View source for 17937971. TUBULAR WING STRUCTURES AND METHODS OF MANUFACTURE simplified abstract (The Boeing Company)

=TUBULAR WING STRUCTURES AND METHODS OF MANUFACTURE=


==Organization Name==

[[:Category:The Boeing Company|The Boeing Company]]


[[Category:The Boeing Company]]

==Inventor(s)==

[[:Category:Jonathan Gabrys of Downington PA (US)|Jonathan Gabrys of Downington PA (US)]][[Category:Jonathan Gabrys of Downington PA (US)]]

[[:Category:Megan Prucnal of Wallingford PA (US)|Megan Prucnal of Wallingford PA (US)]][[Category:Megan Prucnal of Wallingford PA (US)]]

[[:Category:Kevin Michael Drayer of Media PA (US)|Kevin Michael Drayer of Media PA (US)]][[Category:Kevin Michael Drayer of Media PA (US)]]

[[:Category:Daniel Stephen Kraynik of West Chester PA (US)|Daniel Stephen Kraynik of West Chester PA (US)]][[Category:Daniel Stephen Kraynik of West Chester PA (US)]]

==TUBULAR WING STRUCTURES AND METHODS OF MANUFACTURE - A simplified explanation of the abstract==


This abstract first appeared for US patent application 17937971 titled 'TUBULAR WING STRUCTURES AND METHODS OF MANUFACTURE

==Simplified Explanation==

The abstract describes a wing structure with a unitary body formed by tubular sections arranged side-by-side, creating internal spar structures that eliminate the need for non-integral spars or fasteners. The structure can be overwrapped with composite material for added strength.

* Tubular sections arranged side-by-side
* Internal spar structures created by adjacent walls of tubular sections
* Eliminates need for non-integral spars or fasteners
* Can be overwrapped with composite material for additional strength

== Potential Applications ==
The technology could be applied in aircraft manufacturing, specifically in the construction of wings for airplanes and drones.

== Problems Solved ==
This innovation eliminates the need for additional spars and fasteners in wing structures, simplifying the manufacturing process and reducing weight.

== Benefits ==
The unitary body design reduces weight and complexity in wing structures, potentially leading to improved fuel efficiency and performance in aircraft.

== Potential Commercial Applications ==
This technology could be utilized by aircraft manufacturers looking to streamline production processes and enhance the performance of their products.

== Possible Prior Art ==
There may be prior art related to composite materials used in aircraft wing structures, but the specific design of a unitary body formed by tubular sections creating internal spar structures may be a novel approach.

=== Unanswered Questions ===

=== How does this technology impact the overall cost of manufacturing aircraft wings? ===
The article does not provide information on the cost implications of implementing this technology in aircraft wing production. 

=== What are the potential challenges in integrating this design into existing aircraft manufacturing processes? ===
The article does not address any potential challenges that may arise when incorporating this innovative wing structure design into current aircraft manufacturing practices.


==Original Abstract Submitted==

A wing structure having a unitary body formed by a plurality of tubular sections that are arranged side-by-side and configured such that adjacent internal walls of the tubular sections create internal spar structures that substantially reduce or eliminate the need for non-integral spars, or for fasteners to attach conventional spars and ribs into the wing skins. The unitized structure formed by the plurality of tubular sections can be further overwrapped with a composite material to provide additional strength to the wing structure.



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