Tank and method for manufacturing same

Patent metadata

Field	Value
Publication number	US-9963997-B2
Application number	US-201414285071-A
Country	US
Kind code	B2
Filing date	May 22, 2014
Priority date	May 27, 2013
Publication date	May 8, 2018
Grant date	May 8, 2018

Abstract

The present invention relates to a method for manufacturing a tank ( 1 ) comprising a main body ( 4 ) with several compartments ( 7 ), a base ( 6 ) closing the lower part of the main body ( 4 ), and a cover ( 5 ) closing the upper part of the main body ( 4 ), said method comprising the following steps:
shaping sheets to produce the parts making up the tank ( 1 ); assembling each of the component parts by butt welding in order to produce the tank ( 1 ).

First claim

The invention claimed is:

1. A fluid tank for a turbojet engine, said tank comprising:
a main body provided with several compartments, each of the several compartments having one of a closed cylindrical or ovoid cross-sectional shape and extending along a longitudinal axis between a lower part and an upper part of the main body;
a base having an open end and a partially closed end; and
a cover having an open end and a partially closed end, wherein the main body, the base and the cover are essentially made from metal sheets and are welded,
wherein each of the several compartments comprises a first end and a second end, wherein exclusively each of the first ends comprise a first flange that extends in a direction that is substantially perpendicular to the longitudinal axis of the compartment, and exclusively each of the second ends comprise a second flange that extend in a direction that is substantially perpendicular to the longitudinal axis of the compartment,
wherein the first flanges of adjacent compartments of the several compartments connect together to establish fluid communication between the adjacent compartments, and the second flanges of the adjacent compartments connect together to establish fluid communication between the adjacent compartments, and
wherein the open end of the cover attaches to the first flanges and the first ends of all of the several compartments, and the open end of the base attaches to the second flanges and the second ends of all of the several compartments.

2. The tank as in claim 1 , said tank comprising butt welds and being free of any fillet welds.

3. The tank as in claim 1 , wherein a cross-section of each of the several compartments is not constant along the longitudinal axis of the compartment.

4. The tank as in claim 1 , wherein said metal sheets are made from steel, stainless steel, copper, brass, aluminum or an aluminum or copper-based alloy.

5. A turbojet engine comprising, said engine comprising a fluid tank, said tank comprising:
a main body provided with several compartments, each of the several compartments having one of a closed cylindrical or ovoid cross-sectional shape and extending longitudinally between a lower part and an upper part of the main body;
a base having an open end and a partially closed end; and
a cover having an open end and a partially closed end,
wherein the main body, the base and the cover are essentially made from metal sheets and are welded;
wherein each of the several compartments comprises a first end and a second end, wherein exclusively each of the first ends comprise a first flange that extends in a direction that is substantially perpendicular to the longitudinal axis of the compartment and exclusively each of the second ends comprise a second flange that extends in a direction that is substantially perpendicular to the longitudinal axis of the compartment,
wherein the first flanges of adjacent compartments of the several compartments connect together to establish fluid communication between the adjacent compartments, and the second flanges of the adjacent compartments connect together to establish fluid communication between the adjacent compartments, and
wherein the open end of the cover attaches to the first flanges and the first ends of all of the several compartments, and the open end of the base attaches to the second flanges and the second ends of all of the several compartments.

6. The tank as in claim 5 , wherein the first flanges and the second flanges, respectively of each of the several compartments, are connected together end-to-end by welding.

7. The tank as in claim 5 , wherein each of the first flanges and of the second flanges have a U-shaped cross section.

Assignees

• Techspace Aero Sa
• Safran Aero Boosters Sa

Inventors

• Cornet Albert
• Bougelet Stéphane

Classifications

• B21D51/18

  vessels, e.g. tubs, vats, tanks, sinks, or the like · CPC title

• B21D51/10

  conically or cylindrically shaped objects · CPC title

• F02C7/04

  Air intakes for gas-turbine plants or jet-propulsion plants · CPC title

• F01D25/18 Primary

  Lubricating arrangements (of machines or engines in general F01M) · CPC title

• F16N19/00 Primary

  Lubricant containers for use in lubricators or lubrication systems · CPC title