CN106247044A - A kind of high-pressure gas flow controls device - Google Patents

A kind of high-pressure gas flow controls device Download PDF

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Publication number
CN106247044A
CN106247044A CN201610639505.1A CN201610639505A CN106247044A CN 106247044 A CN106247044 A CN 106247044A CN 201610639505 A CN201610639505 A CN 201610639505A CN 106247044 A CN106247044 A CN 106247044A
Authority
CN
China
Prior art keywords
conical surface
pad
sealing
pressure gas
gas flow
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
CN201610639505.1A
Other languages
Chinese (zh)
Inventor
宋晶晶
孔凡超
刘瑞敏
王海峰
赵洪波
王燕娜
韩景山
薛方凝
吴爽
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.)
Beijing Institute of Aerospace Testing Technology
Original Assignee
Beijing Institute of Aerospace Testing Technology
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 Beijing Institute of Aerospace Testing Technology filed Critical Beijing Institute of Aerospace Testing Technology
Priority to CN201610639505.1A priority Critical patent/CN106247044A/en
Publication of CN106247044A publication Critical patent/CN106247044A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L19/00Joints in which sealing surfaces are pressed together by means of a member, e.g. a swivel nut, screwed on or into one of the joint parts
    • F16L19/02Pipe ends provided with collars or flanges, integral with the pipe or not, pressed together by a screwed member
    • F16L19/0212Pipe ends provided with collars or flanges, integral with the pipe or not, pressed together by a screwed member using specially adapted sealing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L19/00Joints in which sealing surfaces are pressed together by means of a member, e.g. a swivel nut, screwed on or into one of the joint parts
    • F16L19/02Pipe ends provided with collars or flanges, integral with the pipe or not, pressed together by a screwed member
    • F16L19/025Pipe ends provided with collars or flanges, integral with the pipe or not, pressed together by a screwed member the pipe ends having integral collars or flanges
    • F16L19/028Pipe ends provided with collars or flanges, integral with the pipe or not, pressed together by a screwed member the pipe ends having integral collars or flanges the collars or flanges being obtained by deformation of the pipe wall
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L55/00Devices or appurtenances for use in, or in connection with, pipes or pipe systems
    • F16L55/02Energy absorbers; Noise absorbers
    • F16L55/027Throttle passages
    • F16L55/02709Throttle passages in the form of perforated plates
    • F16L55/02718Throttle passages in the form of perforated plates placed transversely

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Vessels And Lids Thereof (AREA)

Abstract

The invention discloses the volume control device of a kind of gases at high pressure, be made up of the conical surface and orifice plate profile two parts, use red copper as material, it is possible to meet the demand of high-pressure gas seal and flow-control simultaneously.This apparatus structure is small and exquisite, easy accessibility, saving installing space, it is adaptable to what high-pressure gas flow controlled supplies distribution pipeline.

