Abstract: Cryogenic tank for storing liquefied H2 under regulated pressure, comprising an external tank (12), an internal tank (18) wherein the internal tank contains liquefied H2 and the space between tanks contains H2 in gas form, an open cell internal insulation (13) in the space between tanks and in contact with the surface of the inner tank, wherein said inner insulation layer (13) is embedded in the H2 gas atmosphere of the space between tanks, at least one outer insulation layer (14) in contact with the inside of the external tank (12) that includes closed-cell foams gasified with inert gases of low conductivity and that also includes an evaporator (16) that ensures that the passage of H2 to the space between tanks to maintain the balance of pressure is performed in gaseous state.

Abstract: The present disclosure relates to a method of assembling hardpoints in aeronautical structures, and more specifically, the disclosed method allows knowing the relative deviation of the hardpoints and of the positioning elements of the hardpoints with respect to a laser beam emitted by a laser collimator fixed to an adjustable support which can be adjusted in at least two directions in space, and by using a correction algorithm, it is possible to know the displacement necessary for locating the positioning elements such that they are aligned with respect to the hardpoints, the positioning elements in turn being moved as a result of the movement of the driven linear tables in one or in several iterative steps, at which time the position thereof is fixed and they are ready for the rest of the hardpoints to be assembled.

Abstract: The present disclosure relates to a method of assembling hardpoints in aeronautical structures, and more specifically, the disclosed method allows knowing the relative deviation of the hardpoints and of the positioning elements of the hardpoints with respect to a laser beam emitted by a laser collimator fixed to an adjustable support which can be adjusted in at least two directions in space, and by using a correction algorithm, it is possible to know the displacement necessary for locating the positioning elements such that they are aligned with respect to the hardpoints, the positioning elements in turn being moved as a result of the movement of the driven linear tables in one or in several iterative steps, at which time the position thereof is fixed and they are ready for the rest of the hardpoints to be assembled.

Abstract: The present disclosure relates to a method of assembling hardpoints in aeronautical structures, and more specifically, the disclosed method allows knowing the relative deviation of the hardpoints and of the positioning elements of the hardpoints with respect to a laser beam emitted by a laser collimator fixed to an adjustable support which can be adjusted in at least two directions in space, and by using a correction algorithm, it is possible to know the displacement necessary for locating the positioning elements such that they are aligned with respect to the hardpoints, the positioning elements in turn being moved as a result of the movement of the driven linear tables in one or in several iterative steps, at which time the position thereof is fixed and they are ready for the rest of the hardpoints to be assembled.

Abstract: A method for performing the assembly of an aircraft includes, once at least first and second templates (A, B) with through holes (a, b) have been defined on a chassis, taking an initial measurement of the templates to identify the positions of the different components; measuring a laser beam to know the real coordinates through which the laser beam passes through the holes (a, b), calculating the mathematical equation of the straight line of the laser beam in order to calculate its path and target points of the elements to be assembled, performing the mathematical calculation of the point where the laser beam must strike when the element is positioned in its theoretical position, calculating the target readings which the measurement apparatus has to show when the laser is in the target point, positioning the element to be assembled following the reading of the apparatus, and fixing the element.

Abstract: The present disclosure relates to a method of assembling hardpoints in aeronautical structures, and more specifically, the disclosed method allows knowing the relative deviation of the hardpoints and of the positioning elements of the hardpoints with respect to a laser beam emitted by a laser collimator fixed to an adjustable support which can be adjusted in at least two directions in space, and by using a correction algorithm, it is possible to know the displacement necessary for locating the positioning elements such that they are aligned with respect to the hardpoints, the positioning elements in turn being moved as a result of the movement of the driven linear tables in one or in several iterative steps, at which time the position thereof is fixed and they are ready for the rest of the hardpoints to be assembled.

Abstract: A method for performing the assembly of an aircraft includes, once at least first and second templates (A, B) with through holes (a, b) have been defined on a chassis, taking an initial measurement of the templates to identify the positions of the different components; measuring a laser beam to know the real coordinates through which the laser beam passes through the holes (a, b), calculating the mathematical equation of the straight line of the laser beam in order to calculate its path and target points of the elements to be assembled, performing the mathematical calculation of the point where the laser beam must strike when the element is positioned in its theoretical position, calculating the target readings which the measurement apparatus has to show when the laser is in the target point, positioning the element to be assembled following the reading of the apparatus, and fixing the element.