Cone for a loudspeaker with raised curved protrusions and method for controlling resonant modes - Patents.com

Abstract

A loudspeaker transducer diaphragm or cone (e.g., 201, 301, or 401) includes arcuate protrusions projecting distally from a major forward or distal surface 230 to provide stiffening and break-up of resonant vibration modes when the loudspeaker is in use. The protrusions (e.g., 210, 310, or 410) are convex on one surface 230 and concave on the opposite surface 234, so that their average thickness is approximately the same as the frusto-conical region of the cone; i.e., the nature of these surfaces is shell-like, rather than a solid mound or wall. The protrusions 210 are generally curved as they extend radially from the inner opening 204 to the peripheral edge, thereby promoting mode break-up (e.g., suppression of strong vibration modes such as those occurring in region 155).

Description

[Technical Field]

[0001] The present invention relates to a transducer diaphragm for a loudspeaker.

[0002] REFERENCE TO RELATED APPLICATIONS This application claims priority to commonly owned related U.S. Provisional Patent Application No. 62,879,889, filed July 29, 2019, which is incorporated by reference in its entirety. This application also broadly relates to commonly owned U.S. Patent Nos. 7,684,582 and 9,538,268, the entire disclosures of which are also incorporated by reference herein. [Background technology]

[0003] In a typical audio transducer, sound is produced by an electrodynamically driven diaphragm or cone reciprocating along an axis while supported by a suspension, thereby exerting a mechanical restoring force on the diaphragm or cone body.

[0004] A typical prior art or conventional electrodynamic loudspeaker driver (e.g., 100) is shown in Figure 1, and some terminology used by those skilled in the art will be reviewed to provide a technical background and context for the present invention. Referring to Figure 1, a cylindrical voice coil bobbin 103 has a conductive voice coil 102 wound around its outer periphery, which is attached to the center of a frusto-conical diaphragm or cone 101. The diaphragm 101 and voice coil bobbin 103 are secured to the inner peripheral edge of an annular or ring-shaped border or rim 108, which is secured to an annular damper or "spider" 109 with a selected compliance and stiffness. The outer edges of rim 108 and spider 109 are fixed to a rigid support frame or basket 112 that also carries a three-piece magnetic circuit (not shown), such that frame 112 supports diaphragm 101 and voice coil bobbin 103, allowing them to pistonically oscillate within the frame along a central axis 115 of bobbin 103. A centrally located "dust" cap 113 is fixed to diaphragm 101 to cover a centrally located hole in diaphragm 101, and moves integrally with diaphragm 101.

[0005] The edge 108 and damper 109 support the voice coil 102 and voice coil bobbin 103 in their respective predetermined positions within the magnetic gap of the magnetic circuit, which is comprised of a magnet (not shown), a plate or washer (not shown), and a pole yoke (not shown) including a central axisymmetric pole piece. This structure allows the diaphragm or cone 101 to oscillate axially in a piston-like manner within a predetermined amplitude range while being elastically supported without contacting the magnetic circuit.

[0006] First and second ends or leads of voice coil 102 are connected to respective ends of first and second conductive leads (not shown), which in turn are connected to first and second terminals (not shown) carried by frame 112. When an alternating current corresponding to a desired acoustic signal is sent through the leads at the terminals to voice coil 102, voice coil 102 responds to a corresponding electromotive force and is thus driven axially in the direction of piston-like vibration of diaphragm 101 within the magnetic gap of the magnetic circuit. As a result, diaphragm or cone 101 vibrates together with voice coil 102 and voice coil bobbin 103 and converts the electrical signal into acoustic energy, thereby producing sound waves such as, for example, music or other sounds.

[0007] Returning to first principles, the function of a loudspeaker or transducer (e.g., 100) is to convert electrical energy into an analog acoustic signal. This conversion process occurs in two steps. The first step is the conversion of electrical energy to mechanical energy. The second step is the conversion of mechanical energy to acoustic energy. The first step produces a mechanical displacement proportional to the electrical input signal. The second step couples the mechanical displacement of the system to the surrounding air through some mechanism, such as the forced movement of a diaphragm or cone 101. A class of loudspeakers known as electrodynamic loudspeakers employ a combination of permanent magnets (not shown) and electromagnets to produce the conversion from electrical energy to mechanical (or acoustic) energy.