Description

A kind of high-pressure gas flow controls device
Technical field
The present invention is that the high-pressure gas flow used by the test of a kind of liquid rocket dynamical system controls device, it is possible to simultaneously full Foot high-pressure gas seal and the demand of flow-control, it is adaptable to what high-pressure gas flow controlled supplies distribution pipeline.
Background technology
The test of liquid rocket dynamical system, to requiring higher for gas medium, supply gas pressure, gas supply flow, is nitrogen for gas medium Gas, hydrogen, helium, the highest supply gas pressure 35MPa, gas supply flow scope is at 15g/s~380g/s.Usual at tradition air feed craft Constrictor can be selected as the flow control element of gas, have two kinds with the mode of pipeline assembly connection: Flange joint and screw thread Compress and connect.And in actual mechanical process, both modes but also exist weak point:
(1) testing in liquid rocket dynamical system, owing to gas supply flow scope is relatively wider, constrictor to be carried out the most more Change, as used flange connection, operation complexity is installed, wastes time and energy;
(2) using screw thread to compress connected mode, sealing is poor, especially at the helium supply line of operating pressure 35MPa. Meanwhile, supply air line will be through technological processes such as welding, pickling, passivation before installing, and the globe joint of pipeline easily weares and teares, and it is close Envelope property is worse.
Accordingly, it would be desirable to a kind of be not only easily installed, sealing property but also good volume control device.
Summary of the invention
The technology of the present invention solves problem: the invention provides a kind of easy accessibility, compact structure, can meet high pressure gas Body sealing, can play again the device of flow-control, and can be used for Rocket propulsion system test supplies distribution pipeline.
The technical solution of the present invention: 37 ° of high pressure bulbs of tradition seal by welding straight coupling 1, cap nut 3 and ball Shape joint 4 forms.The present invention arranges special conical gasket 2 between welding straight coupling 1 and globe joint 4.Sealing gasket 2 It is made up of the conical surface and orifice plate profile two parts.Welding straight coupling 1 welds with supply air line, and globe joint 4 welds with another pipeline Connect, conical gasket 2 is arranged on globe joint, and with cap nut by straight-through for the welding conical surface pressure with conical gasket Tightly, conical gasket installation on high-pressure air feed pipeline is completed.
The conical surface seals, conical surface thickness 1mm, and cone angle is 37 °, can meet pressure spherical less than or equal to 35MPa gas The demand sealed.Orifice plate profile plays gas flow control action, and profile thickness should be less than or be equal to 0.05 times of caliber, hole-shaped Formula can select right angle aperture, wedge angle aperture and nozzle orifice according to demand, and aperture can be determined according to gas flow.
The present invention compared with prior art provides the benefit that:
(1) improving the sealing problem that pressure duct is threaded, especially working pressure range is at 23MPa~35MPa, The helium supply line of caliber DN15~DN32.
(2) its simple in construction, it is simple to install, for the pipeline that gas supply flow scope is wider, it is possible to achieve be switched fast Function.
Accompanying drawing explanation
Fig. 1 is that conical gasket installs sectional structure chart.1 it is welding straight coupling, 2 is conical gasket, 3 is overcoat spiral shell Female, 4 be globe joint.
Detailed description of the invention
The invention will be further described with specific embodiment in explanation below in conjunction with the accompanying drawings:
As it is shown in figure 1, this erecting device is by welding straight coupling 1, conical gasket 2, cap nut 3 and globe joint 4 Composition.Wherein welding straight coupling welds with supply air line, and globe joint welds with another pipeline, is arranged on by conical gasket On globe joint, and the conical surface with conical gasket welding is straight-through with cap nut compresses, and completes conical gasket at high pressure Installation on supply air line.
The operation principle of the present invention is: when gases at high pressure are carried out in the face of gases at high pressure through conical gasket, orifice plate type Current limliting, serves the effect of flow-control, and the conical surface presses in globe joint, it is achieved that the sealing function of gases at high pressure.
The present invention is successfully applied to liquid rocket dynamical system test 35MPa helium tank loading line, flow 15g/s; 12MPa cabin section blows down pipeline, flow 380g/s;And achieve good application effect.

Claims (4)

1. a kind of taper orifice plate sealing gasket of invention, it is characterised in that: this pad is made up of the conical surface and orifice plate profile two parts, permissible Meet simultaneously and seal and the effect of flow-control.There is a through hole at pad center, and aperture is less than caliber, can be true according to gas flow Gases at high pressure are played the effect of current limliting by the size of set aperture.
Pore plate by sealing pad the most according to claim 1, it is characterised in that: employing red copper is as material, and makes annealing treatment.
Pore plate by sealing pad the most according to claim 1, it is characterised in that: the conical surface and orifice plate profile use different-thickness, and the conical surface is thick Degree 1mm, profile thickness should be less than or be equal to 0.05 times of caliber.
Pore plate by sealing pad the most according to claim 1, it is characterised in that: pad has certain cone angle conical surface and seals, Cone angle is 37 °, it is possible to meet the requirement of high pressure sealing.
CN201610639505.1A 2016-08-08 2016-08-08 A kind of high-pressure gas flow controls device Pending CN106247044A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610639505.1A CN106247044A (en) 2016-08-08 2016-08-08 A kind of high-pressure gas flow controls device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610639505.1A CN106247044A (en) 2016-08-08 2016-08-08 A kind of high-pressure gas flow controls device

Publications (1)

Publication Number Publication Date
CN106247044A true CN106247044A (en) 2016-12-21

Family

ID=58079212

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610639505.1A Pending CN106247044A (en) 2016-08-08 2016-08-08 A kind of high-pressure gas flow controls device

