Stacking sequence combinations for double-double laminate structures

Patent metadata

Field	Value
Publication number	US-2022297407-A1
Application number	US-202217694054-A
Country	US
Kind code	A1
Filing date	Mar 14, 2022
Priority date	Mar 16, 2021
Publication date	Sep 22, 2022
Grant date	—

Abstract

A sub-laminate module is described for use in forming composite laminate structures. The module includes a first ply set containing a first ply layer oriented at a first angle and a second ply layer oriented at a second angle, the second angle being unequal the first angle; a second ply set containing a third ply layer oriented at a third angle and a fourth ply layer oriented at a fourth angle, the fourth angle being unequal the third angle; first and second equal acute angles are defined by differences between an absolute value of the first and second angles and the third and fourth angles, respectively, wherein the second ply layer is positioned adjacent the third ply layer and the second and third ply layers are both positioned intermediate the first and fourth ply layers, so as to define a staggered double-double helix sequence of the respective ply layers. Associated composite laminate structures and methods are also disclosed.

First claim

1 . A sub-laminate module for use in forming a composite laminate structure, the sub-laminate module comprising:
a first ply set containing a first ply layer oriented at a first angle and a second ply layer oriented at a second angle, the second angle being unequal the first angle; a second ply set containing a third ply layer oriented at a third angle and a fourth ply layer oriented at a fourth angle, the fourth angle being unequal the third angle; a first acute angle defined by a first difference between an absolute value of the first angle and the second angle; and a second acute angle defined by a second difference between an absolute value of the third angle and the fourth angle, the second acute angle being the same as the first acute angle, wherein the second ply layer is positioned adjacent the third ply layer and the second and third ply layers are both positioned intermediate the first and fourth ply layers, so as to define a staggered double-double helix sequence of the respective ply layers.

2 . The sub-laminate module of claim 1 , wherein the staggered double-double helix sequence is [Φ/−Ψ/−Φ/Ψ], such that the first ply layer is oriented at Φ, the second ply layer is oriented at −Ψ, the third ply layer is oriented at −Φ, and the fourth ply layer is oriented at T.

3 . The sub-laminate module of claim 2 , wherein:
Φ lies in a range from 0 to 60 degrees; and Ψ lies in a range from 30 to 90 degrees.

4 . The sub-laminate module of claim 3 , wherein the first and second acute angles are less than or equal to 40 degrees.

5 . The sub-laminate module of claim 1 , wherein the staggered double-double helix sequence is [Φ/Ψ/−Φ/−Ψ], such that the first ply layer is oriented at Φ, the second ply layer is oriented at Ψ, the third ply layer is oriented at −Φ, and the fourth ply layer is oriented at −Ψ.

6 . The sub-laminate module of claim 5 , wherein:
Φ lies in a range from 20 to 70 degrees; and Ψ lies in a range from 20 to 70 degrees.

7 . The sub-laminate module of claim 5 , wherein the first and second acute angles are less than or equal to 40 degrees.

8 . The sub-laminate module of claim 1 , wherein the staggered double-double helix sequence is [Φ/−Ψ/Ψ/−Φ], such that the first ply layer is oriented at Φ, the second ply layer is oriented at −Ψ, the third ply layer is oriented at Ψ, and the fourth ply layer is oriented at −Φ.

9 . The sub-laminate module of claim 8 , wherein:
Φ lies in a range from 10 to 40 degrees when Ψ lies in a range from 0 to 10 degrees; Φ lies in a range from 50 to 70 degrees when Ψ lies in a range from 20 to 40 degrees; and Φ lies in a range from 80 to 90 degrees when Ψ lies in a range from 50 to 80 degrees.

10 . The sub-laminate module of claim 8 , wherein the first and second acute angles are less than or equal to 40 degrees.

11 . The sub-laminate module of claim 1 , wherein the staggered double-double helix sequence is [Φ/Ψ/−Ψ/−Φ], such that the first ply layer is oriented at Φ, the second ply layer is oriented at Ψ, the third ply layer is oriented at −Ψ, and the fourth ply layer is oriented at −Φ.

12 . The sub-laminate module of claim 11 , wherein:
Φ lies in a range from 10 to 40 degrees when Ψ lies in a range from 0 to 10 degrees; Φ lies in a range from 30 to 70 degrees when Ψ lies in a range from 20 to 40 degrees; and Φ lies in a range from 80 to 90 degrees when Ψ lies in a range from 50 to 80 degrees.

