Motor Vehicle with a Cryogenic Pressure Vessel and Method for Refuelling a Cryogenic Pressure Vessel of a Motor Vehicle
20170225939 · 2017-08-10
Inventors
Cpc classification
F17C2260/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0326
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0629
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/018
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B67D7/04
PERFORMING OPERATIONS; TRANSPORTING
F17C2205/0192
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0391
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0421
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/001
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B67D7/78
PERFORMING OPERATIONS; TRANSPORTING
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
F17C2250/0636
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2265/065
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/072
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0439
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0161
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0491
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B67D7/3218
PERFORMING OPERATIONS; TRANSPORTING
F17C1/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/034
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
B67D7/32
PERFORMING OPERATIONS; TRANSPORTING
B67D7/78
PERFORMING OPERATIONS; TRANSPORTING
F17C1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method is provided for refueling a cryogenic pressure vessel of a motor vehicle. The motor vehicle has: a) a cryogenic pressure vessel having an internal vessel which stores a fluid, an external vessel and heat insulation which is arranged between the internal vessel and the external vessel, at least in certain areas; and b) a controller, wherein the controller is designed to interrupt refueling of the motor vehicle if, in the case of damaged thermal insulation, a lower fluid density limiting value for the fluid in the internal vessel is exceeded. The lower fluid density limiting value is lower than an upper fluid density limiting value for the fluid in the internal vessel in the case of refueling of the internal vessel with intact thermal insulation.
Claims
1. A motor vehicle, comprising: a cryogenic pressure vessel with an inner vessel storing a fluid, an outer vessel and thermal insulation which is arranged at least in regions between the inner vessel and the outer vessel; and a controller, wherein the controller is configured to interrupt refueling of the motor vehicle if, in an event of damaged thermal insulation, a lower fluid density limit value for the fluid in the inner vessel is exceeded, wherein the lower fluid density limit value is lower than an upper fluid density limit value for the fluid in the inner vessel in the case of refueling of the inner vessel with intact thermal insulation.
2. The motor vehicle as claimed in claim 1, further comprising: a refueling valve configured to interrupt the inflow of fluid into the inner vessel.
3. The motor vehicle as claimed in claim 2, further comprising: a communication interface that transmits a refueling termination signal and/or a refueling limiting signal to a refueling device.
4. The motor vehicle as claimed in claim 1, further comprising: a communication interface that transmits a refueling termination signal and/or a refueling limiting signal to a refueling device.
5. A method for refueling a cryogenic pressure vessel of a motor vehicle, the method comprising the steps of: determining damage to thermal insulation which is arranged at least in regions between an inner vessel and an outer vessel of the cryogenic pressure vessel; and interrupting refueling of the motor vehicle if, in an event of damaged thermal insulation, a lower fluid density limit value for the fluid in the inner vessel is exceeded, wherein the lower fluid density limit value is lower than an upper fluid density limit value for the fluid in the inner vessel in the case of refueling of the inner vessel with intact thermal insulation.
6. The method as claimed in claim 5, wherein the lower fluid density limit value is selected such that the inner vessel in an uninsulated state can store a fluid without the maximally permissible inner vessel pressure being exceeded.
7. The method as claimed in claim 5, further comprising the step of: interrupting, via a refueling valve, inflow of fluid into the inner vessel in the event of damaged thermal insulation when the lower fluid density limit value is reached.
8. The method as claimed in claim 6, further comprising the step of: interrupting, via a refueling valve, inflow of fluid into the inner vessel in the event of damaged thermal insulation when the lower fluid density limit value is reached.
9. The method as claimed in claim 5, further comprising the step of: transmitting, via a communication interface, a refueling termination signal and/or a refueling limiting signal to a refueling device.
10. The method as claimed in claim 6, further comprising the step of: transmitting, via a communication interface, a refueling termination signal and/or a refueling limiting signal to a refueling device.
11. The method as claimed in claim 7, further comprising the step of: transmitting, via a communication interface, a refueling termination signal and/or a refueling limiting signal to a refueling device.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0025]
[0026]
DETAILED DESCRIPTION OF THE DRAWINGS
[0027] The cryogenic pressure vessel 100 illustrated in
[0028] A connection 150 is provided at the other end of the supply line 300. The connection or filler neck 150 is designed to be coupled to a corresponding connection 200 of a refueling device.
[0029] Furthermore, a communication interface 160 is arranged here in the connection 150. The communication interface is able to be connected to a corresponding communication interface 210 in the connection 200. A refueling termination signal and/or a refueling limiting signal can be transmitted to the refueling device 200 via the communication interface 160/210. In addition to this configuration, a radio-based communication (interface) is likewise contemplated (for example WiFi, WLAN, NFC, etc.) which does not have to be accommodated in the connection 200.
[0030] The refueling valve 180 is designed here to interrupt the fluid flow, here a hydrogen flow. The refueling valve 180 can be arranged anywhere in the supply line 300.
[0031] The controller 140 is designed to control the refueling and the operation of the cryogenic pressure vessel.
[0032]
[0033] If the cryogenic pressure vessel 100 now has damaged thermal insulation V, the pressure vessel 100 has to comparatively rapidly dissipate comparatively large quantities of hydrogen so that the inner vessel 110 is not destroyed by the expanding hydrogen. In
[0034] If damage to the thermal insulation V is then determined, refueling should be ceased up to the upper fluid density limit value DOB. However, it is not necessary to completely dispense with refueling. On the contrary, it is possible to cryogenically refuel the inner vessel 110 in such a manner that a critical inner vessel pressure does not arise even in the heated state of the cryogenically filled fluid. For this purpose, at the cryogenic refueling temperature, the fluid density D should be limited to a lower fluid density limit value D.sub.UB for the fluid in the inner vessel 110, wherein the lower fluid density limit value D.sub.UB is selected in such a manner that the inner vessel 110 in the uninsulated state can store the fluid without the maximally permissible inner vessel pressure Pmax being exceeded. For an inner vessel 110 with a maximally permissible inner vessel pressure Pmax of approx. 350 bar, a lower fluid density limit value DUB of approx. 21 gram/liter (point PKB in
[0035] The preceding description of the present invention serves only for illustrative purposes and not for the purpose of limiting the invention. Within the scope of the invention, various amendments and modifications are possible without departing from the scope of the invention and the equivalents thereof. Even though the description is primarily focused on hydrogen as fuel, other fuels, such as compressed natural gas, are likewise included therewith. The numerical values mentioned are merely preferred values. It is likewise possible, for example, to provide inner vessels 110 with higher or low design pressures.
[0036] The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.