Panel structure and associated method

Patent metadata

Field	Value
Publication number	US-10086923-B2
Application number	US-201514883897-A
Country	US
Kind code	B2
Filing date	Oct 15, 2015
Priority date	Oct 16, 2014
Publication date	Oct 2, 2018
Grant date	Oct 2, 2018

Abstract

A panel structure for a vehicle, and especially for an aircraft or spacecraft, includes an area member, especially a skin member, that defines an areal expanse with a first surface and an opposite second surface and having a thickness between the first and second surfaces; and a plurality of elongate stiffener members which are attached to the area member and extend over at least one of the first and second surfaces; wherein at least one of the stiffener members is bifurcated at a bifurcation point into two or more branch stiffener members.

First claim

The invention claimed is:

1. A panel structure for a vehicle, comprising:
an area member that defines an areal expanse with a first surface and an opposite second surface and having a thickness between the first and second surfaces; and
a plurality of elongate stiffener members which are attached to the area member and extend over at least one of the first and second surfaces;
wherein at least one of the stiffener members is not branched or bifurcated along its entire length,

wherein at least one of the stiffener members is branched or bifurcated at a branch point into at least two branch stiffener members,
wherein the at least two branch stiffener members each have a length which extends away from the branch point and the at least two branch stiffener members remain spaced from each other along their entire lengths, except where they are joined together at a single point, being the branch point.

2. The panel structure according to claim 1 , wherein an angle of branching or bifurcation between the branch stiffener members decreases as the branch stiffener members extend away from the branch point.

3. The panel structure according to claim 1 , wherein at least one of the branch stiffener members extends through a bend or a kink to reduce or decrease the bifurcation angle as the branch stiffener members extend away from the branch point.

4. The panel structure according to claim 3 , wherein the bend or kink of the at least one branch stiffener member is through an angle back towards the other branch stiffener member.

5. The panel structure according to claim 1 , wherein each of a plurality of the stiffener members is branched or bifurcated at a respective branch point into two or more branch stiffener members.

6. The panel structure according to claim 5 , wherein the respective branch points are distributed or offset with respect to one another.

7. The panel structure according to claim 6 , wherein the respective branch points are offset from one another or distributed in a radial direction.

8. The panel structure according to claim 1 , wherein the stiffener members and branch stiffener members are arranged to provide an approximately uniform pitch or spacing between adjacent ones of the stiffener members and branch stiffener members in a localized region of the panel structure.

9. The panel structure according to claim 1 , wherein the thickness of the area member remains substantially constant.

10. A method of producing a panel structure for a vehicle, comprising:
providing an area member that defines an areal expanse comprising a first surface and an opposite second surface, the area member having a thickness defined between the first and second surfaces; and
arranging a plurality of elongate stiffener members extending over at least one of the first and second surfaces of the area member for attachment to the area member;
wherein the step of arranging the stiffener members comprises not branching or not bifurcating at least one of the stiffener members along its length and branching or bifurcating at least one of the stiffener members at a branch point into at least two branch stiffener members, wherein the at least two branch stiffener members each have a length which extends away from the branch point and the at least two branch stiffener members remain spaced from each other along their entire lengths, except where they are joined together at a single point, being the branch point.

11. The method according to claim 10 , wherein a position of the branch point in the at least one stiffener is selected based on at least one of:
a buckling threshold of a region of the area member adjacent the at least one stiffener member and a required minimum design load for the area member in that region, and
a maximum allowable longitudinal force in the at least one stiffener member.

12. The method according to claim 10 , wherein the step of arranging the stiffener members comprises decreasing an angle of bifurcation between the branch stiffener members as the branch stiffener members extend away from the branch point.

13. The method according to claim 10 , wherein the step of arranging the stiffener members comprises extending at least one of the branch stiffener members through a bend or a kink to reduce the bifurcation angle as the branch stiffener members extend away from the branch point.

14. The method according to claim 10 , wherein the step of arranging the stiffener members comprises branching or bifurcating a plurality of the stiffener members at a respective branch point into two or more branch stiffener members, the method further comprising:
distributing or offsetting the branch points with respect to one another.

15. The method according to claim 14 , wherein the step of distributing or offsetting the branch points with respect to one another comprises distributing or offsetting the branch points with respect to one another in a radial direction.

16. The method according to claim 10 , wherein the step of arranging the stiffener members comprises a preliminary digital modelling with respect to positions of the stiffener members.

17. The method according to claim 10 , wherein the method comprises an Additive Layer Manufacturing technique with which either or both of the area member and the stiffener members are deposited and built up in an integral construction.

18. The method of claim 17 , wherein the stiffener member are deposited and built up in an integral construction based upon a digital model of the panel structure.

19. The method according to claim 10 , wherein the elongate stiffener members are formed of fiber-reinforced polymer, and wherein the method comprises one of bonding and fastening the elongate stiffener members to the area member.

20. A vehicle including at least one panel structure, the panel structure comprising:
an area member, especially a skin member, that defines an areal expanse with a first surface and an opposite second surface and having a thickness between the first and second surfaces; and
a plurality of elongate stiffener members which are attached to the area member and extend over at least one of the first and second surfaces;
wherein at least one of the stiffener members is not branched or bifurcated along its entire length,
wherein at least one of the stiffener members is branched or bifurcated at a branch point into at least two branch stiffener members, wherein the at least two branch stiffener members each have a length which extends away from the branch point and the at least two branch stiffener members remain spaced from each other along their entire lengths, except where they are joined together at a single point, being the branch point.

Assignees

• Airbus Operations Gmbh

Inventors

• Seack Oliver

Classifications

• B64C1/12

  Construction or attachment of skin panels · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B64G1/22

  Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles · CPC title

• B33Y10/00

  Processes of additive manufacturing · CPC title

• B64C3/22

  Geodetic or other open-frame structures · CPC title