MODULAR ACOUSTIC PROTECTION ARRANGEMENT AND METHOD FOR MANUFACTURING SUCH AN ACOUSTIC PROTECTION ARRANGEMENT
20210074256 ยท 2021-03-11
Assignee
Inventors
Cpc classification
B64G1/22
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
An acoustic protection arrangement comprises acoustic protection modules, in particular acoustic absorber modules, wherein at least one of the acoustic protection modules is tuned to a different frequency, in particular has a different peak absorption frequency or acoustic frequency response, than at least another one of the acoustic protection modules. Furthermore, a kit of parts for assembling such an acoustic protection arrangement is provided, and a method for manufacturing such an acoustic protection arrangement is proposed. The acoustic protection arrangement can be implemented based on the kit of parts by selecting appropriate acoustic protection modules and combining them to form an acoustic protection arrangement that fulfils the specific acoustic and geometric requirements for an application, such as a launch vehicle type and/or launch mission. The acoustic protection arrangement can thus be adapted, in particular by tuning the proposed acoustic protection arrangement to achieve a desired overall level of acoustic attenuation.
Claims
1. An acoustic protection arrangement (1) comprising a plurality of acoustic protection modules (2, 2, . . . ), in particular acoustic absorber modules, wherein at least one of the acoustic protection modules (2) is tuned to a different frequency, in particular has a different peak absorption frequency (f.sub.p) or acoustic frequency response, than at least another one of the acoustic protection modules (2).
2. The acoustic protection arrangement (1) of claim 1, wherein the plurality of acoustic protection modules (2, 2, . . . ) comprises at least a first set (A) of one or more acoustic protection modules (2, 2, . . . ) with a first structure and a second set (B) of one or more acoustic protection modules (2, 2, . . . ) with a second structure, the first and second structures being different from one another, in particular wherein the first structure constitutes a first type of Helmholtz resonator and the second structure constitutes a second type of Helmholtz resonator, for instance wherein the first type of Helmholtz resonator comprises an enclosure (3) with a horn- or funnel-shaped inlet (4, 4) extending into the enclosure (3) and the second type of Helmholtz resonator comprises an enclosure (3) with an opening (5) and a plurality of partitions formed by interior walls (6) displaced relative to one another providing a meander-like pathway within the enclosure (3).
3. The acoustic protection arrangement (1) of claim 1, wherein at least one of the following applies: the acoustic protection modules (2, 2, . . . ) all have the same shape, and in particular all have the same size; the acoustic protection modules (2, 2, . . . ) belonging to the first set (A) all have the same shape, and in particular all have the same size; the acoustic protection modules (2, 2, . . . ) belonging to the second set (B) all have the same shape, and in particular all have the same size, more particularly are all larger or smaller than the acoustic protection modules (2, 2, . . . ) belonging to the first set (A); the peak absorption frequency (f.sub.p) of the acoustic protection modules (2, 2, . . . ) belonging to the second set (B) is lower or higher than the peak absorption frequency (f.sub.p) of the acoustic protection modules (2, 2, . . . ) belonging to the first set (A).
4. The acoustic protection arrangement (1) of claim 1, wherein the acoustic protection modules (2, 2, . . . ), in particular the enclosures (3), are box-, cylinder- or cone-shaped or are at least partly box-, cylinder- or cone-shaped, for instance are a combination of cylinder- and cone-shaped, or have a doubly curved surface.
5. The acoustic protection arrangement (1) of claim 1, wherein a wall (6) of at least one of the acoustic protection modules (2, 2, . . . ) or an interior wall (6) within at least one of the acoustic protection modules (2, 2, . . . ), in particular one of the enclosures (3, 3), is moveable within the acoustic protection module (2, 2, . . . ) or enclosure (3, 3), in particular removable from the acoustic protection module (2, 2, . . . ) or enclosure (3, 3), more particularly replaceable by another wall (6) having a different stiffness, more particularly with a different thickness and/or made of a different material.
6. The acoustic protection arrangement (1) of claim 5, wherein the wall (6) features a hole, in particular forming an inlet (4) or an opening (5) to an exterior of the acoustic protection module (2, 2, . . . ) or enclosure (3), in particular wherein the wall (6) is replaceable by another wall (6) having a different inlet (4) or opening (5), in particular wherein the inlet (4) or opening (5) has a different shape and/or size.
7. The acoustic protection arrangement (1) of claim 1, wherein at least a part of the plurality of acoustic protection modules (2, 2, . . . ) is jointly covered by a microperforated sheath (9), in particular wherein the sheath (9) has a thickness of less than 10 mm, more particularly less than 5 mm, even more particularly less than 1 mm, and in particular wherein the sheath (9) features perforations having a diameter or an extent of less than 2 mm, more particularly of less than 1 mm, even more particularly of less than 0.5 mm, and in particular wherein the perforations are spaced apart by less than 50 mm, more particularly by less than 10 mm, even more particularly by less than 5 mm, in particular wherein the sheath is made of a polyester, in particular biaxially-oriented polyethylene terephthalate, such as Mylar.
