About 31 results
https://drivepatents.com/patents/1015403 · 2 Mar 2011
A supply system (100) for the energy supply in an aircraft comprising an engine (101) for propelling an aircraft, a fuel cell (102) for supplying an aircraft with electric energy, a first fuel reservoir (103) for supplying the engine (101) with engine fuel...
https://drivepatents.com/patents/1067542 · 10 May 2006
The mounting device has a support element (101), a first belt rewinder (102) with a rollable belt (103) and with a fitting (104), a second rewinder belt (106) with a rollable belt (107) and with a fitting (108) whereby the first belt rewinder and the secon...
https://drivepatents.com/patents/1067918 · 26 Apr 2006
The unit has a two dimensional light source (1) and a partial translucent screen (2). The light source is connected to the translucent screen by an attachment unit (3), where the screen partially shining. The light source is arranged behind the translucent...
https://drivepatents.com/patents/1068141 · 19 Apr 2006
The cover for a gap (5) between a first (3) and a second (4) element in an aircraft has a cover section (2) to cover the gap, and a clamping element (6) for the fastening of the cover on a third element in such a way that the first and second elements are ...
https://drivepatents.com/patents/1068730 · 29 Mar 2006
A fuel cell (1) rotates on bearings. A first non-positive link (9,10) is set up between the fuel cell and a motor (12). Energy can be transferred from the motor onto the fuel cell via the first non-positive link, so that the fuel cell can be made to rotate...
https://drivepatents.com/patents/1069154 · 22 Mar 2006
The seat has a seat part and a backrest (20) fitted to the seat mounting (30). It has at least one free-bearing bearer beam (31) supported on the mounting foot (32); and at least two seat parts (33) fixed to the bearer beam. It has a bearer bolt which can ...
https://drivepatents.com/patents/1071145 · 4 Jan 2006
The present invention relates to a holder for a panel such as a light cover in an aircraft. According to an exemplary embodiment of the present invention a mounting section, a shoe receiving section and a pin are adapted such that a pin and shoe principle ...
https://drivepatents.com/patents/1072097 · 30 Nov 2005
The aircraft has a supply system with first electrochemical reactor (1) for generating energy, hydrogen, oxygen and clear water from grey water, hydrocarbon fuel and air, whereby the first reactor at least partly forms at least one of the systems selected ...
https://drivepatents.com/patents/1072093 · 30 Nov 2005
The electrochemical reactor has a fuel cell arrangement, an electrolytic cell arrangement and a fuel processing arrangement (6), whereby the electrochemical reactor can be used to generate energy, hydrogen, oxygen and clear water from grey water (5), a fue...
https://drivepatents.com/patents/1072275 · 23 Nov 2005
The aircraft seat has a seat element and backrest element with a resetting element (16) acting on the pivotal seat or backrest element. The seat element defines a first volume and the backrest element defines a second volume with the resetting element moun...