# US 12,005,682 B2 · Composite laminate cards of finite size, tapered composite laminate structures formed from the same, and methods of manufacturing and using the same > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,005,682 B2 - Document ID: US12005682B2 - Status: Granted - Kind: B2 - Application number: 17/798,513 - Filed: 2021-03-18 - Published: 2023-03-09 - Granted: 2024-06-11 - Earliest claimed: 2020-03-18 - Assignees: The Board of Trustees of the Leland Stanford Junior University - Applicants: The Board of Trustees of the Leland Stanford Junior University - Inventors: Stephen W. Tsai - Web page: https://patentgrep.com/patent/US12005682B2 ## CPC - B29C 70/302: {Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination} - B32B 27/08: of synthetic resin - B29D 99/0003: {Producing profiled members, e.g. beams} - B32B 3/10: characterised by a discontinuous layer, i.e. formed of separate pieces of material - B32B 5/02: characterised by structural features of a {fibrous or filamentary} layer {(layer formed of metallic wires B32B15/02; layer formed of natural mineral fibres B32B19/02; layer formed of wood fibres B32B21/02)} - B32B 5/12: 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} - B32B 5/26: another layer {next to it} also being fibrous or filamentary {(relative arrangement of fibres or filaments of different layers B32B5/12)} - B29L 2031/3076: {Aircrafts (blades, propellers B29L2031/08)} - B32B 2250/20: All layers being fibrous or filamentary - B32B 2250/24: All layers being polymeric - B32B 2250/44: Number of layers variable across the laminate - B32B 2260/023: Two or more layers - B32B 2260/046: Synthetic resin - B32B 2262/101: Glass fibres - B32B 2262/106: Carbon fibres, e.g. graphite fibres - B32B 2262/14: Mixture of at least two fibres made of different materials - B32B 2307/732: Dimensional properties - B32B 2590/00: Signboards, advertising panels, road signs - B32B 2603/00: Vanes, blades, propellers, rotors with blades - B32B 2605/00: Vehicles - B32B 2605/18: Aircraft - Y02T 50/40: Weight reduction - B29C: SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING (making preforms B29B11/00; making laminated products by combining previously unconnected layers which become one product whose layers will remain together B32B37/00 - B32B41/00) - B32B: LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM - B29D: PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE (making granules B29B9/00; making preforms B29B11/00) - B29L: INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract Described are various dual-tapered composite laminate structures. These structures may comprise a plurality of finite sub-laminate cards, each one of the plurality of cards having the same shape and size as the other ones of the plurality of cards and having opposing surfaces oriented in a card plane, opposing primary edges of the planar surfaces, and opposing secondary edges of the planar surfaces, the opposing secondary edges being perpendicular to the opposing primary edges. The finite sub-laminate cards are stacked relative to one another in a successively offset manner. Also described are methods of stacking and sliding (for offset) the finite sub-laminate cards. Tapered fuselage skin and fuel tank covers are also considered. ## Claims ### Claim 1 A dual-tapered composite laminate structure, the structure having a longitudinal axis and comprising: a plurality of finite sub-laminate cards, each card of the plurality of cards having the same shape and size as the other ones of the plurality of cards and having opposing planar surfaces oriented in a single card plane, opposing primary edges of the opposing planar surfaces, and opposing secondary edges of the opposing planar surfaces, the opposing secondary edges being perpendicular to the opposing primary edges; a top surface defined by an uppermost one of the plurality of finite sub-laminate cards; and a tool surface defined by a lowermost one of the plurality of finite sub-laminate cards, the tool surface being oppositely oriented relative to the top surface; wherein: each of the plurality of cards is stacked atop adjacently positioned cards of the plurality of cards in a direction orthogonal to the opposing planar surfaces and the opposing primary and secondary edges of the plurality of cards; each of the plurality of cards is offset an offset distance in the card plane relative to an adjacently positioned card of the plurality of cards; the offset distance is defined as a distance between respective ones of the opposing primary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards; one of the opposing primary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards defines a top tapered portion of the top surface of the composite laminate structure; the other of the opposing primary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards defines a tool tapered portion of the tool surface of the composite laminate structure, the tool tapered portion being oppositely oriented relative to the top tapered portion, each card of the plurality of cards contains four distinct ply layers; and two of the four distinct ply layers within each card of the plurality of cards are offset at an angle relative to another two of the four distinct ply layers, the angle being between 22 and 70 degrees. ### Claim 2 (depends on 1) The structure of claim 1, wherein each card of the plurality of cards is substantially rectangular-shaped. ### Claim 3 (depends on 1) The structure of claim 1, wherein at least one of: at least a portion of each card of the plurality of cards is quasi-trapezoidal-shaped; or a taper of each of the trapezoidal-shaped cards is linear. ### Claim 4 (depends on 1) The structure of claim 1, wherein the offset distance is one of: between ⅛ and 1.0 inches; between ¼ and ¾ inches; between ¼ and ½ inches; between 0.01 and 4.0 inches; or between 1/16 and ⅛ inches. ### Claim 5 (depends on 1) The structure of claim 1, wherein the offset distance is the same for at least two adjacently positioned cards of the plurality of cards. ### Claim 6 (depends on 1) The structure of claim 1, wherein the offset distance varies linearly. ### Claim 7 (depends on 1) The structure of claim 1, wherein the offset distance variably increases from a lowermost