MODULE AND SYSTEM FOR DEPRESSURISING A CRYOGENIC TANK
20190249828 ยท 2019-08-15
Inventors
- Patrick Subreville (Ferrieres Haut Clocher, FR)
- Philippe Liegeois (Maisons-Laffitte, FR)
- Yacine Zellouf (Asnieres sur Seine, FR)
- Karim Osman (Gennevilliers, FR)
- Hicham Guedacha (Marnes la Coquette, FR)
Cpc classification
F17C2225/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/054
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/0302
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2265/07
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C6/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2265/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0439
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0161
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2265/027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2225/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2225/047
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/0135
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/056
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0443
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/043
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E60/32
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F17C2221/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
Some embodiments are directed to a module for depressurisation and storage of a portion of a gas coming from at least one cryogenic tank. Some other embodiments are directed to a system using such a module.
Claims
1. A module for depressurisation, collection and storage of a portion of a gas layer coming from at least one vehicle cryogenic tank the cryogenic tank comprising at least one valve, the gas layer being the gaseous phase of a gas energy source, the cryogenic tank containing, apart from the gas layer, a liquid layer that is the liquid phase of a gas energy source, the module being characterised in that it constitutes a sealed assembly comprising: an inlet intended to be connected, by a removable inlet pipe, to at least one orifice of the tank for the discharge, out of the cryogenic tank, of a portion of gas layer, the orifice being fitted or not with a valve. an outlet intended to be connected, by a removable outlet pipe, to an external system suitable for using the portion of gas layer once discharged, a heater connected to the inlet of the module, a damping buffer tank, connected to the heater, and also to a compressor, connected to the buffer tank, and also to a storage connected to the outlet of the module, the storage making it possible to store the portion of gas layer discharged.
2. The module according to claim 1, wherein the storage is able to store the portion of gas layer discharged at a pressure equal to or greater than 200 bar.
3. The module according to claim 1, further including an odouriser situated between the buffer tank and the compressor.
4. The module according to claim 1, further including an additional outlet connected to the outlet of the compressor.
5. A system for depressurisation, collection and storage of a portion of gas layer coming from at least one vehicle cryogenic tank comprising at least one valve, the gas layer being the gaseous phase of a gas energy source, the cryogenic tank containing, apart from said the gas layer, a liquid layer that is the liquid phase of a gas energy source, the system being characterised in that it comprises: the compact module according to claim 1; a main removable inlet pipe for transporting the portion of gas layer coming from the cryogenic tank, between at least one orifice of the tank and the inlet of the module, the orifice being provided or not with a valve, at least one connecting device for connecting the discharge orifice of the tank with the removable inlet pipe, the connection device being sealed and cryogenic, and a removable outlet pipe for transporting the portion of gas layer stored in the storage, between the outlet of the module and an external system configured to store and/or use the portion of gas layer stored.
6. The system according to claim 5, wherein the removable outlet pipe is suitable for being connected to a gas transport and/or distribution network, or to a mixed heat and electricity cogeneration system, or to an electricity production system, or to a system for distributing vehicle natural gas VNG.
7. The system according to claim 5, wherein the inlet pipe and/or the outlet pipe are flexible hoses.
8. The system according to claim 5, wherein the main removable inlet pipe includes a manifold provided with a plurality of connection devices, so as to be able to be connected to a plurality of cryogenic tanks.
9. The system according to claim 5, wherein the main removable inlet pipe is a pipe for the controlled depressurisation of one or more cryogenic tanks, the pipe including a maintaining device or maintainer for maintaining or reducing the internal pressure of the cryogenic tank at a value equal to or less than a predetermined value.
10. The system according claim 5, wherein the main removable inlet pipe is connected to one or more cryogenic tanks, the discharge orifice of which is provided with a flap valve.
11. A method for maintaining or reducing the internal pressure of the cryogenic tank in active mode of the drainage system according to claim 9 for at a value below a predetermined value.
12. A method for maintaining or reducing the internal pressure of the cryogenic tank in passive mode of the drainage system according to claim 10, for recovering the portion of gaseous phase escaping from a flap valve.
Description
BRIEF DESCRIPTION OF THE FIGURES
[0050] Other advantages and particularities of some embodiments will emerge from the following description given by way of non-limitative example and made with reference to the accompanying figures:
[0051]
[0052]
[0053] The identical elements shown in
[0054] DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS
[0055]
[0056] More particularly,
[0057] The depressurisation and storage module 400 illustrated in
[0058] an inlet E intended to be connected, by a removable inlet pipe 300, to an orifice 102 (not provided with a flap valve in these embodiments) of a plurality of cryogenic tanks 100, 111, 112, for the discharge, out of these tanks, of a portion of gas layer,
[0059] an outlet S intended to be connected, by a removable outlet pipe 500, to an external system able to use the portion of gas layer once discharged;
[0060] a heater 4010 connected to the inlet E of the module 400,
[0061] a damping buffer tank 4004, connected to the heater 4010, and also to a compressor 4002, connected to the buffer tank 4004, and also to
[0062] a storage means 4006 connected to the outlet S for storing the portion of gas layer discharged.
[0063] The depressurisation, collection and storage system according to some embodiments further includes:
[0064] a main removable inlet pipe 300 for transporting the portion of gas layer coming from three cryogenic tanks 100, 111, 112, the pipe 300 being connected to
[0065] a manifold provided with a plurality of connection devices 200, 201, 202 (for example three in number),
[0066] each of the connection devices 200, 201, 202 being connected to each of the discharge orifices 102 of the cryogenic tanks 100, 111, 112, these connection devices being sealed and cryogenic,
[0067] a removable outlet pipe 500 for transporting the portion of gas layer stored in the storage means 4008, between the outlet S of the module 400 and an external system 600 able to store and/or use the portion of gas layer stored.
[0068]
[0069]
[0070]
[0071] Thus
[0072] Likewise,
[0073] Finally,