IP Library Patent Application 14420947
Patent Application
App. No. 14/420,947

COOLING METHOD

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Quick Facts
Patent No.
US None
App. No.
14/420,947
Abstract

A cooling method for cooling a device connected to a cryogenic tank via a main admission duct for feeding the device with cryogenic fluid once the device is cooled. In contrast, during cooling, a cryogenic fluid is introduced into the device via a cooling admission duct that is different from the main admission duct and that presents a flow section that is narrower than the flow section of the main admission duct.

Claims (10)

1 . A cooling method for cooling a device connected to a cryogenic tank via a main admission duct for feeding the device with cryogenic fluid once the device is cooled, wherein during cooling the cryogenic fluid is introduced into the device via a cooling admission duct that is different from the main admission duct and that presents a flow section that is narrower than the flow section of the main admission duct.

2 . A cooling method according to claim 1 , wherein said device is a pump.

3 . A cooling method according to claim 2 , wherein said device is a turbopump.

4 . A cooling method according to claim 2 , wherein said device is a propellant pump of a rocket engine.

5 . A cooling method according to claim 1 , wherein the cryogenic fluid introduced into the device via the cooling admission duct during cooling also comes from said cryogenic tank.

6 . A cooling method according to claim 5 , wherein, during cooling, the cryogenic fluid is pumped from the tank to said device via the cooling admission duct and returns from the device to the tank via said main admission duct in a direction opposite to the normal flow direction of the cryogenic fluid once the device is cooled.

7 . A cooling method according to claim 5 , wherein, during cooling, the main admission duct remains closed and the cryogenic fluid introduced into the device from the cryogenic tank is subsequently expelled via a purge line.

8 . A cooling method according to claim 1 , wherein the cryogenic fluid introduced into the device via the cooling admission duct comes from a source other than the cryogenic tank that feeds the device with cryogenic fluid via said main admission duct once the device is cooled.

9 . . A cooling method according to claim 1 , wherein the cooling admission duct is a main discharge duct once the device is cooled.

10 . . A cooling method according to claim 9 , wherein, during cooling, the cryogenic fluid is introduced into said main discharge duct via a purge line.

Assignments (3)
CHANGE OF NAME Recorded Nov 20, 2017
From: AIRBUS SAFRAN LAUNCHERS SAS
To: ARIANEGROUP SAS
Reel/Frame 044800/0080 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 10, 2017
From: SNECMA
To: AIRBUS SAFRAN LAUNCHERS SAS
Reel/Frame 044787/0425 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 11, 2015
From: LE GOFFIC, YVAN
To: SNECMA; CENTRE NATIONAL D'ETUDES SPATIALES CNES
Reel/Frame 034936/0500 →