CN105089775A - Actuator pressure regulating connecting valve used for pressurizer of turbine engine - Google Patents

Actuator pressure regulating connecting valve used for pressurizer of turbine engine Download PDF

Info

Publication number
CN105089775A
CN105089775A CN201510560214.9A CN201510560214A CN105089775A CN 105089775 A CN105089775 A CN 105089775A CN 201510560214 A CN201510560214 A CN 201510560214A CN 105089775 A CN105089775 A CN 105089775A
Authority
CN
China
Prior art keywords
controlling element
final controlling
groove structure
valve pocket
stop nut
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.)
Pending
Application number
CN201510560214.9A
Other languages
Chinese (zh)
Inventor
朱茂蒙
刘鹏展
胡辽平
苏泓
李广能
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.)
Hunan Tianyan Machinery Co Ltd
Original Assignee
Hunan Tianyan Machinery Co 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 Hunan Tianyan Machinery Co Ltd filed Critical Hunan Tianyan Machinery Co Ltd
Priority to CN201510560214.9A priority Critical patent/CN105089775A/en
Publication of CN105089775A publication Critical patent/CN105089775A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Supercharger (AREA)

Abstract

The invention discloses an actuator pressure regulating connecting valve used for a pressurizer of a turbine engine. The actuator pressure regulating connecting valve comprises a valve sleeve; the valve sleeve is a sleeve connection piece provided with a through groove structure; a limiting nut is fixedly connected in the through groove structure; the limiting nut can rotate freely in the space provided by the through groove structure of the valve sleeve but can not move transversely relative to the valve sleeve; the valve sleeve further comprises a fixing hole. According to the technical scheme, the height of the connecting valve relative to an actuator can be adjusted by using the limiting nut fixed in the valve sleeve in a rotary mode, the condition that the limiting nut can only rotate by 180 degrees in each adjustment process is not limited, so that the rotation adjusting accuracy is improved, the pressure limit can be controlled accurately, and the normal work of the pressurizer of the turbine engine can be guaranteed.

