Turbopump with anti-vibration system

Patent metadata

Field	Value
Publication number	US-10190592-B2
Application number	US-201414892867-A
Country	US
Kind code	B2
Filing date	May 14, 2014
Priority date	May 20, 2013
Publication date	Jan 29, 2019
Grant date	Jan 29, 2019

Abstract

A turbopump includes a turbine fed with hot gas, a pump driven by the turbine and fed with liquid fluid, and a hot gas exhaust pipe situated downstream from the turbine. The turbopump includes a bleed-and-injection circuit including a bleeder for bleeding the liquid fluid at the outlet from the pump, a heater for heating the liquid fluid as bled off in this way so as to transform it into gaseous fluid, and an injector for injecting the gaseous fluid into an interface region of the turbopump situated between the pump and the turbine, so as to optimize the flow and temperature conditions of the fluid entering into the turbine cavity in order to eliminate the vibratory phenomena that result from interaction between the fluid and the turbine disk.

First claim

The invention claimed is:

1. A turbopump, comprising:
a casing;
a turbine fed with hot gas;
a pump driven by the turbine via a shaft and fed with liquid fluid;
a hot gas exhaust pipe situated downstream from the turbine; and
a bleed-and-injection circuit comprising
a bleed pipe adapted to bleed a liquid fluid at an outlet from the pump,
a heat exchanger adapted to heat the liquid fluid as bled off so as to transform the liquid fluid into gaseous fluid, and
an injector pipe adapted to inject the gaseous fluid into an interface region of the turbopump situated between the pump and the turbine,

wherein the gaseous fluid is injected directly between first and second dynamic seals that define a dynamic sealing system that cooperates with the shaft and with the casing of the turbopump, which dynamic sealing system is located in an interface region situated between the pump and the turbine.

2. The turbopump according to claim 1 , wherein the turbine is fed with hot gas and the pump is fed with liquid hydrogen.

3. The turbopump according to claim 1 , wherein the bleed pipe extends from the outlet of the pump to an inlet of the heat exchanger cooperating with the exhaust pipe, and the injection pipe extends from an outlet of the heat exchanger to the interface region.

4. The turbopump according to claim 3 , wherein the heat exchanger comprises a fluid flow chamber with a wall situated in the hot gas exhaust pipe.

5. The turbopump according to claim 4 , wherein the flow chamber is coil shaped.

6. The turbopump according to claim 3 , wherein the bleed-and-injection circuit includes a constriction for controlling a flow of the liquid fluid in the bleed pipe.

7. The turbopump according to claim 6 , wherein the constriction adjusts a fluid pressure in the bleed pipe.

8. The turbopump according to claim 3 , wherein the bleed-and-injection circuit includes a bypass pipe for bypassing the heat exchanger between the bleed pipe and the injection pipe, and an adjustable constriction for sharing the liquid fluid between the bypass pipe and the heat exchanger.

9. The turbopump according to claim 8 , wherein the adjustable constriction is provided on at least one of the bypass pipe and a segment of the bleed pipe that extends between the bypass pipe and the heat exchanger.

10. The turbopump according to claim 3 , wherein the bleed-and-injection circuit includes a constriction for adjusting flow rate in the injection pipe.

11. The turbopump according to claim 1 , further comprising a helium flow circuit for injecting helium into at least one of the pump and the turbine.

12. The turbopump according to claim 11 , wherein the helium is injected via the dynamic sealing system.

13. The turbopump according to claim 1 , wherein the first dynamic seal includes a first sealing gasket held by a first flange and a spacer, the second dynamic seal includes a second sealing gasket held by a second flange and the spacer, and the gaseous fluid is injected from the injector pipe in a location between the first and second sealing gaskets via holes that are radially pierced through the spacer.

14. The turbopump according to claim 13 , wherein a first radial end of the spacer is sandwiched between the first sealing gasket and the second sealing gasket, a second radial end of the spacer is sandwiched between the first flange and the second flange, and the holes are radially pierced through the first radial end of the spacer.

Assignees

• Arianegroup Sas

Inventors

• Le Louedec Dominique
• Chemla Guillaume
• Even Philippe
• Millon Frederick
• Collongeat Laurent

Classifications

• F04D25/045

  the pump wheel carrying the fluid driving means, e.g. turbine blades · CPC title

• F02K9/566

  elements and safety devices, e.g. pressure relief valves · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F02K9/48

  driven by a gas turbine fed by propellant combustion gases {or fed by vaporized propellants or other gases} · CPC title

• F01D11/06 Primary

  Control thereof · CPC title