Abstract: A positioning device is provided for positioning of a spring leg and a shock damper motor axis when a connection to a body-shaped pieces of a suspension promoter suspended coach industry unit with a mounting stored chassis unit of the vehicle, with the positioning device includes an attachment element Fixture for fixing the direction positioning to mount one of the fixture resistance element jointed affiliated gripping central carrier with a gripper attached to appropriation reach of the spring leg and shock damper, with the gripping means by moving the grief-structural funds his joints in a rest medium defined rest positions to warden can be brought, namely a working position in which the grief by the central taken one spring leg or shock absorbers positioned, and the suspension strut or shock absorbers are not positioned normally.

Abstract: A positioning device is provided for positioning of a spring leg and a shock damper motor axis when a connection to a body-shaped pieces of a suspension promoter suspended coach industry unit with a mounting stored chassis unit of the vehicle, with the positioning device includes an attachment element Fixture for fixing the direction positioning to mount one of the fixture resistance element jointed affiliated gripping central carrier with a gripper attached to appropriation reach of the spring leg and shock damper, with the gripping means by moving the grief-structural funds his joints in a rest medium defined rest positions to warden can be brought, namely a working position in which the grief by the central taken one spring leg or shock absorbers positioned, and the suspension strut or shock absorbers are not positioned normally.

Abstract: A combination tool is provided that includes, but is not limited to a tool shaft with an inner part and an outer part, a first tool head that is integrally formed on the inner part and a differently designed second tool head that is integrally formed on the outer part. The tool shaft is realized in such a way that it can be inserted into a machine and features at least one holding element for mounting a tool head thereon in a locking fashion.

Abstract: In an exhaust gas treatment system and a utility vehicle having an exhaust gas treatment system, the exhaust gas treatment system includes a particle reduction unit, a reducing agent tank and a nitrogen oxide reduction unit of a modular design, wherein the reducing agent tank is arranged between the particle reduction unit and the nitrogen oxide reduction unit and extends around a connecting line extending between the particle reduction unit and the nitrogen oxide reduction unit, and in a utility vehicle, the associated exhaust gas treatment system is arranged within a predefined cuboid envelope volume on a support structure which is attached to a frame member of the vehicle.

Abstract: In an exhaust gas treatment system and a utility vehicle having an exhaust gas treatment system, the exhaust gas treatment system includes a particle reduction unit, a reducing agent tank and a nitrogen oxide reduction unit of a modular design, wherein the reducing agent tank is arranged between the particle reduction unit and the nitrogen oxide reduction unit and extends around a connecting line extending between the particle reduction unit and the nitrogen oxide reduction unit, and in a utility vehicle, the associated exhaust gas treatment system is arranged within a predefined cuboid envelope volume on a support structure which is attached to a frame member of the vehicle.

Abstract: Since, as a rule, there are several such PSTs on an aircraft, this results in a marked reduction in weight and aerodynamic drag, and savings in the required electric power in conjunction with a simultaneous increase in the accuracy of measurement of the angle of attack. All this permits a substantial increase in the competitiveness of the proposed fuselage Pitot-static tube.

Abstract: A Pitot-Static tube including three groups of orifices for determining the total pressure, static pressure and angle of attack, an axially symmetric body and a strut for fastening to pneumatic paths arranged between them and to electric heating elements. In order to reduce the aerodynamic drag of the Pitot-Static tube and the power required for heating the anti-icing system, the orifices for measuring the static pressure are arranged on a plate upstream of the strut.

Abstract: Since, as a rule, there are several such PSTs on an aircraft, this results in a marked reduction in weight and aerodynamic drag, and savings in the required electric power in conjunction with a simultaneous increase in the accuracy of measurement of the angle of attack. All this permits a substantial increase in the competitiveness of the proposed fuselage Pitot-static tube.

Abstract: The invention relates to a fuselage Pitot-static tube comprising three groups of orifices for determining the total pressure (2), static pressure (3) and angle of attack (6, 7), and an axisymmetric body (1) and strut (5) for mounting an anti-icing system having, arranged between them, airways (10) and electric heating elements (8). The orifices for determining the angle of attack are arranged on the strut, whose cross section is constructed in the form of a subsonic aerodynamic profile with a rounded-off nose or a tapered nose, and are arranged between the nose of the profile and the position of its maximum thickness.

Abstract: A sensor for measuring the relative velocity of an oncoming medium includes a tubular and preferably radially symmetrical sensor body having a leading front end, and a wall with an inner surface defining an axial hollow space being open to the outside at the leading front end. The sensor body includes a preferably streamlined sensor head portion associated with the front end, and a remainder of the sensor body forming a sensor shaft. The wall has at least one conduit being radial or having a radial component. The at least one conduit is separated from the axial hollow space and spaced apart from the front end. The at least one conduit is open to the outside from one of the portions. A method of measuring the relative velocity of the medium includes detecting a first measured value representing the sum of the static pressure and the velocity-dependent dynamic pressure of the medium with an axial pitostatic tube discharging at the front end of a sensor body.