[0008] A typical cone-equipped transducer (e.g., 100, shown in FIG. 1A ) suffers from the drawback that the cone body (101) exhibits non-piston behavior, resulting in a condition known as “cone break-up” when the cone body begins to flex and bend (see, e.g., region 155 as shown in FIG. 1B ) rather than all moving simultaneously in the same axial direction. This behavior occurs at certain frequencies determined by the specific design of the cone 101 and rim 108, where cone resonances or resonant modes result in distortions and deviations from a flat frequency response. Generally speaking, transducer cones (e.g., 101) generate the sound they are designed to produce when driven by a motor. These cones require low mass for high efficiency, which generally means they are thin. Because these cones are driven over a wide frequency range (or bandwidth), they inevitably are driven at frequencies or frequencies corresponding to the cone’s resonant modes. Driving the cone in resonant modes can cause deviations from a uniform, smooth frequency response. One way to mitigate the effects of such modes is to stiffen the cone so that these modes occur at higher frequencies (e.g., beyond the passband of the transducer). Making a rigid or stiff cone creates other tuning problems because rigid structures can be heavy. While rigid cones can be made from expensive laminate structures made of exotic materials, such transducer structures may not be commercially or economically justifiable for the desired loudspeaker system application. Summary of the Invention [Problem to be solved by the invention]

[0009] Therefore, there is a need for an effective yet economically affordable structure and method that provides high control over the behavior of the diaphragm (eg, cone) body while avoiding problems with the frequency response of the driver.

[0010] It is therefore an object of the present invention to overcome the above-mentioned drawbacks by providing an effective and economically affordable structure and method that provides greater control over the behavior of the diaphragm (e.g., cone) body and avoids problems with the acoustic frequency response of the driver. [Means for solving the problem]

[0011] In accordance with the present invention, the structure and method for fabricating the diaphragm in a loudspeaker transducer has economically incorporated structural features to control the resonant behavior of the cone so that there is no longer a single strong resonant mode. By dispersing these modes, many weak modes arise, as opposed to only one or a few strong modes. Strong modes cause larger deviations from the frequency response than weak modes, and many weak modes are superior to a few strong modes.

[0012] The loudspeaker transducer cone of the present invention has specially contoured protrusions extending from its major surfaces to provide stiffening and decoupling of resonant vibration modes. The protrusions are convex on one surface and concave on the other, so that their average thickness is approximately the same as the flat region of the cone (i.e., they are shell-like in nature, rather than solid). The protrusions are generally curved from the inside to the outside, thereby promoting mode decoupling (suppression of strong vibration modes). The curved, distally or forwardly projecting protrusions resemble an array of turbine airfoils; therefore, a preferred embodiment of the diaphragm is referred to as a "turbine cone," and the diaphragm preferably has a laminated or multi-layer foam core structure molded to the turbine geometry to provide a diaphragm with dramatically increased stiffness and damping without adding undesirable mass.

[0013] The cone body is made more rigid by using distal or forward-projecting protrusions that extend forward beyond the frusto-conical cone surface. Curving the turbine pattern protrusions partially eliminates consistent path lengths that can lead to strong vibration modes, resulting in modal breakup. The cone protrusions are preferably molded into the cone body to provide a unitary structure in the form of a generally rounded, curved bump, shell, or channel. The protrusions are convex on one side (preferably the front) and concave on the other side (the back), meaning that they have approximately the same thickness as the cone body and are generally not solid.

[0014] It is well known that a shell with even a small amount of curvature is significantly stiffer than a flat plate of the same size. This principle is roughly exploited in cones by introducing protrusions into the middle of the cone. These protrusions provide additional stiffness to the cone, pushing modes to higher frequencies (i.e., beyond the passband of the signal provided to the transducer from the host loudspeaker system). Alternatively, the protrusions may be more channel-like, in that they are longer than they are wide, and therefore each protrusion behaves more like a stiffening rib.

[0015] The curvature of the protrusions has the effect of "turbulence" the surface of the cone. This turbulence minimizes the number of different paths that can produce vibration modes of approximately the same length. Because modal frequency is a function of path length, creating many different path lengths means that a wide range of modes will be produced, but none of these modes will be strong. This means that many weak modes will be produced, rather than a few strong modes.

