Impact Resistant Sandwich Structure

Abstract

A sandwich structure architecture for high speed impact resistant structure includes sandwich skins which enclose a sandwich core formed by a plurality of spacing layers and a plurality of trigger layers, wherein these layers are stacked alternatively in the core. The walls of the trigger layers are thicker than the walls of the spacing layers and/or the walls of the trigger layers include at least one part inclined with respect to the walls of the spacing layers. The spacing and the trigger layers are made of the same type of material, preferably composite materials or metallic materials. The structure is capable of absorbing high-speed impacts, and at the same time can be used as load carrying structure in aircraft fuselages, wings, vertical or horizontal stabilizers.

Claims

1. An impact resistant structure comprising: a sandwich core having upper and lower skins, the core comprising a plurality of spacing layers and a plurality of trigger layers, stacked together and alternatively arranged in the core, wherein the spacing and triggering layers are configured as multi-cell hollow structures having walls, disposed perpendicular to a plane (Y) substantially parallel to the upper and lower skins, wherein the spacing layers and the trigger layers are made of the same type of material, and wherein trigger layers mass per unit of volume, is larger than the one for the spacing layers.

2. The structure according to claim 1, wherein the walls of the trigger layers are thicker than the walls of the spacing layers.

3. The structure according to claim 2, wherein the walls of the trigger layers includes at least one part inclined with respect to the walls of the spacing layers.

4. The structure according to claim 1, wherein the walls of the trigger and spacing layers have substantially the same thickness, and wherein the walls of the trigger layers includes at least one part inclined with respect to the walls of the spacing layers.

5. The structure according to claim 1, wherein the walls of the trigger layers have an inclined part, such as that inclined part forms an angle (α) with the walls of adjacent spacing layers, and wherein that angle (α) is within the range 90° to 150°.

6. The structure according to claim 1, wherein the walls of the trigger layers include a rhomboidal shape in a cross-sectional view.

7. The structure according to claim 1, wherein the walls of the trigger layers include a T-shaped configuration in a cross-sectional view.

8. The structure according to claim 1, wherein the walls of the trigger layers are straight, thicker than the walls of the spacing layers and perpendicular to a plane defined by the spacing and trigger layers.

9. The structure according to claim 1, wherein the spacing layers and trigger layers have respectively constant height, and wherein the spacing layers are higher than the trigger layers.

10. The structure according to claim 1, wherein the cells of the spacing and trigger layers have substantially the same shape in a top plan view of the layers.

11. The structure according to claim 1, wherein the upper and lower skins, spacing and trigger layers are made of a composite material.

12. The structure according to claim 1, wherein upper and lower skins, the spacing and trigger layers are metallic.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Preferred embodiments of the invention are henceforth described with reference to the accompanying drawings, wherein:

[0016] FIG. 1 shows a front view of a preferred embodiment of an impact resistant structure according to the invention.

[0017] FIG. 2 shows a top plan view of the structure of FIG. 1 with the upper skin partially removed to show the core configuration.

[0018] FIG. 3 shows an enlarged view of the portion (A) of FIG. 1.

[0019] FIG. 4 shows an enlarged view of the portion (B) of FIG. 2, which corresponds to a view taken along cutting line IV-IV in FIG. 3.

[0020] FIG. 5 shows a view taken along cutting line V-V in FIG. 4.

[0021] FIGS. 6A-6E show in cross-sectional views, alternative designs of the trigger layers, wherein only one vertical wall of the core is partially represented for the sake of clarity of the illustration.

DETAILED DESCRIPTION

[0022] FIG. 1 shows a preferred embodiment of an impact resistant structure (1), comprising a sandwich core (2) having external upper and lower skins (3,4) attached to the core (2) preferably by bonding. The sandwich core (2) comprises a plurality of spacing layers (5) and a plurality of trigger layers (6), wherein these layers (5,6) are stacked alternatively in the core as it can be seen in FIG. 1.

[0023] As shown in FIGS. 2 and 3, spacing and trigger layers (5,6) are multi-cell structures, having walls (5a,6a) (see FIG. 3) perpendicular to a plane (Y) preferably parallel to layers (5,6). In this preferred embodiment the multi-cell core has a honey-comb configuration, wherein each cell (7) (see FIG. 2) is defined by a surrounding wall in this case with hexagonal shape. Additionally, the spacing and trigger layers (5,6) (see FIG. 1) have substantially the same geometric configuration, except trigger layers walls which are thicker and shorter than the walls of the spacing layers. Spacing and trigger layers (5,6) (see FIG. 1) are stacked alternatively until sandwich height is achieved.

[0024] In other preferred embodiments, the cells (7) (see FIG. 2) of the layers (5,6) (see FIG. 1) can have different cross sections, such as rectangular, circular, elliptical etc.

[0025] Preferably, trigger layer walls (6a) are thicker than spacing layers walls (5a). This feature can be obtained in many different ways, for example in the exemplary embodiment represented in FIGS. 1 to 5 and 6E, trigger layer walls (6a) have a rhomboidal cross-section (6b).

[0026] Alternatively as shown in FIG. 6B, instead of this rhomboidal cross-section, trigger layer walls (6a) are thicker than spacing layer walls (5a) and have no dedicated part or segment in a different plane than the one defined by spacing layer walls. In the embodiment of FIG. 6C, these walls (6a) have a T-shape cross-section.

[0027] Another relevant feature of the invention, common for all the above-described embodiments, is that spacing and trigger layers heights (h5,h6) are constant for most of the structure, and wherein the spacing layers (6) are higher than the trigger layers (5), that is h5>h6. Preferably, (h5) is 20%-40% higher than (h6).

[0028] In the exemplary embodiment of FIG. 6A, spacing and trigger layer (5a,6a) walls have the same thickness. On top of this, the trigger layer walls (6a) have a V-shape cross-section. These walls (6a) have two inclined parts with respect to spacing layer walls (5a). An angle (α) is defined between a trigger layer wall (6a) and its adjacent spacing layer wall (5a). Preferably, this angle (α) is within the range 90° to 150°.

[0029] In the practical embodiment of FIG. 6A, the walls (6a) could also be thicker than the walls (5a), (FIG. 6D).

[0030] Impact resistant sandwich core depicted in FIGS. 1 to 6, can be manufactured for example in aluminum, composites, Nomex®, etc. In the case of composite materials, the entire assembly is obtained by co-curing and/or adhesive bonding the layers together. Other technologies, as becoming available and mature, could enable one-shot manufacturing favouring lead time and cost reduction (for example 3D printing).

[0031] The architecture of the sandwich core of the invention enhances the energy absorption capability due to the trigger layers configuration, acting as impactor (blade, bullet, bird, etc.) local damage initiator (hard points or reinforcements optimized layout) and favouring core progressive failure. The conjunction of these two mechanisms generates superior impact resistant sandwich cores, and maximizes the energy absorption of the sandwich core.

[0032] The use of the invention is especially advantageous for aircraft rotor blade release protection, for example in the case of open rotors or turbo-propellers powered aircrafts.

[0033] In a specific test case, an impact of a 16 kg rotor blade at speed of 171.5 m/s was absorbed by a sandwich structure of 490 mm total height and 1860 mm×2340 mm area.

[0034] Other preferred embodiments of the present invention are described in the appended dependent claims and the multiple combinations threreof.

[0035] While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms “comprise” or “comprising” do not exclude other elements or steps, the terms “a” or “one” do not exclude a plural number, and the term “or” means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.