Hyundai motor company (20240336347). WING LOAD SUPPORT STRUCTURE OF THE FUSELAGE simplified abstract
Contents
WING LOAD SUPPORT STRUCTURE OF THE FUSELAGE
Organization Name
Inventor(s)
Won Ki Song of Seongnam-si (KR)
WING LOAD SUPPORT STRUCTURE OF THE FUSELAGE - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240336347 titled 'WING LOAD SUPPORT STRUCTURE OF THE FUSELAGE
The abstract of a patent application describes a wing load support structure for a fuselage, including joints on the front and rear spars of a wing unit, a center bulkhead, a spar cover, and a support unit.
- The first joint on the front spar of the wing unit is connected to the center bulkhead to support the vertical load of the front spar.
- The second joint on the rear spar of the wing unit is connected to the spar cover, which is in turn connected to the rear bulkhead by a bulkhead upper support.
- The support unit is designed to support the spar cover and the rear bulkhead inside the fuselage, handling the vertical load of the rear spar.
Potential Applications: - Aircraft design and manufacturing - Aerospace engineering - Structural support systems in other industries
Problems Solved: - Efficient distribution of wing loads within a fuselage - Enhanced structural integrity and support for wing units
Benefits: - Improved safety and stability of aircraft - Optimal weight distribution for better performance - Simplified maintenance and repair processes
Commercial Applications: Title: "Innovative Wing Load Support Structure for Aircraft" This technology could be utilized in the aviation industry for the design and construction of aircraft with enhanced structural support systems, potentially leading to safer and more efficient air travel.
Questions about the technology: 1. How does this wing load support structure improve the overall performance of an aircraft? - The detailed design of the support structure ensures optimal weight distribution and enhanced stability, contributing to improved aircraft performance. 2. What are the key differences between this innovative support structure and traditional wing load support systems? - This support structure offers a more efficient and effective way of distributing wing loads within a fuselage, providing better structural integrity and support for the aircraft.
Original Abstract Submitted
a wing load support structure of a fuselage includes a first joint on a front spar of a wing unit of the fuselage, a center bulk head including a first spar joint coupled to the first joint and configured to support a vertical load of the front spar transmitted by the wing unit, a second joint mounted on a rear spar of the wing unit, a spar cover including a second spar joint coupled to the second joint and connected to a rear bulk head by a bulk head upper support, and a support unit configured to support the spar cover and the rear bulk head inside the fuselage and configured to support a vertical load of the rear spar transmitted by the wing unit.
