Abstract: A refrigeration appliance has a refrigeration appliance component and a cleaning device for cleaning the component. The cleaning device includes a cleaning element, an actuating element, and a connection element. The cleaning element is connected to the actuating element by the connection element. The refrigeration appliance has a cavity which extends from the front side of the refrigeration appliance to the back side of the refrigeration appliance, and in which the connection element is accommodated. The cleaning element is moveable across a surface of the refrigeration appliance component upon actuation of the actuating element in order to remove dirt deposits from the surface of the refrigeration appliance component.

Abstract: A hoist, a hoisting apparatus with said hoist and a method for securing a hoist. A hoist body having a drive mechanism for raising or lowering a hoist chain or a hoist cable is suspended from a support device by a hoist support. A safety device having a loosely arranged coupling element and a damping element is mounted between the hoist body and the support device. If the hoist support is released, the hoist body can drop by a drop height until the coupling element becomes taut. The damping element then damps the fall under the load of the hoist body, the hoist chain and whatever load is suspended from it.

Abstract: A plug connector part includes a housing having first and second housing parts. The housing parts are joined together parallel to a plug contact insertion direction. The housing parts have lateral surfaces which face one another when the housing parts are joined together. The housing parts have parallel grooves at their lateral surfaces. The grooves form plug contact receiving channels when the housing parts are joined together. The plug contacts have lances which engage projections of the receiving channels when the plug contacts are fully received within the receiving channels. The first housing part includes spring tongues along the grooves of the first housing part for fixing the plug contacts within the receiving channels. The spring tongues have tab-like sections which extend into the receiving channels and engage the plug contacts to fix the plug contacts within the receiving channels in a form-fit manner.

Abstract: A plug connector part includes a housing having first and second housing parts. The housing parts are joined together parallel to a plug contact insertion direction. The housing parts have lateral surfaces which face one another when the housing parts are joined together. The housing parts have parallel grooves at their lateral surfaces. The grooves form plug contact receiving channels when the housing parts are joined together. The plug contacts have lances which engage projections of the receiving channels when the plug contacts are fully received within the receiving channels. The first housing part includes spring tongues along the grooves of the first housing part for fixing the plug contacts within the receiving channels. The spring tongues have tab-like sections which extend into the receiving channels and engage the plug contacts to fix the plug contacts within the receiving channels in a form-fit manner.

Abstract: A clutch actuator for transmitting a disengaging force to a disengaging device of a clutch includes an actuating element to which the disengaging force can be applied and includes a piston rod for transmitting the disengaging force from the actuating element to the disengaging device. The piston rod is mounted against a connection region of the actuating element such that the piston rod can be moved towards the connection region by the clutch reaction force of the clutch, and the positioning of the connection region and the piston rod relative to each other as a result of the movement can be fixed by applying the disengaging force to the actuating element. The actuating element is designed to at least partly deflect the disengaging force so as to produce a normal force and/or a radial force which acts between the connection region and the piston rod, and the normal force and/or the radial force fixes the position of the connection region and the piston rod relative to each other.

Abstract: The present disclosure relates to reversal agents, which specifically bind to anti-Factor XI and/or anti-Factor XIa antibodies, and reverse one or more anticoagulant effects of the anti-Factor XI and/or anti-Factor XIa antibodies, as well as to methods of use thereof, such as methods for reversing anticoagulant effects of such anti-Factor XI and/or anti-Factor XIa antibodies, and to related methods for managing bleeding or bleeding risks.

Abstract: A refrigeration appliance has a refrigeration appliance component and a cleaning device for cleaning the component. The cleaning device includes a cleaning element, an actuating element, and a connection element. The cleaning element is connected to the actuating element by the connection element. The refrigeration appliance has a cavity which extends from the front side of the refrigeration appliance to the back side of the refrigeration appliance, and in which the connection element is accommodated. The cleaning element is moveable across a surface of the refrigeration appliance component upon actuation of the actuating element in order to remove dirt deposits from the surface of the refrigeration appliance component.

Abstract: A refrigerating device has an evaporator, a fan, a fan housing for generating an air flow on the evaporator, and a bearing shell for retaining the fan housing on the evaporator in a vibration-decoupled manner. The fan housing has at least one first bearing pin and a second bearing pin. The bearing shell has at least one first receiving recess for receiving the first bearing pin in a pivotal manner and a second receiving recess for receiving the second bearing pin, and a pivotal locking element is provided for locking the second bearing pin in the second receiving recess.

Abstract: The invention relates to a refrigerating device comprising an evaporator, comprising a fan and a fan housing for generating an air flow on the evaporator, and comprising a bearing shell for retaining the fan housing on the evaporator in a vibration-decoupled manner. The fan housing has at least one first bearing pin and a second bearing pin. The bearing shell has at least one first receiving recess for receiving the first bearing pin in a pivotal manner and a second receiving recess for receiving the second bearing pin, and a pivotal locking element is provided for locking the second bearing pin in the second receiving recess.

Abstract: An aircraft capable of making short takeoffs and landings includes essentially a fuselage, a wing secured to the fuselage, a front horizontal stabilizer secured to the fuselage on the front end of the fuselage and at least two jet engines for propulsion. According to the architecture proposed, the propulsion engines are arranged side by side above the fuselage in a rear part of the fuselage with a width at least equal to the width of the propulsion group, a fuselage flap device is arranged in the back of the fuselage so that the fuselage flaps adopt at least a position in which the flaps are considerably in a horizontal plane and take at least a high-lift position in which the flaps are turned downward in such a way that the blast created by the jet engines is channeled towards the top surface of the fuselage flaps to induce a blowing effect.

