ELECTRODE ASSEMBLY WITH HEAT SPREADING LAYER, BATTERY CELL AND BATTERY EMPLOYING SUCH ELECTRODE ASSEMBLIES
20230268582 ยท 2023-08-24
Inventors
- John NORTHWOOD (Munich, DE)
- David FINKELSTEIN (Munich, DE)
- Dominic Pascal FORSTERMANN (Munich, DE)
- Ryan PITRE (Munich, DE)
Cpc classification
H01M10/0413
ELECTRICITY
H01M4/525
ELECTRICITY
H01M4/505
ELECTRICITY
Y02E60/10
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
H01M10/617
ELECTRICITY
G06F1/1635
PHYSICS
H01M10/6551
ELECTRICITY
H01M10/4235
ELECTRICITY
H01M50/131
ELECTRICITY
H01M4/663
ELECTRICITY
H01M10/653
ELECTRICITY
B60L50/70
PERFORMING OPERATIONS; TRANSPORTING
H01M2220/20
ELECTRICITY
H01M10/0525
ELECTRICITY
International classification
H01M10/653
ELECTRICITY
B60L50/70
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Disclosed herein is an electrode assembly, comprising in a stacked manner a first anode layer, an anode current collector layer, a second anode layer, a separator layer, a first cathode layer, a cathode current collector layer, and a second cathode layer. In the electrode assembly, the anode current collector layer and/or the cathode current collector layer comprises at least two conductive layers wherein between neighbouring pairs of conductive layers, a respective heat spreading layer is interposed.
Claims
1. An electrode assembly, comprising in a stacked manner: a first anode layer; an anode current collector layer; a second anode layer; a separator layer; a first cathode layer; a cathode current collector layer and a second cathode layer characterized in that the anode current collector layer and/or the cathode current collector layer comprises at least two conductive layers wherein between neighbouring pairs of conductive layers, a respective heat spreading layer is interposed.
2. The electrode assembly according to claim 1, wherein the at least one heat spreading layer has a thermal conductivity that is larger than 200 W/(mK).
3. The electrode assembly according to claim 1, wherein the at least one heat spreading layer is made from a carbon material, in particular a pyrolytic carbon material.
4. The electrode assembly according to claim 1, wherein the at least one heat spreading layer has a thickness between 0.5 .Math.m and 200 .Math.m.
5. The electrode assembly according to claim 1, wherein the at least one heat spreading layer around its edges is connected to its neighbouring conductive layers in a gas-tight manner.
6. The electrode assembly according to claim 1, wherein the anode layers comprise a carbon material and/or the cathode layers comprise an NMC 811 material.
7. The electrode assembly according to claim 1, wherein the conductive layers of the anode current collector layer comprise a copper material and/or the conductive layers of the cathode current collector layer comprise an aluminium material.
8. The electrode assembly according to claim 1, wherein the separator layer comprises a plastic material.
9. A battery cell, comprising an electrode assembly according to claim 1.
10. The battery cell according to claim 9 in the form of a pouch-type battery cell, wherein the electrode assembly is accommodated within a laminated film.
11. The battery cell according to claim 10, wherein the laminated film also comprises at least one heat spreading layer.
12. The battery cell according to claim 11, wherein at least one heat spreading layer of the electrode assembly is connected to at least one heat spreading layer of the laminated film.
13. The battery, comprising at least one battery cell according to claim 9.
14. The battery according to claim 13, further comprising a thermal management system adapted to control temperature of the at least one battery cell, wherein said thermal management system includes active cooling means and/or passive cooling means.
15. The battery according to claim 13, wherein the battery is adapted to drive an electric aircraft engine, in particular an engine of an electric vertical take-off and landing aircraft, wherein the engine is rotatable between a hover position, in which a thrust direction of the engine is substantially parallel to the vertical axis of the aircraft, and a cruise position, in which a thrust direction of the engine is substantially parallel to the longitudinal axis of the aircraft.
Description
[0018] Further features and advantages of the present invention will become even clearer from the following description of an embodiment thereof, when taken together with the accompanying drawings. Said drawings show in particular:
[0019]
[0020]
[0021]
[0022]
[0023] In
[0024] On the other hand,
[0025] The difference between the electrode assembly 10 shown in
[0026] By introducing the respective heat spreading layer 122b into the cathode current collector layer 122 and/or the anode current collector layer 114, an improved distribution of heat is achieved within the active area of the electrode assembly 100 according to the present invention and temperature gradients therein are avoided or at least reduced. This leads to improved performance of the resulting battery cell as well as improved longevity thereof. It shall be stated that the present invention is also applicable to different variations of electrode assemblies, for example comprising at least two pairs of anode layers or cathode layers and additional separator layers.
[0027]
[0028] Lastly,
[0029] The battery cells 200 are stacked in parallel to one another such as to form a cell stack. To maintain mechanical integrity of the cell stacks, battery 300 comprises a frame or housing 302 holding the cells 200 in position and allowing handling of the battery 300 as a single unit. Furthermore, battery 300 comprises electric connection means 304 for connecting all cells 200 in parallel or in series, depending on the required characteristics of the battery, thus suitably connecting the contact tabs 204 of the cell 200 together and to battery terminals 306.
[0030] In addition, battery 300 may comprise a thermal management system 308, which includes a heat conductor 310, which is in direct contact with the pouches of all cells 200, as well as a cooling device 312 for cooling the heat conductor. The heat conductor may be a metal strip or a metal bar. The cooling device 312 may be an active cooling device such as a fan, a heat exchanger, etc., or a passive cooling device such as a plurality of cooling ribs. Alternatively, heat conductor 310 may be thermally connected to an external heat sink to transport heat away from the battery 300.
[0031] In addition, the thermal management system 308 may comprise means for monitoring and controlling the temperature, for example a temperature sensor or electronics to control an active cooling device depending on the measured temperature.