow and device thereby applied
US20170096897A1 (en) * 2014-05-19 2017-04-06 Atlas Copco Airpower, Naamloze Vennootschap Method for expanding a gas flow and device thereby applied
AU2015263777B2 (en) * 2014-05-19 2019-01-17 Atlas Copco Airpower, Naamloze Vennootschap Method for expanding a gas flow and device thereby applied
US10253631B2 (en) 2014-05-19 2019-04-09 Atlas Copco Airpower, Naamloze Vennootschap Method for expanding a gas flow and device thereby applied
KR102008055B1 (en) 2014-05-19 2019-10-21 아틀라스 캅코 에어파워, 남로체 벤누트삽 Method for expanding a gas flow and device thereby applied
WO2015176145A1 (en) * 2014-05-19 2015-11-26 Atlas Copco Airpower, Naamloze Vennootschap Method for expanding a gas flow and device thereby applied
GB2534377A (en) * 2015-01-21 2016-07-27 Zeropex Group Ltd Water treatment apparatus and method
US20220221316A1 (en) * 2019-05-23 2022-07-14 Electro Mechanical Developments Limited Fluid Monitoring Apparatus

Similar Documents

Publication Publication Date Title
CA2644938A1 (en) System for generating power in a pipeline
CN101371009B (en) Adjustable guiding device
EP2434130B1 (en) Turbine starter valve
US10830156B2 (en) Fuel supply pipeline system for gas turbine
RU2006113447A (en) AIR CONTROL DEVICE CIRCULATING INSIDE A ROTATING SHAFT OF A GAS TURBINE ENGINE
WO2008036394A3 (en) Separator drum and compressor impeller assembly
WO2008125806A3 (en) Fluid turbine
CN207297838U (en) A kind of lubricating oil cooling system for gear-box
WO2009031556A1 (en) Torque converter
KR101981877B1 (en) Method and apparatus for controlling the oil temperature of an oil-injected compressor plant or vacuum pump
ATE554287T1 (en) WIND TURBINE WITH AXIAL AIR INTAKE AND RADIAL AIR OUTLET
WO2009018788A3 (en) Fluid turbine
JP5864600B2 (en) Exhaust gas turbocharger
JP5991310B2 (en) Rotary pump and fuel vapor leak detection device using the same
JP2007046504A (en) Steam turbine control system
CN101616789A (en) Be used for the tool box that comprises improved compressor assemblies that inflatable article is repaired and inflated
JP2009191639A (en) Variable capacity turbine and variable capacity turbo charger
CN212423424U (en) Speed-adjustable propeller
CN106460555B (en) Equipment for sealing turbine interior environment
KR100751706B1 (en) Water flow control valve
JP6185338B2 (en) Power generator
JP4577236B2 (en) Exhaust control device for internal combustion engine
WO2014199643A1 (en) Engine system, and ship
CA2744242A1 (en) Thermostatic valve having an impeller
WO2007104647A3 (en) Gas turbine for a thermal power plant, and method for the operation of such a gas turbine

Legal Events

Date Code Title Description
FZDE Dead