to an uppermost of the adjacently positioned cards of the plurality of cards. ### Claim 8 (depends on 1) The structure of claim 1, further including a continuous card having at least one of a shape or size different than the shape or size of the cards of the plurality of cards. ### Claim 9 (depends on 1) The structure of claim 1, wherein a length of the top tapered portion in the direction of the longitudinal axis of the structure is ¼ to ½ a length of the structure in the longitudinal direction. ### Claim 10 (depends on 1) The structure of claim 1, wherein a length of the tool tapered portion in the direction of the longitudinal axis of the structure is ¼ to ½ a length of the structure in the longitudinal direction. ### Claim 11 (depends on 1) The structure of claim 1, wherein a length of both the top and the tool tapered portions in the direction of the longitudinal axis of the structure is ⅓ a length of the structure in the longitudinal direction. ### Claim 12 (depends on 1) The structure of claim 1, wherein an un-tapered portion is provided, along the longitudinal axis, intermediate the top and the tool tapered portions. ### Claim 13 (depends on 12) The structure of claim 12, wherein the un-tapered portion has a length in the direction of the longitudinal axis of the structure that is ¼ to ⅓ a length of the structure in the longitudinal direction. ### Claim 14 (depends on 1) The structure of claim 1, wherein a weight savings of at least 50% are achieved relative to an un-tapered structure of constant thickness throughout. ### Claim 15 (depends on 1) The structure of claim 1, wherein the offset distance is a first offset distance and a second offset distance is also provided, the second offset distance being defined as a distance between respective ones of the opposing secondary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards, so as to provide a two-dimensional tapering of the opposing top and tool surfaces of the structure. ### Claim 16 (depends on 15) The structure of claim 15, wherein one of the first and second offset distances is variable. ### Claim 17 (depends on 1) The structure of claim 1, wherein the structure is one of: a tapered stiffener or stringer; a tapered fuselage skin a fuel tank cover having one interior continuous layer adjacent the plurality of cards; or a tapered aircraft wing. ### Claim 18 A method of forming a dual-tapered composite laminate structure having a longitudinal axis, the method comprising the steps of: providing a plurality of finite sub-laminate cards, each card of the plurality of cards having the same shape and size as the other ones of the plurality of cards and having opposing planar surfaces oriented in a single card plane, opposing primary edges of the opposing planar surfaces, and opposing secondary edges of the opposing planar surfaces, the opposing secondary edges being perpendicular to the opposing primary edges; establishing a tool surface by positioning of a first card of the plurality of cards in a direction aligned with the longitudinal axis of the structure to be formed; stacking at least a second card of the plurality of cards atop the first card of the plurality of cards, the stacking occurring in an offset manner, so that at least opposing primary edges of the second card do contact the first card; stacking a last card of the plurality of cards atop the at least second card of the plurality of cards in the offset manner so as to define a top surface of the structure, wherein: each of the plurality of cards is stacked atop adjacently positioned cards of the plurality of cards in a direction orthogonal to the opposing planar surfaces and the opposing primary and secondary edges of the plurality of cards; the offset distance is defined as a distance between respective cards of the opposing primary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards; one of the opposing primary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards defines a top tapered portion of the top surface the composite laminate structure; the other of the opposing primary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards defines a tool tapered portion of the tool surface of the composite laminate structure, the tool tapered portion being oppositely oriented relative to the top tapered portion, each card of the plurality of cards contains four distinct ply layers; and two of the four distinct ply layers within each card of the plurality of cards are offset at an angle relative to another two of the four distinct ply layers, the angle being between 22 and 70 degrees. ### Claim 19 (depends on 18) The method of claim 18, wherein one of: the last card of the plurality of cards is a sixteenth of the plurality of cards and fourteen cards are sequentially stacked with successive offset distances between the first and the last cards of the plurality of cards; or the last card of the plurality of cards is an eighth of the plurality of cards and six cards are sequentially stacked with successive offset distances between the first and the last cards of the plurality of cards. ### Claim 20 (depends on 18) The method of claim 18, wherein the offset distance is a first offset distance and a second offset distance is also provided, the second offset distance being defined as a distance between respective ones of the opposing secondary edges of the opposing planar surfaces of adjacently positioned cards of the plurality of cards, so as to provide a two-dimensional tapering of the opposing top and tool surfaces of the structure. ### Claim 21 (depends on 20) The method of claim 20, wherein one of the first and second offset distances is variable. ### Claim 22 (depends on 18) The method of claim 18, wherein either: the offset distance achieved via the offset stacking of the plurality of cards is the same for all adjacently positioned cards of the plurality of cards; or the offset distance achieved via the offset stacking is different for at least two adjacently positioned cards of the plurality of cards. ### Claim 23 (depends on 18) The method of claim 18, further including stacking a continuous card having at least one of a shape or size different than the shape or size of the cards of the plurality of cards adjacent an exterior card of the plurality of cards.