| Patent application number | Description | Published |
|---|
| 20090095004 | SYSTEM FOR PRODUCING AIR - A system for the provision of process air comprises a first cooling system ( | 04-16-2009 |
| 20090255277 | OPTIMIZED DEFROSTING REGULATION OF PARALLEL ARRANGED FRESH AIR OUTLETS OF AIR CONDITIONERS - An arrangement is provided for de-icing pipeline connections of an aircraft, which are connected to all fresh air outlets of an air conditioner, whose construction includes, but is not limited to the functions of multiple turbines and heat exchangers, having a first pipeline, which is connected to a first turbine, and a second pipeline, which is connected to a second turbine, the two pipelines, which are each connected downstream from the two turbines and to which process air is fed at the turbine outlets, being connected at the pipe ends and being continued using a third pipeline. The arrangement is characterized in that a first hot air source is fed hot fresh air from a bleed air system of the aircraft and is connected at its outlet to a fourth pipeline, into which temperature-reduced fresh air is fed from the hot air source. The fourth pipeline is connected at its pipe end to two further valve-regulated pipelines, of which a fifth or a sixth pipeline is connected to the first or the second pipeline, and through which temperature-reduced fresh air is transported and fed valve-regulated to the first and/or second pipeline. | 10-15-2009 |
| 20090308978 | Relief valve for being arranged on an opening of a fuselage shell of an aircraft, fuselage part with such a relief valve and aircraft fuselage - The invention pertains to a relief valve ( | 12-17-2009 |
| 20100101251 | Method And System For Controlling An Aircraft Air Conditioning System With Optimised Fuel Consumption - In a method for controlling an aircraft air conditioning system ( | 04-29-2010 |
| 20110111683 | System For Ventilation Of An Aircraft Area | 05-12-2011 |
| 20110177771 | System For Cooling An Aircraft Zone, To Be Connected To An Aircraft-External Air Unit | 07-21-2011 |
| 20110247432 | Aircraft Conduit Monitoring System And Method - The invention relates to an aircraft conduit monitoring system comprising a conduit that conducts gas from a source to a point of application. A flow sensing device and a pressure sensing device are provided within the conduit. At least one set value of a gas mass flow rate and at least one set value of a pressure are sensed in a learning mode of operation. Said set values are compared with sensed actual values in the normal mode of operation. A gas volume flow rate can also be sensed and processed instead of a gas mass flow rate. | 10-13-2011 |
| 20110283713 | System For Cooling A Heat Exchanger On Board An Aircraft | 11-24-2011 |