[0016] The curvature direction can be varied (e.g., clockwise or counterclockwise are likely to be equally effective), and mixing directions can provide additional mode decoupling, which can have performance benefits. Also, protrusion sizes do not need to be matched to each other, and a mix of sizes can be beneficial in providing additional mode decoupling.

[0017] The benefit of the protrusions can be seen by comparing the measured acoustic frequency response of a transducer with a traditional cone, which is not as smooth, especially at higher frequencies, as the same but non-configured transducer with a cone having the wide, raised, curved protrusions of the present invention.

[0018] The above objects, features and advantages of the present invention, as well as further objects, features and advantages, will become apparent from the following detailed description of specific embodiments of the invention, particularly when considered in conjunction with the accompanying drawings, in which reference characters in the various figures are utilized to designate like parts. [Brief explanation of the drawings]

[0019] [Figure 1A] FIG. 1 is a cross-sectional side view of a traditional loudspeaker driver with a truncated conical diaphragm, according to the prior art. [Figure 1B] FIG. 1B is a perspective view illustrating the undesirable behavior of the diaphragm of FIG. 1A during operation and showing the "split cone vibration" condition that occurs when the cone body undergoes non-piston vibration and begins to flex and bend (rather than all parts moving axially in the same direction at the same time). [Figure 2A] FIG. 1 is a side perspective view of a loudspeaker transducer cone having specially contoured protrusions extending from its major surface to provide stiffening and decoupling of undesired resonant vibration modes, the protrusions having a convex front or distal surface and a concave proximal or rear surface such that the average thickness of the protrusions is approximately the same as the flat areas of the cone, and the protrusions have a general curve from the central opening to the peripheral edge, promoting decoupling of resonant modes (suppression of strong vibration modes) in accordance with the structure and method of this invention. [Figure 2B] 2B is a photographic representation of a preferred embodiment of the driver of FIG. 2A installed in a full-range loudspeaker system in accordance with the structure and method of the present invention. [Figure 2C] 2C is an enlarged cross-sectional view of a foam core for the loudspeaker diaphragm of FIGS. 2A and 2B in accordance with the structure and method of the present invention. FIG. [Figure 2D]FIG. 2C is a front or proximal side view of the cone or diaphragm surface for the loudspeaker diaphragm of FIGS. 2A, 2B, and 2C, illustrating the curved locus defining the spaced apart centers that form the specially contoured protrusions extending from the central opening to the periphery in accordance with the structure and method of the present invention. [Figure 2E] 2D taken along line AA, showing one of the specially contoured protrusions extending from the central opening to the outer periphery in accordance with the structures and methods of the present invention. [Figure 3] 3A, 3B, and 3C are front (3A), top (3B), and side (3C) views of another embodiment of a reinforced loudspeaker diaphragm of the present invention, showing an equally spaced array of distally projecting curved narrow grooves or channels in accordance with the structure and method of the present invention. [Figure 4] FIG. 10 is a side view of the front or proximal surface of another embodiment of a reinforced loudspeaker diaphragm of the present invention, showing distally projecting, unequally spaced, curved, narrow grooves or channels in accordance with the structure and method of the present invention. [Figure 5] 2A-2E are perspective views illustrating a more desirable behavior of the diaphragm of FIG. 2A-2E during operation, showing how, in accordance with the structure and method of the present invention, specially contoured protrusions provide stiffening, thus decoupling, suppressing and reducing undesirable strong resonant vibration modes (e.g., in FIG. 1B), such that the cone body of the present invention behaves more like a piston, with less deflection and bending modes. [Figure 6] 1A and 1B ) and a pair of comparable frequency response plots of a first loudspeaker transducer and a second loudspeaker transducer driven in a loudspeaker system (e.g., as shown in FIGS. 2A-2D and 5 ) that result in a less desirable response shown by dotted line A, and a smoother, more desirable response shown by dashed line B in accordance with the structure and method of the present invention. DETAILED DESCRIPTION OF THE INVENTION

[0020] 2A-2E, an exemplary embodiment of an electrodynamic loudspeaker or transducer is shown (e.g., similar to 100, but with a modified diaphragm or cone). The modified transducer or cone 201 is symmetrical about a central axis 215 (which means that, as in FIG. 1A, the cone 201 may be incorporated into the driver motor structure as shown in FIG. 1A).

