A double-end seal pressure stabilizing device for a turbo pump

A pressure stabilizing device and turbo pump technology, which is applied to parts, pumps, and pump components of pumping devices for elastic fluids, can solve problems such as unfavorable long-term storage, damage to end face seals, and limited pressure stabilizing capacity, and achieve maintenance Good performance, elimination of abnormal high pressure, light weight effect

Active Publication Date: 2016-06-29
NO 11 INST OF NO 6 ACADEMY OF CHINA AEROSPACE SCI & TECH
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to overcome the abnormal high pressure of the fluoroether oil cavity in the double-end seal structure of the engine turbo pump, which leads to the damage of the end seal, solve the problem that the existing voltage stabilizing device requires secondary maintenance (replenishment gas is required, which is not conducive to long-term storage), low reliability, Due to the shortcomings of limited pressure stabilization ability, the present invention provides a new type of pressure stabilization device with double-end seals for turbo pumps. At the same time, it can eliminate the pressure stabilizing device of the high pressure in the oil chamber

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • A double-end seal pressure stabilizing device for a turbo pump
  • A double-end seal pressure stabilizing device for a turbo pump
  • A double-end seal pressure stabilizing device for a turbo pump

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0026] When a normal turbo pump is assembled, the double-end seal oil chamber 12 is filled with about 28mL of fluoroether oil. In the case of a turbo pump without a pressure stabilizing device, the amount of liquid oxidant leaked by the spring-type end face seal is theoretically calculated to be 1mL. The leaked oxidant medium absorbs heat and vaporizes in the remaining cavity of the sealed oil chamber (the largest cavity is 8mL based on experience), expands rapidly and suppresses pressure, and the pressure in the oil chamber can rise to 7.6MPa instantly. In order to keep the oxidant spring-type end face seal from being damaged under this leakage amount (oil chamber pressure ≤ 1.8MPa), it can be known from the above gas isothermal calculation that an effective volume of at least 33.78mL is required to reduce the oil chamber pressure from 7.6MPa to 1.8MPa to achieve the unloading capacity. pressure effect. The total volume of the designed oil cylinder of the present invention i...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention relates to a double-end sealing pressure stabilizing device of a turbo pump, which includes an oil cylinder fixed on the pump body of the turbo pump, an oil inlet conduit, a balance piston, a cylinder head and a balance circuit. The balance piston divides the oil cylinder into a fluoroether oil chamber and a Propellant chamber, one end of the oil inlet conduit is fixed on one end of the oil cylinder and communicates with the fluoroether oil chamber, the other end is fixed on the turbo pump housing and connected with the closed oil chamber, and the cylinder head is fixed on the other end of the oil cylinder One end, one end of the balance circuit is fixed on the cylinder head and communicates with the propellant chamber through the cylinder head, and the other end of the balance circuit is fixed on the pump body of the turbo pump and communicates with the inlet pipeline of the oxidant pump. In order to overcome the abnormal high pressure of the fluoroether oil chamber during the operation of the double-end seal structure of the engine turbo pump, which causes the end-face seal to be damaged, the voltage stabilizing device of the present invention is small in size, light in weight, high-temperature resistant, and corrosion-resistant, which is beneficial to long-term storage and does not require secondary maintenance, and at the same time can eliminate the pressure stabilizing device of the high pressure in the oil chamber.

Description

technical field [0001] The invention relates to a pressure stabilizing device, in particular to a novel pressure stabilizing device suitable for double-end seals of engine turbo pumps, which can be used for lubricating, stabilizing, releasing and maintaining pressure of the double-end seal structures of engine turbo pumps. Background technique [0002] As the heart of the engine, the turbo pump has the characteristics of high temperature, high pressure, high speed and corrosive medium. Turbo pumps include pumps, turbines, and various sealing components. A double seal structure is adopted between the oxidizer pump and the turbine of the engine turbo pump in a finalized state. The spring type face seal 2 is the main seal, which is close to the oxidant pump, and the bellows type face seal 1 is the auxiliary seal, which is close to the turbine side. Between the seals is a closed oil chamber 12, which is filled with fluoroether oil to cool and lubricate. In recent years, double...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Patents(China)
IPC IPC(8): F04D29/06F04D29/08F04D29/58
Inventor 赵瑞勇陈炜刘军年张翠儒白东安郭维毋杰徐楠杨大昱傅春
Owner NO 11 INST OF NO 6 ACADEMY OF CHINA AEROSPACE SCI & TECH
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products