CN203614761U - Ultralow-temperature large-caliber pneumatic exhaust valve - Google Patents

Ultralow-temperature large-caliber pneumatic exhaust valve Download PDF

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Publication number
CN203614761U
CN203614761U CN201320778371.3U CN201320778371U CN203614761U CN 203614761 U CN203614761 U CN 203614761U CN 201320778371 U CN201320778371 U CN 201320778371U CN 203614761 U CN203614761 U CN 203614761U
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CN
China
Prior art keywords
valve
actuator
valve body
air cylinder
cylinder shell
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 - Lifetime
Application number
CN201320778371.3U
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Chinese (zh)
Inventor
孙法国
高健
石朝锋
马飞
何延文
岳兵
余锋
张翼
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.)
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Astronautical Systems Engineering
Original Assignee
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Astronautical Systems Engineering
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
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Application filed by China Academy of Launch Vehicle Technology CALT, Beijing Institute of Astronautical Systems Engineering filed Critical China Academy of Launch Vehicle Technology CALT
Priority to CN201320778371.3U priority Critical patent/CN203614761U/en
Application granted granted Critical
Publication of CN203614761U publication Critical patent/CN203614761U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

An ultralow-temperature large-caliber pneumatic exhaust valve comprises a valve body, a valve flap, a valve seat, an indium wire, a valve rod, a main spring, a flange, an air cylinder casing, an actuator, a position annunciator, an air cylinder casing connection pipe nozzle, an auxiliary spring and an ejection rod piston, wherein static sealing between the valve seat and the valve body is achieved through the indium wire, the valve rod is vertically connected with the middle of the valve flap, a retaining ring is arranged at the end portion of the valve rod, the main spring is arranged between the valve body and the retaining ring, the valve rod corresponds to the ejection rod piston in the axial direction, the air cylinder casing is connected with the valve body through a flange, the actuator is arranged in the air cylinder casing to correspond to the air cylinder casing connection pipe nozzle and adopts a multiple-layer welding film box, and the auxiliary spring sleeves the ejection rod piston. The ultralow-temperature large-caliber pneumatic exhaust valve is easy to seal and is not clamped, and exhaust flows are sufficient.

Description

The pneumatic outlet valve of a kind of ultralow temperature heavy caliber
Technical field
The utility model relates to the pneumatic outlet valve of a kind of ultralow temperature heavy caliber, applies in the pneumatic exhaust of space flight model.
Background technique
Flying model ultralow temperature outlet valve, bore is less, does not meet the usage requirement of carrier rocket heavy caliber of new generation, ultralow temperature.Have no at present the cryopumping valve that is applicable to the large flow of carrier rocket of new generation, ultra-low temperature surroundings.The design of heavy caliber Subzero valve mainly contains three difficult points:
(1) heavy caliber outlet valve is difficult for realizing the requirement of Large Launch Vehicle low temperature seal.A new generation's carrier rocket propellant agent is liquid hydrogen, liquid oxygen, and danger is larger, higher to seal request.And heavy caliber valve seat, spool processing plane degree, perpendicularity are difficult for guaranteeing, be difficult at low temperatures realizing sealing.
(2) cryopumping valve guide structure hardening at low temperatures, deformation-compensated ability reduces greatly, works clamping stagnation easily occurs under low temperature environment, can not realize the normal exhaust of tank, and its pressure is raise, and exceedes allowed band, has great danger.
(3) heavy caliber outlet valve spool area is larger, needs larger gas load to open, and is U-shaped bellows at present in the actuator of use, and U-shaped bellows is easy unstability under high pressure, and reliability is lower, is occurring such fault at present with model cryopumping valve.
Model utility content
Technical problem to be solved in the utility model is: for meeting the requirement of carrier rocket ultralow temperature of new generation, high-flow air-exhaust, provide a kind of heavy caliber outlet valve that can adapt to ultra-low temperature surroundings.
Technical solution of the present utility model is:
The pneumatic outlet valve of a kind of ultralow temperature heavy caliber, comprise valve body, flap, valve seat, indium silk, valve rod, main spring, flange, cylinder shell, actuator, position signalling apparatus, cylinder shell connecting-tube nozzle, auxiliary spring, ram piston, wherein between valve seat and valve body, pass through indium silk static seal, the vertical flap of valve rod middle part connects, valve rod end is provided with back-up ring, main spring is arranged between valve body and back-up ring, valve rod with ram piston axially corresponding, cylinder shell is connected with valve body by flange, actuator is arranged in cylinder shell corresponding with cylinder shell connecting-tube nozzle, actuator adopts multilayer welding bellows, auxiliary spring is placed on ram piston.
Ram piston is overcoat fluoroplastic structures.
Actuator adopts high-temperature alloy material.
The utility model advantage is compared with prior art:
(1) between the utility model valve seat and valve body, static seal adopts indium silk sealing configuration, makes low temperature heavy caliber exhaust valve sealing effect better;
(2) actuator adopts multilayer welding bellows, efficiently solves the lead problem of easy clamping stagnation of heavy caliber cryopumping valve;
(3) piston guide bar is overcoat fluoroplastic structures, and flow is more abundant at low temperatures to make outlet valve.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Embodiment
As shown in Figure 1, the pneumatic outlet valve of a kind of ultralow temperature heavy caliber, comprise valve body 1, flap 2, valve seat 3, indium silk 4, valve rod 5, main spring 6, flange 7, cylinder shell 8, actuator 9, position signalling apparatus 10, cylinder shell connecting-tube nozzle 11, auxiliary spring 12, ram piston 13, wherein between valve seat 3 and valve body 1, pass through indium silk 4 static seals, indium silk fifth wheel control aspect is all respond well, the mounting torque needing is less, not only can reduce valve seat 3 flange thicknesses, and it is good to avoid valve seat 3 to be out of shape valve seat 3 poor sealings that cause, easily guarantee that valve seat 3 end face corresponding to valve body 1 fits tightly location simultaneously, guarantee the sealing at valve seat 3 places.Actuator 9 adopts multilayer welding bellows, multilayer welding bellows is high-temperature alloy material, can adapt to the rugged environment such as high pressure, low temperature, and there is larger deformability, can adapt to the requirement of the larger stroke of heavy caliber outlet valve, this structure has good self lubricity, and has at low temperatures larger displacement compensation capability.
The vertical flap of valve rod 52 middle parts connect, valve rod 5 ends are provided with back-up ring, main spring 6 is arranged between valve body 1 and back-up ring, valve rod 5 and ram piston 12 are axially to corresponding, cylinder shell 8 is connected with valve body 1 by flange 7, actuator 9 is arranged in cylinder shell 8 corresponding with cylinder shell connecting-tube nozzle 11, and auxiliary spring 12 is placed on ram piston 13, and ram piston 13 is overcoat fluoroplastic structures.
Working procedure is: (one) exhaust process, under position signalling apparatus 10 effects, pass into 5MPa and control gas, control gas and promote actuator 9, ram piston 13, overcome auxiliary spring 12 precompressions, to left movement, ram piston 13 promotes flap 2 and overcomes main spring 6 precompressions, and to left movement, outlet valve is opened, tank gas, by entrance, outlet valve internal diameter, is discharged through outlet; (2) closing process, under position signalling apparatus 10 effects, makes gas be reduced to gauge pressure, actuator 9 moves right under auxiliary spring 12 pressure, gets back to closed position, and flap 2 is under main spring 6 pressure-actings simultaneously, move right, spool is closed, and entrance and outlet passage are closed.
The unexposed technology of the utility model belongs to general knowledge as well known to those skilled in the art.