8. A launch vehicle structure with an acoustic protection arrangement (1) according to claim 1 disposed on an inside wall of the structure, in particular on a cylindrical, conical or doubly curved portion of the inside wall, the structure in particular being at least one of the following: a payload fairing, an inter-stage adapter, a multi-launch canister, a heat shield, a payload attachment fitting.
9. A kit of parts for assembling an acoustic protection arrangement (1) according to claim 1, comprising the following parts: at least a first set (A) of acoustic protection modules (2, 2, . . . ) with a first structure, wherein the first set (A) of acoustic protection modules (2, 2, . . . ) comprise acoustic protection modules (2, 2, . . . ) having different acoustic properties, in particular having different peak absorption frequencies (f.sub.p, f.sub.p, . . . ) or acoustic frequency responses; and further optionally comprising one or more of the following parts: a second set (B) acoustic protection modules (2, 2, . . . ) with a second structure which is different than the first structure, in particular wherein the first and second sets (A, B) of acoustic protection modules (2, 2, . . . ) comprise acoustic protection modules (2, 2, . . . ) having different acoustic properties, in particular having different peak absorption frequencies (f.sub.p, f.sub.p, . . . ) or acoustic frequency responses; a set of different wall (6) or interior wall (6) elements adapted to be comprised in the acoustic protection modules (2, 2, . . . ), in particular having different stiffnesses, more particularly with different thicknesses and/or made of different materials, and in particular featuring a hole (4, 4, 5) of different shapes and sizes; a set of different base plates (8), in particular having different shapes and sizes, and in particular having different stiffnesses, more particularly with different thicknesses and/or made of different materials; a set of different microperforated sheaths (9), in particular with different thicknesses, and in particular featuring perforations of different diameters/extents, and in particular wherein the perforations are spaced apart at different distances.
10. A method for manufacturing an acoustic protection arrangement (1) according to claim 1, comprising the steps of: providing acoustic and geometric requirements of a desired acoustic protection arrangement (1); based on the acoustic and geometric requirements selecting parts from a kit of parts according to claim 9 and arranging the selected parts to form a design of the acoustic protection arrangement (1); generating a three-dimensional geometrical model of the design of the acoustic protection arrangement (1); determining acoustic properties of the design of the acoustic protection arrangement (1) based on the three-dimensional geometrical model, in particular by means of computer simulation; comparing the determined acoustic properties with the acoustic requirements (1); modifying the design of the acoustic protection arrangement (1) in case the acoustic properties do not meet the acoustic requirements, in particular by one or more of: replacing/exchanging a part, adding/removing a part, modifying a part by moving a part within the part, and modifying a part by redesigning the part, and in particular adding the redesigned part to the kit of parts; repeating the steps of generating a three-dimensional geometrical model, determining acoustic properties, comparing the determined acoustic properties and modifying the design until the acoustic properties of the design of the acoustic protection arrangement (1) meet the acoustic requirements of the desired acoustic protection arrangement (1); manufacturing the parts, in particular by means of computer-controlled additive manufacturing, in particular 3D-printing, moulding, in particular vacuum moulding, and deep-drawing; and assembling the parts to form a manufactured acoustic protection arrangement (1).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0068] The present invention is further explained below by means of non-limiting specific embodiments and with reference to the accompanying drawings, which show the following:
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[0074] In the figures same reference symbols refer to same or corresponding elements.
DETAILED DESCRIPTION OF THE INVENTION
[0075]
[0076] The individual acoustic absorber modules 2, 2, . . . are chosen from a set of pre-designed, -tested and perhaps even prefabricated modules having different frequency responses such that the resulting acoustic protection arrangement 1 fulfils the specific requirements of a customer for his dedicated application, taking into account a certain launch vehicle, mission type and payload.
[0077] As illustrated in
[0078] As depicted in
[0079] The wall 6 may feature a hole forming an inlet 4 or an opening 5 to an exterior of the acoustic protection module 2, 2, . . . or enclosure 3, 3 which influences the acoustic properties of the module 2, 2, . . . . The wall 6 can therefore for instance be replaceable by another wall 6 having a different inlet 4 or opening 5, e.g. having a different shape and/or size in order to alter the acoustic properties and fine-tune the acoustic characteristics to the specific needs of the customer. Instead of replacing the wall 6 with another wall 6 having a different inlet 4 or opening 5, alternatively the size of the inlet 4 or opening 5 can be made adjustable for instance by means of a moveable shutter or an iris mechanism (such as known from optical lenses), which can be opened and closed to adjust the size of the aperture. Such a mechanism could be either manually adjusted during (pre-launch) assembly of the acoustic protection arrangement 1 or even be automatically controllable in use (in-flight) in order to optimise the acoustic performance in real-time.
[0080] As indicated in
[0081] Alternatively, the individual acoustic protection modules 2, 2, . . . may be joined together (either fixedly or releasably) to form a panel, e.g. whereby the acoustic protection modules 2, 2, . . . form compartments of the panel. The panel is shaped to be mounted, for instance in a form-fitting manner, on the inside surface of a launch vehicle structure.
