CN107940064A - Gas ballast valve is based on pump warm air vapor partial pressure regulating device - Google Patents
Gas ballast valve is based on pump warm air vapor partial pressure regulating device Download PDFInfo
- Publication number
- CN107940064A CN107940064A CN201610901672.9A CN201610901672A CN107940064A CN 107940064 A CN107940064 A CN 107940064A CN 201610901672 A CN201610901672 A CN 201610901672A CN 107940064 A CN107940064 A CN 107940064A
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- China
- Prior art keywords
- module
- partial pressure
- pump
- vapor partial
- temperature
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- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K31/00—Actuating devices; Operating means; Releasing devices
- F16K31/02—Actuating devices; Operating means; Releasing devices electric; magnetic
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K37/00—Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
- F16K37/0025—Electrical or magnetic means
- F16K37/0041—Electrical or magnetic means for measuring valve parameters
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, including a body (1), set temperature induction module (2), pressure induction module (3), vacuum feedback module (4), management module (5) on body (1), during operation, temperature sense module (2) is arranged on pump, sense its temperature, pressure induction module (3) senses vapor partial pressure numerical value, vacuum feedback module (4) feeds back fuselage vacuum sealing situation, management module (5) processing integrated information；Air-flow adjustment module (6) is set in temperature sense module (2), according to the appropriate speed for adjusting air-flow and passing through of pump temperature；On pressure induction module (3) set humidity inductive module (7), sensing steam in fuselage present in state status；Reminding module (8) is set in management module (5)；By controlling pump temperature, air velocity, avoid influencing steam discharge effect.
Description
Technical field
The present invention relates to a kind of gas ballast valve.
Background technology
Gas ballast valve is a kind of valve for making most of steam non-condensing and being discharged together with gas, has and does not pollute oil etc.
Effect, also there are some defects, its steam not to discharge in time in terms of vapor partial pressure in gas ballast valve operation, can be to operation effect
Fruit produces deleterious effect.
The content of the invention
The purpose of the present invention is that providing a kind of effective gas ballast valve is based on pump warm air vapor partial pressure regulating device.
What the present invention was realized in.Gas ballast valve is based on pump warm air vapor partial pressure regulating device, including a body,
Set temperature induction module, pressure induction module, vacuum feedback module, management module on body, during operation, temperature sense mould
Block is arranged on pump, senses its temperature, pressure induction module sensing vapor partial pressure numerical value, it is true that vacuum feedback module feeds back fuselage
Empty sealing situation, management module processing integrated information.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, and air-flow adjustment module is set in temperature sense module,
According to the appropriate speed for adjusting air-flow and passing through of pump temperature.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, and humidity inductive module is set on pressure induction module,
Sense steam in fuselage present in state status.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, reminding module is set in management module, when sensing
When fuselage pressure or tightness have abnormal, prompting is sent.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, reminding module send the mode of prompting for sound or
LED is shown.
Above-mentioned gas ballast valve is based on pump warm air vapor partial pressure regulating device, by controlling pump temperature, air velocity, avoids influencing
Steam discharges effect.
Brief description of the drawings
Attached drawing is structure diagram of the gas ballast valve based on pump warm air vapor partial pressure regulating device.
Figure label is respectively：1- bodies, 2- temperature senses module, 3- pressure induction module, 4- vacuums feedback module,
5- management modules, 6- air-flows adjustment module, 7- humidity inductive modules, 8- reminding modules.
Embodiment
Embodiment：As shown in drawings.Gas ballast valve is based on pump warm air vapor partial pressure regulating device, including a body (1),
Set temperature induction module (2), pressure induction module (3), vacuum feedback module (4), management module (5) on body (1),
During operation, temperature sense module (2) is arranged on pump, senses its temperature, and pressure induction module (3) senses vapor partial pressure numerical value,
Vacuum feedback module (4) feeds back fuselage vacuum sealing situation, management module (5) processing integrated information.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, sets air-flow to adjust mould in temperature sense module (2)
Block (6), according to the appropriate speed for adjusting air-flow and passing through of pump temperature.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, and humidity inductive mould is set on pressure induction module (3)
Block (7), sensing steam in fuselage present in state status.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, and reminding module (8) is set in management module (5), when
When sensing that fuselage pressure or tightness have abnormal, prompting is sent.
Gas ballast valve is based on pump warm air vapor partial pressure regulating device, reminding module (8) send the mode of prompting for sound or
Person LED is shown.
Above-mentioned gas ballast valve is based on pump warm air vapor partial pressure regulating device, by controlling pump temperature, air velocity, avoids influencing
Steam discharges effect.
Claims (5)
1. gas ballast valve is based on pump warm air vapor partial pressure regulating device, it is characterised in that including a body (1), in body (1)
Upper set temperature induction module (2), pressure induction module (3), vacuum feedback module (4), management module (5), during operation, temperature
Degree induction module (2) is arranged on pump, senses its temperature, pressure induction module (3) sensing vapor partial pressure numerical value, vacuum feedback
Module (4) feeds back fuselage vacuum sealing situation, management module (5) processing integrated information.
2. gas ballast valve according to claim 1 is based on pump warm air vapor partial pressure regulating device, it is characterised in that in temperature
Air-flow adjustment module (6) is set on induction module (2), according to the appropriate speed for adjusting air-flow and passing through of pump temperature.
3. gas ballast valve according to claim 1 is based on pump warm air vapor partial pressure regulating device, it is characterised in that in pressure
On induction module (3) set humidity inductive module (7), sensing steam in fuselage present in state status.
4. gas ballast valve according to claim 1 is based on pump warm air vapor partial pressure regulating device, it is characterised in that is managing
Reminding module (8) is set in module (5), when sensing that fuselage pressure or tightness have abnormal, sends prompting.
5. gas ballast valve according to claim 4 is based on pump warm air vapor partial pressure regulating device, it is characterised in that prompting mould
The mode that block (8) sends prompting shows for sound or LED.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610901672.9A CN107940064A (en) | 2016-10-12 | 2016-10-12 | Gas ballast valve is based on pump warm air vapor partial pressure regulating device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610901672.9A CN107940064A (en) | 2016-10-12 | 2016-10-12 | Gas ballast valve is based on pump warm air vapor partial pressure regulating device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107940064A true CN107940064A (en) | 2018-04-20 |
Family
ID=61928981
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610901672.9A Pending CN107940064A (en) | 2016-10-12 | 2016-10-12 | Gas ballast valve is based on pump warm air vapor partial pressure regulating device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107940064A (en) |
-
2016
- 2016-10-12 CN CN201610901672.9A patent/CN107940064A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180420 |
|
| WD01 | Invention patent application deemed withdrawn after publication |