13 . The sub-laminate module of claim 11 , wherein the first and second acute angles are greater than less than or equal to 40 degrees.

14 . A composite laminate structure comprising:
at least two sub-laminate modules according to claim 1 , wherein:
the fourth ply of a first of the at least two sub-laminate modules is positioned, during stacking thereof, adjacent the first ply of a second of the at least two-sub-laminate modules; and
orientation values of [Φ/Ψ] are independent in each of the at least two sub-laminate modules.

15 . The composite laminate structure of claim 14 , wherein:
the staggered double-double helix sequence of the first sub-laminate module is a first sequence of [Φ/−Ψ/−Φ/Ψ], the staggered double-double helix sequence of the second sub-laminate module is a second sequence of [Φ/−Ψ/Ψ/−Φ], and a 45-degree difference separates the first and second sequences.

16 . A composite laminate structure comprising a plurality of sub-laminate modules each comprising:
a first ply set containing a first ply layer oriented at a first angle and a second ply layer oriented at a second angle, the second angle being unequal the first angle; a second ply set containing a third ply layer oriented at a third angle and a fourth ply layer oriented at a fourth angle, the fourth angle being unequal the third angle; a first acute angle defined by a first difference between an absolute value of the first angle and the second angle; and a second acute angle defined by a second difference between an absolute value of the third angle and the fourth angle, the second acute angle being the same as the first acute angle, wherein the second ply layer is positioned adjacent the third ply layer and the second and third ply layers are both positioned intermediate the first and fourth ply layers, so as to define a staggered double-double helix sequence of the respective ply layers.

17 . The composite laminate structure of claim 16 , wherein:
the plurality of sub-laminate modules comprises at least three distinct modules; the staggered double-double helix sequence of two or more of the sub-laminate modules are different relative to one another; and the staggered double-double helix sequence is selected from the group consisting of:
a first staggered sequence of [Φ/−Ψ/−Φ/Ψ];
a second staggered sequence of [Φ/Ψ/−Φ/−Ψ];
a third staggered sequence of [Φ/−Ψ/Ψ/−Φ]; and
a fourth staggered sequence of [Φ/Ψ/−Ψ/−Φ].

18 . The composite laminate structure claim of 17 , wherein:
the plurality of sub-laminate modules comprises at least four distinct modules stacked such that two modules are exterior facing and two modules are interior facing relative to a set of opposing outside surfaces of the composite laminate structure; the staggered double-double helix sequence of the two interior facing modules are different relative to the staggered double-double helix sequence of the two exterior facing modules; and the staggered double-double helix sequences are selected from the group consisting of:
a first staggered sequence of [Φ/−Ψ/−Φ/Ψ];
a second staggered sequence of [Φ/Ψ/−Φ/−Ψ];
a third staggered sequence of [Φ/−Ψ/Ψ/−Φ]; and
a fourth staggered sequence of [Φ/Ψ/−Ψ/−Ψ].

19 . The composite laminate structure of claim 18 , wherein:
the staggered double-double helix sequences of the first and fourth sub-laminate modules define a first sequence of [Φ/−Ψ/−Φ/Ψ], the staggered double-double helix sequences of the second and third sub-laminate modules define a second sequence of [Φ/−Ψ/Ψ/−Φ], the second and third sub-laminate modules being interior and adjacent modules intermediate the exterior first and fourth sub-laminate modules, and a 45-degree difference separates the first and second sequences.

20 . A method of manufacturing a sub-laminate module for use in forming a composite laminate structure, the method comprising the steps of:
positioning a first ply set in a first orientation, the first ply set containing a first ply layer oriented at a first angle and a second ply layer oriented at a second angle, the second angle being unequal th

Assignees

• Univ Leland Stanford Junior

Inventors

• Tsai Stephen W
• Miravete Antonio

Classifications

• B32B2603/00

  Vanes, blades, propellers, rotors with blades · CPC title

• B32B2605/18

  Aircraft · CPC title

• B32B2307/748

  Releasability · CPC title

• B32B2262/106

  Carbon fibres, e.g. graphite fibres · CPC title

• B32B5/12

  characterised by the relative arrangement of fibres or filaments of {different layers, e.g. the fibres or filaments being parallel or perpendicular to each other} · CPC title