Damping sealing device for oxygen hydrogen turbine pump with large power

A technology for sealing devices and turbo pumps, which is applied to the components of pumping devices for elastic fluids, jet propulsion devices, rocket engine devices, etc., can solve problems such as instability and precession amplitude increase, and reduce cross stiffness , Reduce the circumferential flow velocity, improve the fluid stiffness and damping effect

Active Publication Date: 2020-01-10
BEIJING AEROSPACE PROPULSION INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the rotor is disturbed, the large sealing fluid cross stiffness can easily increase the precession amplitude and even cause instability

Method used

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  • Damping sealing device for oxygen hydrogen turbine pump with large power
  • Damping sealing device for oxygen hydrogen turbine pump with large power
  • Damping sealing device for oxygen hydrogen turbine pump with large power

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0031] A low-temperature, high-speed, heavy-duty hydrogen-oxygen turbo pump damping and sealing device (that is, a damping and sealing device for a high-power hydrogen-oxygen turbo pump), which can be applied to the impeller shoulder of a cryogenic pump or the interstage seal of a multi-stage pump, Its structure is composed of a damping sealing assembly 1 and a sealing shaft sleeve 2 . The damping seal assembly 1 is installed on the turbo pump casing 3 through bolt connection, and is a stationary assembly. The shaft sleeve 2 is installed on the rotating shaft 4, and its two sides are respectively clamped by the shafting parts and rotate with the shaft. The schematic diagram of the damping sealing device is shown in figure 1 , the schematic diagram of the damping seal assembly is shown in figure 2 . Such as figure 1 As shown, the right side of the damping seal device is the high-pressure chamber in the pump, and the left side is the low-pressure chamber in the pump. The da...

Embodiment 2

[0039] A low-temperature pump impeller shoulder and a damping seal device between pump stages for high-speed liquid hydrogen and liquid oxygen turbo pumps. Its structure is composed of a static damping seal assembly 1 and a rotating seal bushing 2. For the assembly relationship, see figure 1As shown, the damping seal assembly 1 is assembled on the pump housing 3 of the hydrogen-oxygen turbo pump, and the sealing sleeve 2 is assembled on the rotor sleeve 2 of the turbo pump to rotate with the shaft at high speed.

[0040] The right side of the damping seal device is the high-pressure area of ​​the pump chamber, and the left side is the low-pressure area of ​​the pump chamber. The damping seal can not only limit the leakage rate of the medium inside the pump chamber, but also reduce the cross stiffness of the seal, improve the damping effect, suppress the vibration of the rotor, and improve Rotor stability.

[0041] The damping sealing assembly 1 is brazed by a stainless steel o...

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Abstract

The invention provides a damping sealing device for an oxygen hydrogen turbine pump with large power and belongs to the technical field of rocket engines. The damping sealing device comprises a damping sealing assembly 1 and a sealing shaft sleeve 2. The damping sealing assembly 1 is installed on an external turbine pump shell 3. The sealing shaft sleeve 2 is installed on an external rotating shaft 4. The damping sealing assembly 1 comprises a shell 5 and a lining 6. The shell 5 and the lining 6 are matched by the adoption of a conical face. The lining 6 and the sealing shaft sleeve 2 form a friction pair. Holes arranged in a staggered manner are formed in the inner surface, close to the sealing shaft sleeve 2, of the lining 6. A rotating preventing blade 9 is arranged on the end face, located on high-pressure liquid, of the lining 6. The damping sealing device can improve the throttling ability, reduce the sealing leakage rate remarkably and improve rotor stability remarkably.

Description

technical field [0001] The invention relates to a damping and sealing device for a high-power hydrogen-oxygen turbo pump, which belongs to the technical field of rocket engines. Background technique [0002] The hydrogen-oxygen engine has the advantages of high performance, high reliability, and environmental protection. The world's major aerospace powers have adopted it as the main power system of high-thrust launch vehicles. The hydrogen-oxygen turbo pump is the core component of the hydrogen-oxygen engine, and its technical level often reflects the technical level of the engine. [0003] Compared with small-thrust engines, the working conditions of large-thrust or heavy-duty engine turbopumps are extremely high, and their power is greatly increased. For example, the power of the hydrogen turbopump of the main engine of the space shuttle reaches the megawatt level, and the pump outlet pressure reaches more than 40MPa. In order to meet the comprehensive performance requir...

Claims

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Application Information

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IPC IPC(8): F04D29/08F04D29/10F04D29/66F02K9/46
CPCF02K9/46F04D29/083F04D29/102F04D29/668
Inventor黄克松李小芬叶小强沈文金蒋文山崔垒杨文静周丹洋金志磊林奇燕孙纪国
OwnerBEIJING AEROSPACE PROPULSION INST