Patent ID: 9617008
Date: 2017-04-11
CPC Classifications: B61D,B64C,B64D,B64F

Claim:
1. An aircraft comprising, as a structure for mounting a device to be installed outside the aircraft onto an airframe: a penetration member which penetrates the airframe inwardly and outwardly through an opening included in the airframe, and has a portion to be provided with the device and a portion located inside the aircraft; a seat support member which supports a seat disposed inside the aircraft, the seat support member comprising a first rail member and a second rail member disposed in parallel to each other in a front-rear direction along a floor of the aircraft, wherein the first rail member and the second rail member each comprise a plurality of engaging parts at regular intervals along the front-rear direction; and a load transmission member which is connected with the penetration member inside the aircraft and transmits a load input from the penetration member to the seat support member.