Abstract: Devices for protecting aircraft against bad weather. A device for protecting a wing of an aircraft including a load-bearing structure for a protective wall for the wing, the load-bearing structure having a supporting frame having at least two uprights linked by at least one cross member, at least one upright, at the end of the frame having a linking attachment arrangement permitting at least rotation about an axis perpendicular to the surface, the other uprights, each having one foot with an arrangement configured to facilitate the movement of the frame over the surface on which the frame rests. The protection device enables immediate, rapid and easy positioning requiring very few operators.

Abstract: A device for checking at least one pressurized testing tool for a fluid circuit of an aircraft includes at least one tank that includes at least one connection to connect a pressurized gas supply and at least one connection system arranged to connect at least one pressurized testing tool. This device makes it possible to perform preventive checks on pressurized testing tools without having to immobilize an aeroplane on an assembly line.

Abstract: Devices for protecting aircraft against bad weather. A device for protecting a wing of an aircraft including a load-bearing structure for a protective wall for the wing, the load-bearing structure having a supporting frame having at least two uprights linked by at least one cross member, at least one upright, at the end of the frame having a linking attachment arrangement permitting at least rotation about an axis perpendicular to the surface, the other uprights, each having one foot with an arrangement configured to facilitate the movement of the frame over the surface on which the frame rests. The protection device enables immediate, rapid and easy positioning requiring very few operators.

Abstract: A tool for sealing at least one opening of a fluid circuit element, the tool including a support, at least one sealing device for an opening connected to the support and positioning structure for positioning and immobilizing the support with respect to the fluid circuit element, the frame comprising a U-shaped stirrup with a base and two arms, a rod and two connections connecting the rod to each arm, each arm including a centering wedge attached to the internal face of the arm which presents a bearing surface, the bearing surfaces being spaced apart by a distance making it possible to immobilize the fluid circuit element in a first direction in a transverse plane.

Abstract: A device for carrying out a test on a fluid circuit of an aircraft including a test unit which includes, at the inlet, at least one means of connection to a pressurized gas supply connected to means for regulating the pressure of the gas provided by the supply as a function of the test to be carried out and, at the outlet, at least two connection means connected to the means for regulating the pressure of the gas, wherein at least two connection means have different dimensions tailored to a range of pressures or a given pressure.

Abstract: A sealing device is suitable, for example, for conducting verification and testing of fluid-tightness, and includes a body supporting an end piece equipped with a gasket. The gasket presents an outer surface in which at least one area is in the form of a truncated cone. A sealing method concerns the sealing of an aircraft pipe presenting an opening arranged behind a wall, with the aid of a sealing device as described above.

Abstract: A device for checking at least one pressurized testing tool for a fluid circuit of an aircraft includes at least one tank that includes at least one connection to connect a pressurized gas supply and at least one connection system arranged to connect at least one pressurized testing tool. This device makes it possible to perform preventive checks on pressurized testing tools without having to immobilize an aeroplane on an assembly line.

Abstract: A tool for sealing at least one opening of a fluid circuit element, the tool including a support, at least one sealing device for an opening connected to the support and positioning structure for positioning and immobilizing the support with respect to the fluid circuit element, the frame comprising a U-shaped stirrup with a base and two arms, a rod and two connections connecting the rod to each arm, each arm including a centering wedge attached to the internal face of the arm which presents a bearing surface, the bearing surfaces being spaced apart by a distance making it possible to immobilize the fluid circuit element in a first direction in a transverse plane.

Abstract: A device for shutting an aircraft jettisoning circuit includes a coupling endpiece. The endpiece carries a sealing gasket and means suitable for modifying a dimension of the gasket.

Abstract: A sealing device is suitable, for example, for conducting verification and testing of fluid-tightness, and includes a body supporting an end piece equipped with a gasket. The gasket presents an outer surface in which at least one area is in the form of a truncated cone. A sealing method concerns the sealing of an aircraft pipe presenting an opening arranged behind a wall, with the aid of a sealing device as described above.

Abstract: A device for shutting an aircraft jettisoning circuit includes a coupling endpiece. The endpiece carries a sealing gasket and means suitable for modifying a dimension of the gasket.