[0021] 2A-2E, in a first exemplary embodiment, an improved loudspeaker driver of the present invention has an improved diaphragm or cone 201 with seven economically accepted structural features 210 that are preferably shaped in place to control the resonant behavior of the cone so that there is no longer a single strong resonant mode. By dispersing the resonant modes, many weak modes arise as opposed to only one or a few strong modes (see, for example, FIG. 1B with FIG. 5). A strong mode (generally designated 155 in FIG. 1B) causes a larger undesirable deviation from the frequency response than a weak mode, and many weak modes (generally designated 255 in FIG. 5) are superior to a few strong modes.

[0022] 2A-2E is a generally frusto-conical loudspeaker transducer cone 201 terminating proximally in a central opening 204 configured to receive a voice coil former (e.g., 103). The cone 201 terminates forward or distally in a peripheral edge that projects radially outward from and symmetrically about a central axis 215 of a resonant vibration mode to provide a distal annular or circular surface bearing suspension 208, with seven specially contoured turbine or petal-shaped protrusions 210 extending or projecting distally from a main surface 230 to provide stiffening and decoupling of the resonant vibration mode. The protrusions 210 are convex on their distal or forward facing surface and concave on their opposite proximal or rearward facing surface, and thus their average thickness (e.g., 0.5 mm) is approximately the same as the frustoconical region of the cone (i.e., this means that the protruding petals or protrusions 210 are shell-like in nature, rather than thick solid features (which would add undesirable mass)).

[0023] These protrusions 210 are generally radially arrayed and curved from the inside of the central opening 204 toward the outer peripheral edge, thereby promoting mode decoupling (suppression of strong vibration modes). The distally projecting curved protrusions 210 resemble an array of turbine airfoils, and thus a preferred embodiment of the diaphragm or cone 201 is referred to as a "turbine cone" (e.g., as shown in the photographic representation of FIG. 2B), with the diaphragm preferably having a foam core structure (e.g., as shown in cross section in FIG. 2C) molded into a turbine geometry to provide a diaphragm with dramatically increased stiffness and damping without adding undesirable mass. Preferably, as shown in Figures 2A-2E, the diaphragm or cone (e.g., 201) has seven equally spaced turbine blade or petal-shaped convex protrusions 210 that protrude distally from the substantially frusto-conical front facing 230 of the cone by a protrusion projection distance 240 (e.g., about 3 mm) that is greater than the thickness of the cone (e.g., 0.5 mm).

[0024] In accordance with the method of the present invention, the protrusions 210 are molded from a polymer resin or foaming agent (e.g., polypropylene) by introducing a selected amount of foaming agent into an open mold, then closing the mold and applying a selected amount of pressure to cure the foam within the mold, and once cured, providing solid, imperforate front and back cone facings or solid (note that the modifiers "solid" and "solid" are used interchangeably herein, and may also be referred to as "solid") skin layers (230, 234) that encapsulate the foam core structure 232 (e.g., as shown in the photomicrograph of FIG. 2C). The difference in density and stiffness between the solid skin layers 230, 234 and the foam core 232 increases the cross-sectional stiffness of the cone (due to increased cross-sectional thickness) and increases internal damping due to shear between the rigid skin layers and the soft foam core 232. The cone body 201 and its protrusions 210 are molded distally from the distal or front surface 230 of the cone, with the protrusions 210 bulging or extending to a thickness significantly greater than the cone thickness (e.g., 0.5 mm as shown in Figures 2B and 2E). The cone body 201 and its protrusions 210 are molded together in situ, making the body of the cone lighter and more rigid. Curving the protrusions 210 partially eliminates consistent path lengths that can lead to strong vibration modes (e.g., as shown in Figure 1B), thereby providing the desired mode decoupling.

