Rolls-royce Deutschland Ltd & Co. Kg

Rolls-royce Corporation

Dräger Safety Ag&co. Kgaa

Björn Petersen

Hans-Ullrich Hansmann

Andrea Minelli

Ivo Martin

Marcus Romba

Thomas Pernot

Philip Brian Walker

Lutz Rüffert

Sandra Dankertt

A planetary gearbox device includes a static ring gear, a rotatable planet carrier, a plurality of planet gears, each planet gear being connected to a bearing device, wherein at least one of the bearing devices is coupled to at least one lubricant scooping device and/or at least one lubricant reservoir device for collecting lubricant, in particular oil coming from the at least one bearing device, and at least one lubricant channel allows a flow of the collected lubricant towards a lubrication location and/or a lubricant supply for the planetary gearbox device.

Planetary gearbox device and gas turbine engine with a planetary gearbox device

A gas turbine engine for an aircraft, including the following: a core engine including a turbine, a compressor, and a core shaft connecting the turbine to the compressor; a fan, which is positioned upstream of the core engine, wherein the fan includes a plurality of fan blades; and a gear box which can be driven by the core shaft, wherein the fan can be driven at a lower rotational speed than the core shaft by means of the gear box, wherein the core shaft is designed as a drive shaft for the gear box and has at least one axial first region which has a diameter greater than the diameter of at least one axial second region, wherein the at least one first region is arranged axially between the drive side of the gear box and a mounting and/or attachment on a static part of the gas turbine engine.

Gas turbine engine

A breathing apparatus includes a filter, a motor and a blower driven by the motor. The filter is disposed ahead of the blower and the blower is configured to generate an air volume flow over the filter. A data storage unit has calibration curves for the air volume flow stored therein and the calibration curves are provided in characteristic line fields referenced to a known ambient pressure (p, p). Each of the characteristic line fields has a reference calibration curve referred to a predetermined operating state. A control unit is connected to the motor and the data storage unit. The control unit is configured to extrapolate one of the characteristic line fields for the operation of the motor by comparing a calibration curve ({dot over (V)}) for an unknown ambient pressure (p) recorded at a predetermined operating state with a reference calibration curve.

Breathing apparatus with compensation of the ambient pressure

Growing community of inventors

Berlin, Germany

Björn Petersen