Method for monitoring for a rupture in a fuel vapor container
09797345 · 2017-10-24
Assignee
Inventors
Cpc classification
F02M25/0872
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B60K2015/03514
PERFORMING OPERATIONS; TRANSPORTING
F02M25/089
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/0854
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/0818
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/0836
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A method for monitoring for a rupture in a storage element of a fuel tank system having a fuel tank includes: detecting, by a mass flow sensor, thermal conductivity of an unmoved air mass in a first line of the fuel tank system; and identifying a rupture in the storage element if the detecting by the mass flow sensor detects a change in the thermal conductivity of the unmoved air mass in the first line when a second valve is in a closed state and/or when an air pump is at a standstill.
Claims
1. A method for monitoring for a rupture in a storage element (5) of a fuel tank system, the fuel tank system having a fuel tank (4) and the storage element (5) being configured to temporarily store hydrocarbons, the fuel tank (4) and the storage element (5) being connected to one another such that hydrocarbons outgassed from fuel situated in the fuel tank (4) are stored in the storage element (5), the storage element (5) being connected to a first line (6) through which fresh air is deliverable to the storage element (5), and the storage element (5) being connected to a second line (12) connecting the storage element (5) to an intake line (16) and through which fresh air enriched with hydrocarbons is deliverable from the storage element (5) to the intake line (16), wherein a mass flow sensor (8) and an air pump (7) are arranged in the first line (6) upstream of the storage element (5) as viewed in the direction of the fresh air flow, and a second valve (13) is arranged in the second line (12) between the storage element (5) and the intake line (16), the method comprising: detecting, by the mass flow sensor (8), thermal conductivity of an unmoved air mass in the first line (6); and identifying that a rupture has occurred in the storage element (5) if the detecting by the mass flow sensor (8) detects a change in the thermal conductivity of the unmoved air mass in the first line (6) in a case in which the second valve (13) is in a closed state and/or in a case in which the air pump (7) is at a standstill.
2. The method as claimed in claim 1, wherein the air pump (7) is a radial pump.
3. The method as claimed in claim 1, wherein the mass flow sensor (8) is a sensor that operates based on the calorimetric principle.
4. The method as claimed in claim 3, wherein the mass flow sensor (8) is integrated in the housing of the air pump (7).
5. The method as claimed in claim 4, wherein the fuel tank system further has a first valve arranged in the first line (6).
6. The method as claimed in claim 5, wherein a rupture in the storage element (5) is identified if the mass flow sensor (8) detects a change in the thermal conductivity of the air in the first line (6) when the first valve is in the closed state.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) An advantageous embodiment of the invention will be described on the basis of the figures, in which:
(2)
(3)
DETAILED DESCRIPTION OF THE PRESENTLY PREFERRED EMBODIMENTS
(4)
(5)
(6) The fuel tank system illustrated in
(7) Furthermore, a mass flow sensor 8 is arranged in the first line 6, preferably in the housing of the air pump 7. This mass flow sensor 8 may, for example, operate on the basis of the thermal (i.e., calorimetric) principle. An example of a mass flow sensor 8 that operates on the basis of the thermal (i.e., calorimetric) principle is a hot-wire anemometer. Within the mass flow sensor 8 there are situated at least two wires, for example platinum wires, or film resistors, which are heated by electrical current. One wire or resistor is cooled directly by the air flowing past, and the other is situated in a position shielded from the flowing air. The flow of electrical current causes both resistor elements to be heated, wherein the air flowing past cools the non-shielded heating element more intensely than that which is shielded from the air. The heating element therefore heats up to a greater degree, and the resistance thereof thus increases. From the resistance values of the two heating elements, and the difference thereof, it is possible, by a characteristic map, to derive the mass flow of the fresh air in the first line 6 and the presence of hydrocarbons in the air, that is to say also a breakthrough through the storage element.
(8) A further example of a mass flow sensor 8 that operates on the basis of the thermal principle is illustrated in
(9) A method according to the invention for monitoring for a breakthrough through a storage element 5 of a fuel tank system can be performed with the fuel tank system illustrated in
(10) Now, in the case of a static air mass, should a change in the thermal conductivity of the air in the first line 6 be detected by the mass flow sensor 8, this can only have occurred owing to a breakthrough of the hydrocarbons through the storage element 5. Thus, the breakthrough of the hydrocarbons through the storage element 5 can be reliably detected, and measures can be implemented which prevent an escape of the hydrocarbons into the surroundings of the fuel tank system. The immediate initiation of purging of the storage element 5 with fresh air is a suitable measure which can prevent the escape of the hydrocarbons. In the case of hybrid vehicles, it may be necessary to start the internal combustion engine in order that the hydrocarbons purged from the storage element 5 can also be burned. All of the measures can be initiated by a control unit 21, wherein the control unit 21 is also configured to process the data detected by the mass flow sensor 8 and to detect information regarding the position of the first valve 9 and of the second valve 13 and the operating state of the air pump 7.
(11) Thus, while there have been shown and described and pointed out fundamental novel features of the invention as applied to a preferred embodiment thereof, it will be understood that various omissions and substitutions and changes in the form and details of the devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those elements and/or method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.