Abstract: An aircraft, the propulsive units of which include engines, and which is distinguished by reduced noise emissions, includes a wing structure fixed to an upper region of the fuselage, and a vertical tail system having at least two vertical stabilizers which are generally vertically fixed to the fuselage aftwardly of the wing structure. The engines are disposed side by side in a propulsive package disposed above the fuselage, which propulsive package includes the following: air inlet openings for the propulsive package, which openings are disposed above the fuselage between a point at the leading edge and a point at the trailing edge of an aerodynamic root chord of the wing structure; and exhaust nozzle conduit outlets associated with exhaust nozzle conduits, which outlets are formed by the structure (cowling structure) of the propulsive package, and are disposed above the fuselage forwardly of an aft terminus of the fuselage and between the vertical stabilizers.

Abstract: A force-moment sensor is provided for measuring at least one force and/or moment, which comprises a first part, a second part and an optical fibre arranged therebetween, said optical fibre comprising in at least one section a component for detecting deformations and/or stresses of the fibre transversely to its longitudinal axis. The present invention further relates to a method for measuring forces and/or moments. Thus, a fibre is provided which comprises at least one component for detecting deformations and/or stresses of the fibre transversely to a longitudinal axis of the fibre and into which light is introduced. According to this method, a force and/or moment acts on the fibre, wherein at least one component of the force and/or moment acts perpendicularly to the longitudinal axis of the fibre. The light reflected in the fibre is then detected and the detected spectrum analysed.

Abstract: An RF isolation container that includes a counterweight system to assist an operator with opening and closing operations, an electromagnet locking mechanism for easier and consistent locking of the RF isolation container and a motion damping mechanism to relieve fatigue on operating components and on human operators.

Abstract: An improved test probe assembly has an improved mounting assembly which provides the test probe multi-directional freedom of movement with respect to a base in order to resist damage frequently caused to the test probe. The improved mounting assembly may, for example, include at least a first resilient mount disposed on the base and having at least a first support and at least a first resilient element. The at least a first resilient element, which may, for example, be at least a first spring, is deflectable when the test probe engages a structure, such as a device under testing (DUT). Accordingly, the improved test probe assembly of the invention can be deflected an infinite number of positions, in order to resist damage caused, for example, by misalignment between the probe and the DUT.

Abstract: An improved test probe assembly has an improved mounting assembly which provides the test probe multi-directional freedom of movement with respect to a base in order to resist damage frequently caused to the test probe. The improved mounting assembly may, for example, include at least a first resilient mount disposed on the base and having at least a first support and at least a first resilient element. The at least a first resilient element, which may, for example, be at least a first spring, is deflectable when the test probe engages a structure, such as a device under testing (DUT). Accordingly, the improved test probe assembly of the invention can be deflected an infinite number of positions, in order to resist damage caused, for example, by misalignment between the probe and the DUT.

Abstract: A fixture is provided for functional testing of an assembled wireless device. The wireless device has a first port and a second port. The fixture comprises: a base having an opening formed therein for receiving a retainer, the retainer being rotatably mounted in the opening for rotating from a first position to a second position, the retainer for receiving the wireless device while in the first position; a first connector mounted in the retainer for engaging the first port of the wireless device when the wireless device is received by the retainer in the first position; and a second connector rotatably mounted on the base, the second connector for engaging the second port of the wireless device when the retainer is rotated to the second position.

Abstract: An aircraft the propulsive units of which include engines, and which is distinguished by reduced noise emissions, includes a wing structure fixed to an upper region of the fuselage, and a vertical tail system having at least two vertical stabilizers which are generally vertically fixed to the fuselage aftwardly of the wing structure. The engines are disposed side by side in a propulsive package disposed above the fuselage, which propulsive package includes the following, air inlet openings for the propulsive package, which openings are disposed above the fuselage between a point at the leading edge and a point at the trailing edge of an aerodynamic root chord of the wing structure; and exhaust nozzle conduit outlets associated with exhaust nozzle conduits, which outlets are formed by the structure (cowling structure) of the propulsive package, and are disposed above the fuselage forwardly of an aft terminus of the fuselage and between the vertical stabilizers.

Abstract: An improved test probe assembly has an improved mounting assembly which provides the test probe multi-directional freedom of movement with respect to a base in order to resist damage frequently caused to the test probe. The improved mounting assembly may, for example, include at least a first resilient mount disposed on the base and having at least a first support and at least a first resilient element. The at least a first resilient element, which may, for example, be at least a first spring, is deflectable when the test probe engages a structure, such as a device under testing (DUT). Accordingly, the improved test probe assembly of the invention can be deflected an infinite number of positions, in order to resist damage caused, for example, by misalignment between the probe and the DUT.

Abstract: An RF isolation container that includes a counterweight system to assist an operator with opening and closing operations, an electromagnet locking mechanism for easier and consistent locking of the RF isolation container and a motion damping mechanism to relieve fatigue on operating components and on human operators.

Abstract: An RF isolation container that includes a counterweight system to assist an operator with opening and closing operations, an electromagnet locking mechanism for easier and consistent locking of the RF isolation container and a motion damping mechanism to relieve fatigue on operating components and on human operators.