DEVICE FOR STORING A PRESSURIZED GAS, IN PARTICULAR HYDROGEN
A tank has a generally prismatic shape, and is capable of containing a pressurized gas. The tank comprises a composite shell, which has fibrous reinforcements and a matrix extending continuously over the six faces of the prism and delimits a sealed internal cavity comprising a plurality of open cells. The tank comprises continuous fibrous reinforcements extending into and bonded to the composite shell and further extending through the internal cavity between two opposite faces of the tank. The tank is advantageously integrated into the floor of a vehicle, in particular to the structure of an aircraft.
1 . A tank with for a pressurized gas, comprising:
a composite shell which has fibrous reinforcements and a matrix extending continuously over all faces of a prism shape of the tank, and the composite shell delimiting a sealed internal cavity comprising a plurality of open cells, comprising fibrous reinforcements extending into and bonded to the composite shell and which, in addition, extend through the sealed internal cavity between two faces of the tank, wherein the tank comprises a sealed liner between the composite shell and the sealed internal cavity, and spacers extending between two faces of the sealed internal cavity.
2 . The tank according to claim 1 , wherein the spacers are hollow spacers and the fibrous reinforcements extend inside said hollow spacers.
3 . The tank according to claim 1 , wherein the spacers are made of a three-dimensional nonwoven structure.
4 . The tank according to claim 1 , comprising a flange made of material with the composite shell, the flange configured to fasten the tank to a desired structure.
5 . The tank according to claim 1 , comprising a coupling comprising a part extending through the composite shell into the sealed internal cavity.
6 . The tank according to claim 5 , wherein the part of the coupling extending into the sealed internal cavity is threaded.
7 . The tank according to claim 5 , wherein the part of the coupling extending into the sealed internal cavity is a conical needle.
8 . The tank according to claim 5 , wherein the part of the coupling extending into the sealed internal cavity is a ribbed needle.
9 . The tank according to claim 5 , wherein the coupling is held by holding strips surrounding the tank.
10 . The use of the tank according to claim 1 , to store hydrogen under a pressure between 200 bar and 1000 bar.
11 . The use according to claim 10 , wherein the tank is integrated into a floor structure of an aircraft.
12 . The use according to claim 10 , wherein the tank is integrated into a floor structure of an electric motor vehicle chassis powered by a fuel cell.