Patent · US Active

Aircraft structural component that is adapted for absorbing and transmitting forces in an aircraft

US10399658B2 · kind B2 · utility

2Cited by

2References

20Claims

0Family size

Assignee

AIRBUS HELICOPTERS DEUTSCHLAND GMBH · DE

Inventors

Kaspar Von-Wilmowsky · Donauwörth, DE
Christian REICHENSPERGER · Asbach-Bäumenheim, DE
Andreas Rack · Hanau, DE

Key dates

Filing date	Jun 8, 2016
Grant date	Sep 3, 2019
Priority date	—
Expiry date	Oct 13, 2037

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF16B11/006
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

An aircraft structural component that is adapted for absorbing and transmitting forces in an aircraft, the aircraft structural component comprising at least one panel element and at least one reinforcing structure. The at least one reinforcing structure is rigidly attached to the at least one panel element such that at least one cavity is defined between the at least one panel element and the at least one reinforcing structure, the at least one cavity being adapted for distributing forces that are absorbed by the aircraft structural component in operation.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.