Claims (3)

1. the pneumatic outlet valve of ultralow temperature heavy caliber, it is characterized in that, comprise valve body (1), flap (2), valve seat (3), indium silk (4), valve rod (5), main spring (6), flange (7), cylinder shell (8), actuator (9), position signalling apparatus (10), cylinder shell connecting-tube nozzle (11), auxiliary spring (12), ram piston (13), wherein between valve seat (3) and valve body (1), pass through indium silk (4) static seal, the vertical flap (2) of valve rod (5) middle part connects, valve rod (5) end is provided with back-up ring, main spring (6) is arranged between valve body (1) and back-up ring, valve rod (5) with ram piston (12) axially corresponding, cylinder shell (8) is connected with valve body (1) by flange (7), actuator (9) is arranged in cylinder shell (8) corresponding with cylinder shell connecting-tube nozzle (11), actuator (9) adopts multilayer welding bellows, auxiliary spring (12) is placed on ram piston (13).
2. the pneumatic outlet valve of a kind of ultralow temperature heavy caliber as claimed in claim 1, is characterized in that, ram piston (13) is overcoat fluoroplastic structures.
3. the pneumatic outlet valve of a kind of ultralow temperature heavy caliber as claimed in claim 1, is characterized in that, actuator (9) adopts high-temperature alloy material.
CN201320778371.3U 2013-11-29 2013-11-29 Ultralow-temperature large-caliber pneumatic exhaust valve Expired - Lifetime CN203614761U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320778371.3U CN203614761U (en) 2013-11-29 2013-11-29 Ultralow-temperature large-caliber pneumatic exhaust valve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320778371.3U CN203614761U (en) 2013-11-29 2013-11-29 Ultralow-temperature large-caliber pneumatic exhaust valve

Publications (1)

Publication Number Publication Date
CN203614761U true CN203614761U (en) 2014-05-28

Family

ID=50767410

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320778371.3U Expired - Lifetime CN203614761U (en) 2013-11-29 2013-11-29 Ultralow-temperature large-caliber pneumatic exhaust valve

Country Status (1)

Country Link
CN (1) CN203614761U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108591551A (en) * 2018-07-17 2018-09-28 阜宁县中洲阀门有限公司 A kind of forged steel fuel feeding valve
CN109027398A (en) * 2018-09-19 2018-12-18 北京航天动力研究所 Ultralow temperature high pressure double spool linkage valve
CN110985197A (en) * 2018-10-02 2020-04-10 高级知识产权有限公司 Air release valve with corrugated pipe

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108591551A (en) * 2018-07-17 2018-09-28 阜宁县中洲阀门有限公司 A kind of forged steel fuel feeding valve
CN108591551B (en) * 2018-07-17 2023-09-19 江苏应流机械制造有限责任公司 Forged steel oiling valve
CN109027398A (en) * 2018-09-19 2018-12-18 北京航天动力研究所 Ultralow temperature high pressure double spool linkage valve
CN109027398B (en) * 2018-09-19 2024-05-03 北京航天动力研究所 Ultralow temperature high pressure double-valve core linkage valve
CN110985197A (en) * 2018-10-02 2020-04-10 高级知识产权有限公司 Air release valve with corrugated pipe
CN110985197B (en) * 2018-10-02 2022-02-25 高级知识产权有限公司 Air release valve with corrugated pipe

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Granted publication date: 20140528