Patent ID: 9428258
Filing Date: 2016-08-30
CPC Classification: B29L,B32B,B60R,B64C,B64D,E04B,E04H,Y02T

Claim Text:
1. A holding device for an interior lining part of a fuselage, the holding device comprising: a supporting device, which is configured to anchor the holding device on a structure of the fuselage and comprises a joint, a connecting tube, which extends out of the supporting device and has one end attached to the joint, a mounting for an interior lining part, wherein another end of the connecting tube is attached to said mounting, the another end being opposite to the one end, so that the mounted connecting tube defines a first distance between the supporting device and the mounting, a slacked lanyard fastened to the supporting device and the mounting and extending through the connecting tube, wherein the lanyard becomes straightened out and holds the supporting device and the mounting together in the event that the connecting tube breaks and separates, wherein the lanyard in its straightened out condition defines a second distance between the supporting device and the mounting, wherein the second distance is greater than the first distance, and wherein said one end of the connecting tube is directly attached to a hemispherical joint body of the joint, said another end of the connecting tube is directly attached to an adjusting sleeve of the mounting, one end of the lanyard is attached to said hemispherical joint body, and another end of the lanyard is attached to said adjusting sleeve, wherein the first distance and the second distance are between the hemispherical joint body and the adjusting sleeve.