A method for facilitating the design and manufacturing of a tiltrotor aircraft, including the steps of: determining a compatible mission data set; identifying lift propulsion module components for the compatible mission data set; determining compatible specifications; and generating a design for a lift propulsion module; wherein the lift propulsion module is configured to be connected to at least two different fuselages. There is also a method of designing a tiltrotor aircraft, comprising the step of modularizing a lift propulsion system, wherein the lift propulsion system is configured to be connected to at least two different fuselages. In another aspect, there is a tiltrotor aircraft including a fuselage; and a lift propulsion module, the lift propulsion module including a mounting surface; wherein the lift propulsion module is coupled to the fuselage on the mounting surface. Also included are methods of assembling and systems including a lift propulsion module.
LIFT PROPULSION MODULE FOR A TILTROTOR AIRCRAFT
2019-01-31
Patent
Electronic Resource
English
TILTROTOR PROPULSION SYSTEM FOR AN AIRCRAFT AND AIRCRAFT HAVING A TILTROTOR PROPULSION SYSTEM
European Patent Office | 2018
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