Wing flap with torque member and method for forming thereof

Patent metadata

Field	Value
Publication number	US-10759516-B2
Application number	US-201815941320-A
Country	US
Kind code	B2
Filing date	Mar 30, 2018
Priority date	Mar 30, 2018
Publication date	Sep 1, 2020
Grant date	Sep 1, 2020

Abstract

A wing flap includes a flap body and a torque member. The torque member is integrally formed with at least a portion of the flap body.

First claim

What is claimed is:

1. A wing flap comprising:
at least three spars, wherein each one of at least the three spars comprises a spar major portion and a spar extension portion that extends from the spar major portion;
an upper skin, coupled to at least the three spars and comprising an upper-skin major portion and an upper-skin extension portion that extends from the upper-skin major portion; and
a lower skin, coupled to at least the three spars, opposite the upper skin, and comprising a lower-skin major portion and a lower-skin extension portion that extends from the lower-skin major portion, wherein:
the spar major portion of each one of at least the three spars, the upper-skin major portion, and the lower-skin major portion at least partially define a flap body of the wing flap;
the spar extension portion of each one of at least the three spars, the upper-skin extension portion, and the lower-skin extension portion at least partially define a torque member of the wing flap;
the spar extension portion of each one of at least the three spars is straight and is oblique to the spar extension portion of any another one of at least the three spars;
the flap body comprises a leading edge, a trailing edge that is opposite the leading edge, an outboard end, an inboard end that is opposite the outboard end, and a flap-body width dimension between the leading edge and the trailing edge; and
the torque member extends from the inboard end of the flap body and comprises a torque-member width dimension that is less than the flap-body width dimension.

2. The wing flap of claim 1 , wherein the torque member has a noncircular cross-sectional shape.

3. The wing flap of claim 1 , wherein:
one of at least the three spars is a front spar; and
the spar major portion of the front spar is located adjacent to the leading edge of the flap body.

4. The wing flap of claim 3 , wherein:
one of at least the three spars is a rear spar; and
the spar major portion of the rear spar is located adjacent to the trailing edge of the flap body.

5. The wing flap of claim 4 , wherein:
one of at least the three spars is a middle spar; and
the spar major portion of the middle spar is located between the spar major portion of the front spar and the spar major portion of the rear spar.

6. The wing flap of claim 5 , wherein:
the torque member further comprises an extension member that is coupled to the flap body, the upper-skin extension portion, and the lower-skin extension portion; and
the extension member is located between the spar extension portion of the front spar and the spar extension portion of the middle spar or the spar extension portion of the rear spar and the spar extension portion of the middle spar.

7. The wing flap of claim 5 , wherein the torque member further comprises an extension rib that is coupled to the spar extension portion of the front spar, the spar extension portion of the middle spar, the upper-skin extension portion, and the lower-skin extension portion.

8. The wing flap of claim 5 , wherein the torque member further comprises an extension rib that is coupled to the spar extension portion of the rear spar, the spar extension portion of the middle spar, the upper-skin extension portion, and the lower-skin extension portion.

9. The wing flap of claim 1 , wherein:
the flap body further comprises an inboard rib that is coupled to the spar major portion of at least two of at least the three spars, the upper-skin major portion, and the lower-skin major portion at the inboard end of the flap body;
the torque member further comprises an extension member that is coupled to the inboard rib, the upper-skin extension portion, and the lower-skin extension portion; and
the extension member is located between the spar extension portion of two of at least the three spars.

10. The wing flap of claim 1 , wherein the torque member further comprises an extension rib that is coupled to the spar extension portion of at least two of at least the three spars, the upper-skin extension portion, and the lower-skin extension portion.

11. The wing flap of claim 1 , further comprising an inboard flap fairing, coupled to the upper-skin major portion, opposite the spar major portion of at least the three spars, wherein the inboard flap fairing is located proximate to the inboard end of the flap body.

12. The wing flap of claim 1 , further comprising a door coupled to the spar extension portion of one of at least the three spars and the lower-skin extension portion.

13. The wing flap of claim 1 , the spar major portion of each one of at least the three spars runs in a straight line and is oblique to the spar major portion of any other one of at least the three spars.

14. A method for forming a wing flap, the method comprising:
at least partially forming a flap body of the wing flap with a spar major portion of each one of at least three spars, an upper-skin major portion of an upper skin, and a lower-skin major portion of a lower skin;
at least partially forming a torque member of the wing flap with a spar extension portion of each one of at least the three spars, extending from the spar major portion of each corresponding one of at least the three spars, an upper skin extension portion of the upper skin, extending from the upper-skin major portion of the upper skin, and a lower-skin extension portion of the lower skin, extending from the lower-skin major portion of the lower skin, wherein:
the flap body comprises a leading edge, a trailing edge that is opposite the leading edge, an outboard end, an inboard end that is opposite the outboard end, and a flap-body width dimension between the leading edge and the trailing edge; and
the torque member extends from the inboard end of the flap body and comprises a torque member width dimension that is less than the flap-body width dimension.

15. A wing flap, comprising:
a first spar, comprising a first-spar major portion and a first-spar extension portion that extends from the first-spar major portion;
a second spar, comprising a second-spar major portion and a second-spar extension portion that extends from the second-spar major portion;
a third spar;
an upper skin, coupled to the first spar, the second spar, and the third spar and comprising an upper-skin major portion and an upper-skin extension portion that extends from the upper-skin major portion; and
a lower skin, coupled to the first spar, the second spar, and the third spar, opposite the upper skin, and comprising a lower-skin major portion and a lower-skin extension portion that extends from the lower-skin major portion, wherein:
the first-spar major portion, the second-spar major portion, the third spar, the upper-skin major portion, and the lower-skin major at least partially define a flap body of the wing flap;
the first-spar extension portion, the second-spar extension portion, the upper-skin extension portion, and the lower-skin extension portion at least partially define a torque member of the wing flap;
the torque member comprises an extension rib, coupled to the first-spar extension portion, the second-spar extension portion, the upper-skin extension portion, and the lower-skin extension portion;
the flap body comprises a leading edge, a trailing edge that is opposite the leading edge, an outboard end, an inboard end that is opposite the outboard end, and a flap-body width dimension between the leading edge and the trailing edge; and
the torque member extends from the inboard end of the flap body and comprises a torque-member width dimension that is less than the flap-body width dimension.

16.

Assignees

• Boeing Co

Inventors

• Kordel Jan A
• Balzer Michael A
• Bleazard Mark M
• Virnig Jacob D
• Choy Wendell C K
• Santini Gregory M

Classifications

• B64C3/187

  Ribs · CPC title

• B64C9/16 Primary

  at the rear of the wing · CPC title

• B64C3/185

  Spars · CPC title

• B64C3/20

  Integral or sandwich constructions · CPC title

• B64C3/182

  Stringers, longerons · CPC title