[0025] The cone protrusions (e.g., 210) are preferably molded in a radial array evenly spaced throughout the cone body, providing a unitary structure in the form of a preferably rounded and curved bump, shell, or channel that is convex on one side and concave on the other, meaning that they are approximately the same thickness as the cone body and are not formed as a solid distal protrusion overall. The curvature of the protrusions results in a cone face that is significantly stiffer and more resistant to bending moments than a flat cone face of the same size. The protrusions 210 prevent the generation of "oil can" bending modes and provide additional stiffness to the cone, pushing the mode to higher frequencies (i.e., beyond the transducer passband).

[0026] Figure 2B is a photographic illustration of a preferred embodiment of a driver constructed in accordance with the structure and method of the present invention, with the diaphragm 201 shown in Figure 2A installed in a full-range loudspeaker system. Figure 2C is an enlarged cross-sectional view of a 0.5 mm thick diaphragm showing the foam core for the loudspeaker diaphragm of Figures 2A and 2B. Figure 2D is a front or proximal side view of the cone or diaphragm surface for the loudspeaker diaphragm 201 of Figures 2A, 2B, and 2C, showing seven equally spaced curved radial loci defining spaced centers of reference for forming seven contoured turbine airfoil or petal-shaped protrusions 210 extending from the central opening 204 to the periphery of the diaphragm. Figure 2E is a cross-sectional side view taken along line AA of Figure 2D, showing one of the forward or distally bulging contoured protrusions above the central opening extending from the central opening 204 to the periphery in accordance with the structure and method of the present invention.

[0027] Alternatively, another embodiment of the diaphragm or cone 301 has protrusions 310 that are more channel-like in that their length is significantly greater than their width (see, e.g., FIGS. 3A, 3B, and 3C), with seven equally spaced channel-like protrusions 310 forming curved stiffening ribs 310 arranged in a radial array. Another exemplary loudspeaker transducer cone 301 shown in FIGS. 3A-3C is also generally frusto-conical, terminating proximally in a central opening 304. Distal to the cone 301 is a peripheral edge symmetrically formed about a central axis 315 that projects forward or distally to provide a distal annular or circular suspension surface 308. Specially contoured protrusions 310 extend or protrude distally from the primary cone surface to provide stiffness and decoupling of otherwise undesirable resonant vibration modes (as shown in FIG. 1B). The protrusions 310 are preferably convex on the distal or front surface and concave on the opposing proximal or back surface, so that the average cross-sectional thickness of the protrusions (e.g., 0.5 mm) is also approximately the same as the flat region of the cone (i.e., tubular rather than solid). These protrusions 310 are also generally curved from their center (inner) near the opening 304 to their outer peripheral edge, thereby promoting mode decoupling (suppression of strong vibration modes).

[0028] Yet another embodiment of the present invention provides a diaphragm or cone 401 with unequally spaced, curved radial protrusions 410 that are also more channel-like in that their length is significantly greater than their width (see, for example, FIG. 4 ), with the channel-like protrusions 410 behaving as unequally spaced, curved stiffening ribs. Another exemplary loudspeaker transducer cone 401 shown in FIG. 4 is also generally frusto-conical, terminating proximally in a central opening 404. The cone 401 terminates distally in a peripheral edge 408 that projects along a central axis 415 to provide a distal annular or circular surface with contoured protrusions 410 extending or projecting distally from the major surface for stiffening and breakup of resonant vibration modes. The protrusions 410 are preferably cylindrically convex on the distal side or front surface and concave on the opposing proximal side or back surface, so that the average thickness of the protrusions also approximates the flat portion of a cone (i.e., tubular rather than solid). These protrusions 410 are also generally curved from their center (inner) near the opening 404 to their outer peripheral edges, which promotes mode decoupling (suppression of strong vibration modes).

