Abstract: The invention relates in particular to an apparatus (100) for disinfecting at least one room, in particular for one or more persons, preferably a dwelling space or treatment room, for example a treatment room in a building, in particular a sickroom, a patient room and/or an operating theatre, by means of an atomiser. Specifically, the apparatus (100) is characterised in that the atomiser includes a rotatable bell cup (1) for atomising a disinfectant into the room. The invention relates to an associated method and furthermore to the use of a bell cup (1) for atomising a disinfectant in a room for, in particular, one or more persons.

Abstract: An air-outlet adjusting assembly for a motor vehicle includes a drive unit configured to be driven by an electric drive and configured to act on at least one pivotable valve flap and at least one pivotable guide slat. The drive unit includes a rotatably arranged sliding-block carrier having a sliding block arranged eccentrically thereon, wherein, in a first rotary motion segment of the sliding-block carrier, the sliding block is configured to engage in a valve-flap slotted link connected for conjoint rotation to the at least one valve flap and, in a second rotary motion segment of the sliding-block carrier, the sliding block is configured to engage in a guide-slat slotted link connected for conjoint rotation to the at least one guide slat.

Abstract: An air-outlet adjusting assembly for a motor vehicle includes a drive unit configured to be driven by an electric drive and configured to act on at least one pivotable valve flap and at least one pivotable guide slat. The drive unit includes a rotatably arranged sliding-block carrier having a sliding block arranged eccentrically thereon, wherein, in a first rotary motion segment of the sliding-block carrier, the sliding block is configured to engage in a valve-flap slotted link connected for conjoint rotation to the at least one valve flap and, in a second rotary motion segment of the sliding-block carrier, the sliding block is configured to engage in a guide-slat slotted link connected for conjoint rotation to the at least one guide slat.

Abstract: An interchangeable cumberbund with integrated wiring to allow for connecting a variety of electronic devices for an intended purpose or mission and exchanging a configured garment for another. The reconfigurable cumberbund allows for multiple quick-disconnect cable harnesses to be weaved into the cumberbund which enables rapid and convenient removal of hardware that incorporates all I/O to a computer. The reconfigurable cumberbund connected to a wearable tactical vest containing a mobile ultra-rugged personal computer is the essential combination that allows hands-free use by the user.

Abstract: An interchangeable cumberbund with integrated wiring to allow for connecting a variety of electronic devices for an intended purpose or mission and exchanging a configured garment for another. The reconfigurable cumberbund allows for multiple quick-disconnect cable harnesses to be weaved into the cumberbund which enables rapid and convenient removal of hardware that incorporates all I/O to a computer. The reconfigurable cumberbund connected to a wearable tactical vest containing a mobile ultra-rugged personal computer is the essential combination that allows hands-free use by the user.

Abstract: An interchangeable cumberbund with integrated wiring to allow for connecting a variety of electronic devices for an intended purpose or mission and exchanging a configured garment for another. The reconfigurable cumberbund allows for multiple quick-disconnect cable harnesses to be weaved into the cumberbund which enables rapid and convenient removal of hardware that incorporates all I/O to a computer. The reconfigurable cumberbund connected to a wearable tactical vest containing a mobile ultra-rugged personal computer is the essential combination that allows hands-free use by the user.

Abstract: A guidance electronics unit is provided for an explosively-launched vehicle, e.g., a projectile or missile, comprising a plurality of circuit card assemblies, each circuit card assembly containing a plurality of electronic components and interconnections, each circuit card assembly maintained in a housing and spaced apart. All spaces surrounding each circuit card assembly are filled with a granular material to provide support for each circuit card assembly during explosive launch. Further, a method for supporting circuit card assemblies in the guidance electronics unit is provided. The problem of enabling guidance electronics to survive the large loads encountered during an explosive launch out of a gun, such as a howitzer, or missile launch tube is thereby solved.

Abstract: A guidance electronics unit is provided for an explosively-launched vehicle, e.g., a projectile or missile, comprising a plurality of circuit card assemblies, each circuit card assembly containing a plurality of electronic components and interconnections, each circuit card assembly maintained in a housing and spaced apart. All spaces surrounding each circuit card assembly are filled with a granular material to provide support for each circuit card assembly during explosive launch. Further, a method for supporting circuit card assemblies in the guidance electronics unit is provided. The problem of enabling guidance electronics to survive the large loads encountered during an explosive launch out of a gun, such as a howitzer, or missile launch tube is thereby solved.

Abstract: Energy (110) and mission data (108) for a guided projectile are transferred from a projectile setter (102) over an inductive interface (118). The projectile may include energy storage element (114) to store the energy and a data storage element (112) to store the mission data. Precision GPS clock circuitry (316) of the projectile may receive power from a capacitive energy storage (304) element during projectile loading until a flight battery (320) is activated. In one embodiment, the capacitive energy storage element (304) includes at least one super capacitor (322) and a gun-hardened capacitor (324). The clock circuitry (316) may receive power from the gun-hardened capacitor (324) if the super capacitor (322) fails during the launching operation. The capacitive energy storage element (304) may include one-way energy transfer elements (326) coupled between the super capacitor (322) and the gun-hardened capacitor (324).

Abstract: Energy (110) and mission data (108) for a guided projectile are transferred from a projectile setter (102) over an inductive interface (118). The projectile may include energy storage element (114) to store the energy and a data storage element (112) to store the mission data. Precision GPS clock circuitry (316) of the projectile may receive power from a capacitive energy storage (304) element during projectile loading until a flight battery (320) is activated. In one embodiment, the capacitive energy storage element (304) includes at least one super capacitor (322) and a gun-hardened capacitor (324). The clock circuitry (316) may receive power from the gun-hardened capacitor (324) if the super capacitor (322) fails during the launching operation. The capacitive energy storage element (304) may include one-way energy transfer elements (326) coupled between the super capacitor (322) and the gun-hardened capacitor (324).