An interior trim arrangement for an aircraft cabin, having lateral ceiling elements, and an angled element having limbs limb extending from one another, one lateral ceiling element arranged offset upwardly and to a first side, the angled element arranged with the first limb adjoining a lateral ceiling element towards the first side, the free end of the first limb located opposite the free end, towards the first side, of a lateral ceiling element, the other limb extending towards the other lateral ceiling element, the free end of the second limb spaced apart from the first free end, towards a lateral ceiling element, of the other lateral ceiling element, a light source for the other lateral ceiling element between the free end of the second limb and the first free end, towards a lateral ceiling element, of the other lateral ceiling element, and the angled element having a lighting element.
INTERIOR TRIM ARRANGEMENT FOR AN AIRCRAFT CABIN
2015-08-20
Patent
Electronic Resource
English
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