[0082] The acoustic characteristics of the acoustic protection arrangement 1 may be adjusted by acoustically coupling multiple adjacent modules with each other, for instance by means of an aperture 10 in a common side or rear wall or in contacting sides or rear walls of two adjacent modules 2, 2, . . . .
[0083] Furthermore, as illustrated in
[0084] The acoustic characteristics of the acoustic protection arrangement 1 can be further adjusted by (at least partially) filling the acoustic protection modules 2, 2, . . . (or selected ones thereof) with a filler material 11 or structure. The filler material 11 may be one or a combination of a porous or gaseous material, such as a(n open-cell) foam, for instance a polystyrene foam, expanded polystyrene or one or more gas, e.g. air, filled plastic sheaths or sheeting or a honeycomb structure. The acoustic protection modules 2, 2, . . . may additionally comprise means adapted to regulate a gas pressure of the filler material 11 such that the acoustic properties may for instance be adjusted in real-time during use of the acoustic protection arrangement 1 (in-flight).
[0085] With all these embodiments of the proposed acoustic protection arrangement 1 it is possible to come up with a design that exactly meets the acoustic and geometric requirements of a customer and thus provide optimal acoustic protection of a specific payload in a certain launch vehicle and mission type.
[0086] To achieve this the proposed method of (designing and) manufacturing an acoustic protection arrangement using computer-aided design, simulation and manufacturing techniques and computer system is proposed as follows. In a first step the acoustic and geometric requirements of the desired acoustic protection arrangement 1 are entered into the computer system. Based on these requirements appropriate parts are (semi-)automatically selected by the computer system (with the aid of a human operator) from the proposed kit of (standard) pre-characterised, pre-tested/certified and potentially even prefabricated parts and (semi-)automatically arranged by the computer system (with the aid of a human operator) to form a design of the acoustic protection arrangement 1 fulfilling the geometric requirements. With this a three-dimensional geometrical model of the design of the acoustic protection arrangement 1 is automatically generated by the computer system. Based on this three-dimensional geometrical model acoustic properties of the design of the acoustic protection arrangement 1 are determining by means of computer simulation. Then the determined acoustic properties are compared with the acoustic requirements. In case the acoustic properties do not meet the acoustic requirements the design of the acoustic protection arrangement is modified, for instance by performing one or more of: [0087] replacing/exchanging a part, [0088] adding/removing a part, [0089] modifying a part by moving a part within the part, and [0090] modifying a part by redesigning the part, and in particular adding the redesigned part to the kit of parts.
[0091] The steps of generating a three-dimensional geometrical model, determining acoustic properties, comparing the determined acoustic properties and modifying the design are (or may be) repeated until the acoustic properties of the design of the acoustic protection arrangement 1 meet the acoustic requirements of the desired acoustic protection arrangement 1. Subsequently, the parts are manufactured, for instance by means of computer-controlled additive manufacturing, such as 3D-printing, (vacuum) moulding and deep-drawing, and assembled to form a manufactured acoustic protection arrangement.
[0092] Additionally, the actual acoustic properties of the manufactured acoustic protection arrangement 1 are measured. In case the measured acoustic properties do not meet the acoustic requirements the manufactured acoustic protection arrangement 1 is modified, for instance by performing one or more of: [0093] replacing/exchanging a part, [0094] adding/removing a part, [0095] modifying a part by moving a part within the part, and [0096] modifying a part by redesigning the part, and in particular adding the redesigned part to the kit of parts.
[0097] The steps of measuring acoustic properties, comparing the measured acoustic properties and modifying the manufactured acoustic protection arrangement 1 are (or may be) repeated until the measured acoustic properties meet the acoustic requirements of the desired acoustic protection arrangement 1.
[0098] Finally, the manufactured acoustic protection arrangement 1 or sections thereof are mounted on an inside wall of a launch vehicle structure.
[0099] In this way it is ensured that the manufactured acoustic protection arrangement 1 meets the expectations of the customer and provides the desired acoustic protection to the payload in an effective manner. This is achieved quickly and efficiently based on the proposed kit of (pre-certified and thus reliable) parts taken a standard library of pre-designed, pre-characterised and potentially even prefabricated parts using the method of designing and manufacturing described above in a cost-effective manner. The (re-)use of pre-certified parts is especially preferable in space applications where a high degree of reliability is required and the certification processes and thus very time-consuming and costly. The acoustic protection arrangement 1 and method of manufacturing such an acoustic protection arrangement 1 are therefore superior compared with known solutions and techniques.
LIST OF REFERENCE SYMBOLS
[0100] 1 acoustic protection arrangement [0101] 2, 2, . . . acoustic protection module [0102] 3, 3 enclosure [0103] 4, 4 inlet [0104] 5 opening [0105] 6, 6 (interior) wall [0106] 7 partition [0107] 8 base plate [0108] 9 microperforated sheath [0109] 10 (internal) aperture [0110] 11 filler material or structure [0111] A first set of acoustic protection/absorber modules [0112] B second set of acoustic protection/absorber modules [0113] f.sub.p, f.sub.p, . . . peak absorption frequency