Description

A kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve
Technical field
The present invention relates to engine turbine supercharging technology field, especially, relate to a kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve.
Background technique
The final controlling element of turbocharger of motor is again turbocharger bypass valve actuator, is one of critical elements of pressurized machine, manages be connected with turbine box bypath valve with gas compressor air outlet.In prior art, the sleeve pipe standing part of final controlling element and attachment portion are an entirety, accurately to meet then needs dismounting to fixing and adjustment simultaneously and the integral multiple of tilt fixing (180 °) can only be rotated, the requirement accurately regulating pressure limits value cannot be reached at all.Final controlling element carries unique control section of pressurized machine and engine control machine internal air pressure limits value, if final controlling element because of air pressure limits value control inaccurate, turbosupercharger may be made to open bypath valve not yet because bearing barometric pressure, and therefore cause that body loosens, heating, leakage of oil, booster turbine rotor speed are too high causes pressurized machine burning machine; Meanwhile, engine section also can be too high because of boost pressure during high speed operation, thus the cylinder-firing pressure of motor exceed limits value after uncontrollable cause damage and cannot work.
Rotate the low pressure limits value that cannot accurately regulate of degree of regulation for prior art middle sleeve and cause the problem of turbocharger of motor job failure, not yet have effective solution at present.
Summary of the invention
Rotate the low pressure limits value that cannot accurately regulate of degree of regulation for prior art middle sleeve and cause the problem of turbocharger of motor job failure, the object of the invention is to propose a kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve, rotation degree of regulation can be improved, accurate pilot pressure restriction, ensures that turbocharger of motor normally works.
Based on above-mentioned purpose, technological scheme provided by the invention is as follows:
According to an aspect of the present invention, a kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve is provided.
Valve pocket is comprised according to turbogenerator pressurized machine final controlling element pressure regulation connection valve provided by the invention, valve pocket is a Coupling with groove structure, wherein, a stop nut is fixedly connected with in groove structure, freely rotate in the space that stop nut can provide in the groove structure of valve pocket, but can not relative to valve pocket translation; Valve pocket also comprises fixed hole.
Wherein, groove structure is positioned at the upper end of valve pocket, and the space in the groove structure of valve pocket is divided into two-part by stop nut, asks compared with the external space of shallow-layer and compared with space in deep layer respectively; When final controlling element is connected with final controlling element pressure regulation connection valve, final controlling element tail end inserts in the groove structure of valve pocket, wherein, final controlling element tail end is through the external space and stop nut and touch interior space, and stop nut can carry out micro-translation by External Force Acting on final controlling element tail end.
Further, physical contact is not had between the outer surface of final controlling element tail end and the groove structure interior surface of valve pocket; The outer surface of final controlling element tail end and the internal surface of stop nut have mutually corresponding male and female screw thread, are fixed between final controlling element tail end and stop nut by screw thread rotation, and stop nut can reach the effect of upward-downward translation on final controlling element tail end by the mode rotated.
Further, fixed hole is arranged at valve pocket lower end; When pressurized machine is connected with final controlling element pressure regulation connection valve, fixed hole is buckled on the bypass valve of pressurized machine, and the bypass valve of pressurized machine is vented to final controlling element by fixed hole.
As can be seen from above, technological scheme provided by the invention adjusts the technological scheme of connection valve relative to final controlling element height by using the rotation stop nut be fixed in valve pocket, no longer be limited to each adjustment and can only rotate 180 degree, therefore improve rotation degree of regulation, accomplish accurate pilot pressure restriction, and ensured that turbocharger of motor normally works.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technological scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural drawing of the turbogenerator pressurized machine final controlling element pressure regulation connection valve according to the embodiment of the present invention.
Embodiment
Clearly understand for making the object, technical solutions and advantages of the present invention, below in conjunction with the accompanying drawing in the embodiment of the present invention, to the technological scheme in the embodiment of the present invention carry out further clear, complete, describe in detail, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain, belongs to the scope of protection of the invention.
According to one embodiment of present invention, a kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve is provided.
As shown in Fig. 1 (a), 1 (b) Yu 1 (c), valve pocket 4 is comprised according to the turbogenerator pressurized machine final controlling element pressure regulation connection valve that embodiments of the invention provide, valve pocket 4 is a Coupling with groove structure, wherein, a stop nut 2 is fixedly connected with in groove structure, freely rotate in the space that stop nut 2 can provide in the groove structure of valve pocket 4, but can not relative to valve pocket 4 translation; Valve pocket 4 also comprises fixed hole 5.
Wherein, groove structure is positioned at the upper end of valve pocket 4, and the space in the groove structure of valve pocket 4 is divided into two-part by stop nut 2, asks compared with the external space 1 of shallow-layer and compared with space in deep layer 3 respectively; When final controlling element is connected with final controlling element pressure regulation connection valve, final controlling element tail end inserts in the groove structure of valve pocket 4, wherein, final controlling element tail end touches interior space 3 through the external space 1 with stop nut 2, and stop nut 2 can carry out micro-translation by External Force Acting on final controlling element tail end.
Physical contact is not had between the outer surface of final controlling element tail end and the groove structure interior surface of valve pocket 4; Outer surface and the internal surface of stop nut 2 of final controlling element tail end have mutually corresponding male and female screw thread, fixed by screw thread rotation between final controlling element tail end and stop nut 2, stop nut 2 can reach the effect of upward-downward translation on final controlling element tail end by the mode rotated.
Fixed hole 5 is arranged at valve pocket 4 lower end; When pressurized machine is connected with final controlling element pressure regulation connection valve, fixed hole 5 is buckled on the bypass valve of pressurized machine, and the bypass valve of pressurized machine is vented to final controlling element by fixed hole 5.
Valve pocket 4 in the present invention does not have direct physical with final controlling element and contacts, and solves the impact by the restriction of final controlling element pull rod screw direction; Simultaneously, tunica pipe is fixing dead overall structure, precisely cannot regulate force value, and the present invention installs stop nut 2 additional with this limit stoper pilot pressure in pressure regulation connection valve, to coordinate with thread pitch with nut and finely tune pulling force size to control limits value height with this, and solve dismounting effort, the problem such as fragile.
In sum, by means of technique scheme of the present invention, the technological scheme of connection valve relative to final controlling element height is adjusted by using the rotation stop nut be fixed in valve pocket, no longer be limited to each adjustment and can only rotate 180 degree, therefore improve rotation degree of regulation, accomplish accurate pilot pressure restriction, and ensured that turbocharger of motor normally works.First, valve pocket and stop nut relatively independent, mutually rely on again, adjustment operation is simple; Meanwhile, connection valve degree of regulation is high, finely tunes by regulating nut, by the control errors that regulates at ± 0.01mm; In addition, connection valve structure is simple, and assembling is easy, highly versatile.
Those of ordinary skill in the field are to be understood that: the foregoing is only specific embodiments of the invention; be not limited to the present invention; within the spirit and principles in the present invention all, any amendment made, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.

Claims (4)