Country Status (1)

Country Link
CN (1) CN106247044A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106855483A (en) * 2016-12-23 2017-06-16 中国矿业大学 Hydrogen Vapor Pressure fatigue rupture and hydrogen-induced delayed failure sensitivity test equipment and method
CN108758152A (en) * 2018-06-11 2018-11-06 中国冶集团有限公司 A kind of wear-resisting pipeline current-limiting apparatus
CN110939806A (en) * 2019-12-11 2020-03-31 徐州徐工液压件有限公司 Low-temperature-resistant rubber combined joint
CN110985777A (en) * 2019-12-25 2020-04-10 中国航空工业集团公司西安飞机设计研究所 Oxygen pipeline sealing performance improving method
CN112253873A (en) * 2020-11-11 2021-01-22 上海众源燃油分配器制造有限公司 Sealing structure for pipeline interface of R744 air-conditioning heat pump system
CN113374949A (en) * 2021-05-20 2021-09-10 广西电网有限责任公司电力科学研究院 Mass flow controller
CN114542818A (en) * 2022-03-08 2022-05-27 北京航天雷特机电工程有限公司 Conical throttling orifice plate

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3164164A (en) * 1960-02-02 1965-01-05 Pall Corp Pressure-responsive valves
CN1059397A (en) * 1990-08-20 1992-03-11 塞萨尔·法拉昂·肖尔 Pressure-responsive fluid saving device
US5716078A (en) * 1996-08-07 1998-02-10 Powers; Ronald L. Thermoplastic pipe joint
CN101040140A (en) * 2004-10-21 2007-09-19 韦尔奈实验室公司 Internal post flow control
CN103883752A (en) * 2014-03-26 2014-06-25 哈尔滨东安发动机(集团)有限公司 Structure for adjusting pipeline air flow
CN104487751A (en) * 2012-07-13 2015-04-01 Smc株式会社 Pipe joint
CN205078949U (en) * 2015-09-11 2016-03-09 江苏福吉特管业有限公司 Clamping formula pipe joint

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3164164A (en) * 1960-02-02 1965-01-05 Pall Corp Pressure-responsive valves
CN1059397A (en) * 1990-08-20 1992-03-11 塞萨尔·法拉昂·肖尔 Pressure-responsive fluid saving device
US5716078A (en) * 1996-08-07 1998-02-10 Powers; Ronald L. Thermoplastic pipe joint
CN101040140A (en) * 2004-10-21 2007-09-19 韦尔奈实验室公司 Internal post flow control
CN104487751A (en) * 2012-07-13 2015-04-01 Smc株式会社 Pipe joint
CN103883752A (en) * 2014-03-26 2014-06-25 哈尔滨东安发动机(集团)有限公司 Structure for adjusting pipeline air flow
CN205078949U (en) * 2015-09-11 2016-03-09 江苏福吉特管业有限公司 Clamping formula pipe joint

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106855483A (en) * 2016-12-23 2017-06-16 中国矿业大学 Hydrogen Vapor Pressure fatigue rupture and hydrogen-induced delayed failure sensitivity test equipment and method
CN106855483B (en) * 2016-12-23 2020-02-14 中国矿业大学 Hydrogen pressure fatigue fracture and hydrogen induced hysteresis fracture sensitivity test device and method
CN108758152A (en) * 2018-06-11 2018-11-06 中国冶集团有限公司 A kind of wear-resisting pipeline current-limiting apparatus
CN110939806A (en) * 2019-12-11 2020-03-31 徐州徐工液压件有限公司 Low-temperature-resistant rubber combined joint
CN110985777A (en) * 2019-12-25 2020-04-10 中国航空工业集团公司西安飞机设计研究所 Oxygen pipeline sealing performance improving method
CN112253873A (en) * 2020-11-11 2021-01-22 上海众源燃油分配器制造有限公司 Sealing structure for pipeline interface of R744 air-conditioning heat pump system
CN113374949A (en) * 2021-05-20 2021-09-10 广西电网有限责任公司电力科学研究院 Mass flow controller
CN114542818A (en) * 2022-03-08 2022-05-27 北京航天雷特机电工程有限公司 Conical throttling orifice plate

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PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
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Application publication date: 20161221