This invention relates to aircraft structure, and has particular reference to a novel structure for an aeroplane wing, elevator, rudder, aileron, wing flap, and like parts. It is a well recognized fact that an aeroplane wing having a given area, span and taper will provide definite advantages...
This is an aircraft having variable wing formation of novel form, one formation for landing and take-off performance and another formation for cruising speeds. A novel form of wing actuation for such formation and a form of control for actuation is included. A novel form of structure of the ...
Wing parts () which influence the lift of aircraft wings (), especially wings () with a cross section and an angle of attack which is suitable for high-speed flight, which parts can be moved out of an aerodynamically inactive servicing position within the aircraft fuselage () or out of ...
In turbulence, however, its wing root structural material would enjoy a more favorable position on the Goodman Diagram, so as to improve the wing structure's fatigue life. If such a system were found to be advantageous for an operational aircraft in the part of preliminary design concerned ...
As per [4], failure of APU rotating parts result in high EGT, high oil consumption, and low power outputs. In Ref. [11], APU failure results have been categorized into two groups; those which can be fixed on-wing by replacing faulty Line Replaceable Units (LRU) and those which require...
This paper is categorized into two parts. (1) A frame work to design the aircraft wing structure and (2) analysis of a morphing airfoil with auxetic structure. The developed design frame work in the first part is used to arrive at the sizes of the various components of an aircraft wing ...
Damage tolerance based design optimisation of a fuel flow vent hole in an aircraft structure This paper investigates the design optimisation of a fuel flow vent hole (FFVH) located in the wing pivot fitting (WPF) of an F-111 aircraft assuming a dam... R Das,R Jones - 《Structural & Mul...
I dont want to build an immovable rigid wing that would overload the bolt joints. So my thought is to do a strength analysis of the truss structure. I've never done something like that's real/that complex. I have solidworks with its Simulation add in... What do I need to do to...
1.A supporting wing structure (3) for an aircraft (1), said supporting wing structure comprising:a plurality of struts (4,4a,4b), a first number of the struts (4a) are primarily disposed in a first direction (R1), and a second number of the struts (4b) are primarily disposed in a...
US aircraft manufacturer will bring parts supplier back under its wing after two decades apart June 25 2024 LexAirbus SE Airbus shows the limits of duopoly powerPremiumcontent Supply capacity is not an area where the European group can profit from the distress of its rival Boeing ...