1. a turbogenerator pressurized machine final controlling element pressure regulation connection valve, it is characterized in that, comprise valve pocket (4), described valve pocket (4) is a Coupling with groove structure, wherein, be fixedly connected with a stop nut (2) in described groove structure, freely rotate in the space that described stop nut (2) can provide in the groove structure of described valve pocket (4), but can not relative to described valve pocket (4) translation; Described valve pocket (4) also comprises fixed hole (5).
2. a kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve according to claim 1, it is characterized in that, described groove structure is positioned at the upper end of described valve pocket (4), space in the groove structure of described valve pocket (4) is divided into two-part by described stop nut (2), asks compared with the external space (1) of shallow-layer and compared with space in deep layer (3) respectively; When final controlling element is connected with final controlling element pressure regulation connection valve, final controlling element tail end inserts in the groove structure of described valve pocket (4), wherein, final controlling element tail end is through the described external space (1) and described stop nut (2) and touch interior space (3), and described stop nut (2) can carry out micro-translation by External Force Acting on final controlling element tail end.
3. a kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve according to claim 2, is characterized in that not having physical contact between the outer surface of described final controlling element tail end and the groove structure interior surface of described valve pocket (4); Outer surface and the internal surface of described stop nut (2) of final controlling element tail end have mutually corresponding male and female screw thread, fixed by screw thread rotation between final controlling element tail end and described stop nut (2), described stop nut (2) can reach the effect of upward-downward translation on final controlling element tail end by the mode rotated.
4. a kind of turbogenerator pressurized machine final controlling element pressure regulation connection valve according to claim 3, it is characterized in that, described fixed hole (5) is arranged at described valve pocket (4) lower end; When pressurized machine is connected with final controlling element pressure regulation connection valve, described fixed hole (5) is buckled on the bypass valve of pressurized machine, and the bypass valve of pressurized machine is vented to final controlling element by described fixed hole (5).
CN201510560214.9A 2015-09-06 2015-09-06 Actuator pressure regulating connecting valve used for pressurizer of turbine engine Pending CN105089775A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510560214.9A CN105089775A (en) 2015-09-06 2015-09-06 Actuator pressure regulating connecting valve used for pressurizer of turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510560214.9A CN105089775A (en) 2015-09-06 2015-09-06 Actuator pressure regulating connecting valve used for pressurizer of turbine engine

Publications (1)

Publication Number Publication Date
CN105089775A true CN105089775A (en) 2015-11-25

Family

ID=54570973

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510560214.9A Pending CN105089775A (en) 2015-09-06 2015-09-06 Actuator pressure regulating connecting valve used for pressurizer of turbine engine

Country Status (1)

Country Link
CN (1) CN105089775A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040055297A1 (en) * 2002-09-20 2004-03-25 Rudiger Allmang Turbocharger
CN1690367A (en) * 2004-04-26 2005-11-02 博格华纳公司 Protector of thread chamfer, operating mechanism with the same and turbocharger
CN201021632Y (en) * 2007-03-17 2008-02-13 湖南天雁机械有限责任公司 Pressure micro-adjustment device for executor of turbine pressure increaser
CN203702324U (en) * 2014-01-02 2014-07-09 宁波威孚天力增压技术有限公司 Air releasing valve used for turbocharger
CN204921148U (en) * 2015-09-06 2015-12-30 湖南天雁机械有限责任公司 Turbine engine is executor pressure regulating junction valve for booster

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040055297A1 (en) * 2002-09-20 2004-03-25 Rudiger Allmang Turbocharger
CN1690367A (en) * 2004-04-26 2005-11-02 博格华纳公司 Protector of thread chamfer, operating mechanism with the same and turbocharger
CN201021632Y (en) * 2007-03-17 2008-02-13 湖南天雁机械有限责任公司 Pressure micro-adjustment device for executor of turbine pressure increaser
CN203702324U (en) * 2014-01-02 2014-07-09 宁波威孚天力增压技术有限公司 Air releasing valve used for turbocharger
CN204921148U (en) * 2015-09-06 2015-12-30 湖南天雁机械有限责任公司 Turbine engine is executor pressure regulating junction valve for booster

Similar Documents

Publication Publication Date Title
CN203871981U (en) Linear displacement type electric steering engine
EP2653717A1 (en) Arrangement to retrofit a wind turbine blade
CN104527969B (en) A kind of aircraft front wing servoactuation system and its method of servo-controlling
JP2016513771A (en) Piston pump power control device and control method thereof
CN204247971U (en) A kind of air floated high speed electric mandrel
CN202297059U (en) Telescopic arm and sliding block mechanism thereof
CN204921148U (en) Turbine engine is executor pressure regulating junction valve for booster
CN108080939A (en) A kind of preposition nut tightening device of aircraft engine high pressure rotor seal pan and method
CN204255319U (en) A kind of stepless-adjustment zero structure of linear movement pick-up
CN105089775A (en) Actuator pressure regulating connecting valve used for pressurizer of turbine engine
CN206366660U (en) Taper rapid-adjusting type thimble structure
CN107444615B (en) Combined elastic self-adaptive wing sweepback changing mechanism and control method
CN205678197U (en) A kind of overflow valve being easy to maintenance
CN104153822A (en) Variable-geometry turbine comprising adjustable stationary blades with groove-shaped small wing structures at leaf ends
CN205373355U (en) Adjusting device of desiccator air door antithetical couplet group
CN203308526U (en) Improved subcritical 300MW steam turbine nozzle block
CN207364078U (en) A kind of anti-loosening bolt assembly easily assembled
CN105464986B (en) A kind of adjustable single screw compressor of star-wheel shafting
CN202972266U (en) Double-movable-joint pipe sealing structure
CN100504038C (en) Axial positioning device for steam turbine low-pressure end outer vapor seal
CN204392002U (en) A kind of servo motor rotor press-fitting tool
CN109026955B (en) Short-ending threaded fastener
CN106194979A (en) Vehicle automatic gear shifting inhaul cable assembly and quickly assemble method
CN207454528U (en) A kind of spherical plain bearing rod end for electric pushrod
CN102588380B (en) A kind of hydraulic jack

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20151125

RJ01 Rejection of invention patent application after publication