[0029] Rather than providing stiffeners or stiffeners aligned along straight radial lines, curving the protrusions (e.g., 210, 310, or 410) has been observed to have the effect of "disrupting" the paths of bending mode vibrations that would otherwise travel along the surface of the cone. This disruption minimizes the number of different paths of approximately the same length along which vibration modes can occur (see, e.g., FIGS. 1B and 5, which show comparative examples of a smooth traditional cone (101) and a modified cone with protrusions (201, with protrusions 210) when driven with drive signals having the same frequency and drive signal amplitude or level). The undesirable strong mode resonance behavior exhibited by the prior art cone 101 exhibits a large affected area (see generally reference numeral 155 in FIG. 1B), which means that strong resonant modes can occur, resulting in undesirable audible frequency response issues. By comparison, the behavior of the electrodynamic transducer of the present invention shown in Figure 5 when driven at the same resonant frequency exhibits only a narrow region of decoupled modes (see generally 255 in Figure 5), indicating that no strong modes are produced, and instead only a narrow region is affected by the decoupled modes, thereby causing less significant problems with respect to the frequency response of the transducer (e.g., as shown in Figure 6). In applicant's prototype testing, it was observed that the strong mode resonance has a significant undesirable effect on performance by strongly emphasizing a narrow frequency range, whereas the weak mode resonance produces only very little emphasis across that frequency range, resulting in a particularly smooth frequency response.

[0030] Because modal frequency is a function of path length, creating many different path lengths means that a wide range of modes are created, but none of these modes are dominant or powerful. This means that many weak modes (e.g., as seen in affected region 255 in FIG. 5 ) are created, rather than a few strong modes (e.g., as seen in affected region 155 in FIG. 1B ). While the directions for curving the protrusions (e.g., 210, 310, or 410) shown in FIGS. 2A-5 are exemplary, variations in such directions are possible; i.e., clockwise or counterclockwise curvatures are equally effective; mixing directions between adjacent protrusions (not shown) is believed to provide performance benefits, possibly by providing additional mode decoupling. Also, the sizes of the protrusions (e.g., 210, 310, or 410) need not match each other; a mix of sizes may also be beneficial, possibly providing additional mode decoupling.

[0031] Audibly perceptible and measurable benefits of the improved diaphragm (e.g., 201) include a smoother acoustic frequency response, as can be seen in FIG. 6, where the data plotted as curve A (dotted trace) represents the frequency response of an unimproved transducer with a traditional cone (e.g., 101) and the data plotted as curve B (dashed trace) represents an otherwise identical transducer with an improved resonant mode reduction cone (e.g., 201, 301, or 401). The plotted data for curve B is remarkably smooth, particularly in the more significant portions of the driver's frequency operating range (e.g., from a few hundred Hz to over 5 kHz). In particular, FIG. 6 shows the driver of FIGS. 2A-2E in which the measured acoustic frequency response for an exemplary embodiment of a 5.25-inch (13.34 cm) petal-cone driver is compared to an otherwise identical but conventional transducer, demonstrating that the driver structure and method of the present invention provides a particularly smooth and flat acoustic response throughout the transducer's operating passband. In particular, a 3.0 dB improvement in broadband response is achieved over the nearly three-octave wide 800 Hz to 5.0 kHz range, a passband critical to midrange reproduction for any high performance audio system.

[0032] The cone or diaphragm of the present invention (e.g., 201, 301, or 401) may be attached to and supported by a cooperating resilient material suspension member (e.g., 208 or 308) secured to a rigid support frame or basket, which also carries a three-piece magnetic circuit (not shown), such that the frame supports the diaphragm which, when actuated, can pistonically oscillate within the frame along a central axis.

[0033] As noted above, the purpose of the cone or diaphragm structure (e.g., 201, 301, or 401) and method of the present invention is to improve performance (compared to the prior art loudspeaker 100 of FIG. 1) by providing greater control over the behavior of the cone body. For the preferred (prototype) embodiment, the diaphragm (e.g., 201, 301, or 401) is a foam-core type cone made of polypropylene material molded into a single piece, as described above, but may also be made of other conventional cone materials (e.g., paper, molded fiber, or metal, such as aluminum). The resiliently supported cone (e.g., 201, 301, or 401) may be thinner than the conventional transducer cone 101, and such cone is supported by an elastic material suspension member (e.g., 208), which is preferably made of an elastic material, such as polyurethane foam, or some other soft, resilient, resonance-damping material.

