Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies

Patent metadata

Field	Value
Publication number	US-9731808-B2
Application number	US-201615266779-A
Country	US
Kind code	B2
Filing date	Sep 15, 2016
Priority date	Aug 23, 2013
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

An upper joint of a wing assembly of an aircraft includes an outboard upper wing panel, a center upper wing panel, a rib, and an upper joint assembly operatively interconnecting the outboard upper wing panel, the center upper wing panel, and the rib. For a substantial fore/aft span of the upper joint, a first subset of a plurality of center upper stringers is operatively coupled to the upper joint assembly, and a second subset of the plurality of center upper stringers terminates without being directly coupled to the upper joint assembly.

First claim

The invention claimed is:

1. An upper joint for a wing assembly of an aircraft, the upper joint comprising:
an outboard upper wing panel of an outboard wing box, wherein the outboard upper wing panel includes an outboard upper skin and a plurality of outboard upper stringers operatively coupled to the outboard upper skin;
a center upper wing panel of a wing center section, wherein the center upper wing panel includes a center upper skin and a plurality of center upper stringers operatively coupled to the center upper skin;
a rib that is located between the outboard wing box and the wing center section; and
an upper joint assembly operatively interconnecting the outboard upper wing panel, the center upper wing panel, and the rib;
wherein for a first substantial fore/aft span of the upper joint:
the plurality of outboard upper stringers comprises hat-shaped stringers;
a first subset of the plurality of center upper stringers is operatively coupled to the upper joint assembly, wherein the first subset of the plurality of center upper stringers comprises hat-shaped stringers; and
a second subset of the plurality of center upper stringers terminates without being directly coupled to the upper joint assembly, wherein the second subset of the plurality of center upper stringers comprises blade stringers, Z-stringers, or I-stringers.

2. The upper joint of claim 1 , wherein the center upper stringers of the second subset of the plurality of center upper stringers are not directly opposed to corresponding outboard upper stringers of the plurality of outboard upper stringers at the upper joint assembly.

3. An aircraft, comprising:
a fuselage; and
a wing assembly operatively coupled to the fuselage, wherein the wing assembly includes:
a left wing box;
a right wing box;
a wing center section; and
two upper joints according to claim 1 , including a left upper joint and a right upper joint, wherein the left upper joint interconnects the left wing box and the wing center section, and wherein the right upper joint interconnects the right wing box and the wing center section.

4. The upper joint of claim 1 , wherein the upper joint assembly includes:
an outboard flange operatively coupled to the outboard upper wing panel;
an inboard flange operatively coupled to the center upper wing panel;
a lower flange operatively coupled to the rib;
a plurality of outboard compression fittings operatively coupled between the outboard upper wing panel and the lower flange; and
a plurality of inboard compression fittings operatively coupled between the center upper wing panel and the lower flange.

5. The upper joint of claim 4 , wherein the upper joint assembly includes:
a splice plate, wherein the splice plate defines the outboard flange and the inboard flange; and
a lower T-fitting operatively coupled to the splice plate, wherein the lower T-fitting defines the lower flange.

6. The upper joint of claim 5 , wherein the upper joint assembly further includes:
an upper T-fitting operatively coupled to the splice plate opposite the lower T-fitting.

7. The upper joint of claim 5 ,
wherein the outboard upper wing panel is constructed substantially of a first material;
wherein the center upper wing panel is constructed substantially of a second material that is different from the first material; and
wherein the splice plate and the lower T-fitting are constructed of a third material that is different from the first material and the second material.

8. The upper joint of claim 7 , wherein the first material is a fiber reinforced composite material, wherein the second material is an aluminum alloy, and wherein the third material is a titanium alloy.

9. The upper joint of claim 1 , wherein for a second substantial fore/aft span of the upper joint:
the plurality of outboard upper stringers comprises blade stringers, Z-stringers, or I-stringers;
a third subset of the plurality of center upper stringers is operatively coupled to the upper joint assembly, wherein the third subset of the plurality of center upper stringers comprises blade stringers, Z-stringers, or I-stringers; and
a fourth subset of the plurality of center upper stringers terminates without being directly coupled to the upper joint assembly, wherein the fourth subset of the plurality of center upper stringers comprises blade stringers, Z-stringers, or I-stringers.

10. The upper joint of claim 9 , wherein the center upper stringers of the fourth subset of the plurality of center upper stringers are not directly opposed to corresponding outboard upper stringers of the plurality of outboard upper stringers at the upper joint assembly.

11. An upper joint for a wing assembly of an aircraft, the upper joint comprising:
an outboard upper wing panel of an outboard wing box, wherein the outboard upper wing panel includes an outboard upper skin and a plurality of outboard upper stringers operatively coupled to the outboard upper skin;
a center upper wing panel of a wing center section, wherein the center upper wing panel includes a center upper skin and a plurality of center upper stringers operatively coupled to the center upper skin;
a rib that is located between the outboard wing box and the wing center section; and
an upper joint assembly operatively interconnecting the outboard upper wing panel, the center upper wing panel, and the rib;
wherein for a first substantial fore/aft span of the upper joint:
the plurality of outboard upper stringers comprises hat-shaped stringers;
a first subset of the plurality of center upper stringers is operatively coupled to the upper joint assembly, wherein the first subset of the plurality of center upper stringers comprises hat-shaped stringers; and
a second subset of the plurality of center upper stringers terminates without being directly coupled to the upper joint assembly, wherein the center upper stringers of the second subset of the plurality of center upper stringers comprise blade stringers, Z-stringers, or I-stringers and are not directly opposed to corresponding outboard upper stringers of the plurality of outboard upper stringers at the upper joint assembly; and

wherein for a second substantial fore/aft span of the upper joint:
the plurality of outboard upper stringers comprises blade stringers, Z-stringers, or I-stringers;
a third subset of the plurality of center upper stringers is operatively coupled to the upper joint assembly, wherein the third subset of the plurality of center upper stringers comprises blade stringers, Z-stringers, or I-stringers; and
a fourth subset of the plurality of center upper stringers terminates without being directly coupled to the upper joint assembly, wherein the center upper stringers of the fourth subset of the plurality of center upper stringers comprise blade stringers, Z-stringers, or I-stringers and are not directly opposed to corresponding outboard upper stringers of the plurality of outboard upper stringers at the upper joint assembly.

12. An aircraft, comprising:
a fuselage; and
a wing assembly operatively coupled to the fuselage, wherein the wing assembly includes:
a left wing box;
a right wing box;
a wing center section; and
two upper joints according to claim 11 , including a left upper joint and a right upper joint, wherein the left upper joint interconnects the left wing box and the wing center section, and wherein the right upper joint interconnects the right wing box and the wing center section.

13. The upper joint of claim 11 , wherein the upper joint assembly includes:
an outboard flange operatively coupled to the outboard upper wing panel;
an inboard flange operatively

Assignees

• Boeing Co

Inventors

• Charles Jordan Daniel
• Hamada Jason

Classifications

• B64C1/26 Primary

  Attaching the wing or tail units or stabilising surfaces · CPC title

• B64C2001/0072

  from composite materials · CPC title

• B64C3/187

  Ribs · CPC title

• B64C3/00

  Wings (ornithopter wings B64C33/02) · CPC title

• B64C2001/0081

  from metallic materials · CPC title