[0034] As will be appreciated by those skilled in the art, the present invention provides a loudspeaker transducer including a diaphragm (e.g., 201, 301, or 401) with a plurality of symmetrically extending, radially arranged, distally projecting protrusions (e.g., 210, 310, or 410), the protrusions (e.g., 210, 310, or 410) being formed as convex surfaces or channel-like protrusions extending in equally spaced curved arcs from a central region of the cone to near the peripheral edge of the cone. In the exemplary embodiment shown in FIGS. 2A-5, certain protrusions (e.g., 210, 310, or 410) on the cone extend from the main facing to provide stiffening and decoupling of resonant vibration modes; these protrusions are convex on one surface and concave on the opposite surface, so that the average thickness of the protrusions is approximately the same as the flat areas of the cone; and the protrusions are generally curved as they extend from the inside to the outside, thereby promoting mode decoupling (suppression of strong vibration modes).

[0035] FIG. 5 is a perspective view of the cone 201 and front solid skin facing 230 showing the more desirable behavior of the diaphragm (e.g., of FIGS. 2A-2E) during operation, and illustrates how the specially contoured protrusions provide stiffening and thus decoupling to suppress and reduce undesirable strong resonant vibration modes (e.g., of FIG. 1B), thereby allowing the cone body of the present invention to behave in an approximately pistonic manner with less flexural and bending modes in accordance with the structure and method of the present invention. FIG. 5, like FIG. 1B, is a one-time diagram showing split vibration modes on a cone surface, and FIG. 6 is a pair of comparable frequency response plots of a prior art diaphragm or cone (e.g., of FIGS. 1A and 1B) that produces a less desirable response, shown by dotted line A, and a first loudspeaker transducer and a second loudspeaker transducer (e.g., as shown in FIGS. 2A-2D and 5) driven in a loudspeaker system, showing a smoother, more desirable response, shown by dashed line B, in accordance with the structure and method of the present invention. Based on applicant's research on the prototypes shown in FIGS. 2A-5, it is believed that avoiding symmetry in the layout of protrusions (e.g., 410) generally provides enhanced benefits from mode decoupling by reducing the number of modes with identical frequencies. One form of symmetry to be avoided is bilateral symmetry or mirror symmetry. A bilaterally symmetric cone (e.g., 101) allows for the generation of nearly identical modes on both halves of the cone, resulting in stronger modal behavior than is seen in cones lacking such symmetry. One way to achieve asymmetry according to the methods of the present invention is to use an odd number of lobes (e.g., 5 or 7 lobes). This method does not preclude radial symmetry (also called radial symmetry), but it offers the benefit of being more aesthetically pleasing than a radially asymmetric cone while still providing some of the benefits.

[0036] Based on Applicant's preliminary observations, the improved cone and method of the present invention provides a "piston-type" rigid cone, but because the wide protrusions (e.g., 210) do not extend to the cone's edges (e.g., 208), they do not stiffen the entire cone surface at low frequencies, instead providing a more localized stiffening effect that appears to result in the desired modal isolation and improved frequency response. In comparison, the channel-shaped protrusions (e.g., 310, 410) of the narrow-protrusion embodiment do not have protrusions that extend to the cone's outer edges (e.g., 308, 408), and therefore provide a more global stiffening effect because they are effectively ridges that provide stiffening at low frequencies. Assuming the channel-shaped protrusions (e.g., 310, 410) are hollow or tubular and curved, deflection at higher frequencies would result in approximately the same modal isolation.

[0037] As will be appreciated by those skilled in the art, the present invention may utilize a method for molding a loudspeaker transducer cone or diaphragm (e.g., 201, 301, or 401) from a polymer (e.g., polystyrene foam) by depositing the polymer into an open (e.g., two-piece, clamshell) mold assembly configured with an interior mold surface (not shown) for molding, compressing, heating (if necessary, depending on the material), and thereby forming a one-piece cone or diaphragm (e.g., 201) preferably having a plurality of radially arrayed distally projecting protrusions (e.g., 210, 310, or 410) that provide convex facings or channel-like protrusions extending in preferably equally spaced curved or curved arcs from a central region of the cone (e.g., 204, 304, or 404) to near the peripheral edge of the cone. In the next step, the mold assembly is closed to confining, compressing, and curing the polymer (e.g., foam) material to provide a lightweight, rigid, one-piece foam core diaphragm with non-porous proximal and distal facings and a substantially uniform thickness (e.g., 0.5 mm).

[0038] According to the method and structure of the present invention (e.g., as shown in Figures 2A-2E), the foam core structure 232 is the result of a molding technique in which molten plastic containing a blowing agent is injected into a mold (not shown) containing convex and matching concave features within the mold halves that together form the molded protrusion 210. The injection pressure (tons) prevents the blowing agent from initially forming bubbles (e.g., foam / burbuja). The mold surface is kept cool relative to the plastic by water flowing through strategically placed cooling tubes / channels within the body of the mold. The molten plastic that strikes the mold surface quickly solidifies and becomes a solid skin layer (ultimately becoming solid skin surface materials 230, 234). However, while the cone core is still in a molten state, the mold is slightly opened, thus reducing the pressure on the molten liquid and allowing foam / burbuja to form within the cone core (232). This process can be precisely controlled so that the thickness of the foam and solid skin layer is uniform and repeatable throughout production. As mentioned above, in the integrally formed cone body 201, the difference in density and stiffness between the solid skin layers 230, 234 and the foam core 232 increases the cross-sectional stiffness of the cone (due to the increased cross-sectional thickness) and increases the internal damping due to shear between the hard skin layers and the soft foam core 232.

[0039] While preferred embodiments of the new and improved diaphragm structure and distortion control method have been described, it is anticipated that other modifications, variations, and changes will occur to those skilled in the art in light of the teachings set forth herein, and it is therefore to be understood that all such modifications, variations, and changes are intended to be included within the scope of the present invention.

Claims

1. 1. A transducer cone for a loudspeaker, comprising a diaphragm or cone (e.g., 201, 301, or 401) with a plurality of radially arrayed distally projecting protrusions (e.g., 210, 310, or 410), the protrusions being formed as an odd number of convex surfaces or channel-like protrusions extending in spaced curved arcs from a central region (e.g., 204, 304, or 404) of the cone to near a peripheral edge of the cone; the diaphragm or cone has a foam core enclosed within solid skin layers on one surface and on an opposite surface; 1. A loudspeaker transducer cone, wherein the diaphragm or cone (e.g., 201) includes an array of seven equally spaced distally projecting turbine airfoil or petal-shaped convex protrusions, the convex protrusions projecting distally from the cone's frusto-conical facing (230) by a protrusion projection distance (e.g., 240) greater than the thickness of the cone.

2. 10. A transducer cone for a loudspeaker as in claim 1, wherein a protrusion on the cone provides stiffening and decoupling of undesired resonant vibration modes, the protrusion having one surface that is convex and an opposite surface that is concave, such that the average cross-sectional thickness of the protrusion is approximately the same as the flat area of ​​the cone.

3. 10. A transducer cone for a loudspeaker as claimed in claim 1, wherein the curved protrusions (e.g., 210, 310 or 410) of the cone have the effect of "disrupting" the path of bending mode vibrations that would otherwise travel along the surface (e.g., 155) of the cone, the disrupted vibration path instead resulting in a region (e.g., 255) of many weak resonant modes rather than a few strong resonant modes, thereby resulting in a transducer that exhibits a smooth frequency response.

4. 4. A transducer cone for a loudspeaker as recited in claim 3, wherein the curved protrusions (e.g., 310) of the cone are equally spaced in a symmetric radial array to provide uniform "disruption" of the path of bending mode vibrations that would otherwise travel along the surface of the cone.

5. 4. A transducer cone for a loudspeaker as claimed in claim 3, wherein the curved protrusions (e.g., 210, 310 or 410) of the cone result in a transducer (e.g., 201, 301 or 401) with increased cone stiffness, thereby driving resonant modes beyond the passband of the transducer and providing a smooth frequency response for a system including the host transducer.

6. 10. A loudspeaker transducer cone as in claim 1, wherein the cone protrusions consist of distally projecting curved protrusions (210) resembling a turbine airfoil or an array of petals, and the diaphragm preferably has a laminated or multi-layer (solid skin / foam core / solid skin) structure molded to the turbine geometry to provide a diaphragm with dramatically increased stiffness and damping without adding undesirable mass.

7. 7. A loudspeaker transducer cone as recited in claim 6, wherein the multi-layer (solid skin / foam core / solid skin) structure of the cone comprises a polystyrene foam core encapsulated within front and back non-porous polystyrene solid skin facings 230, 234.

8. 8. A loudspeaker transducer cone as in claim 7, wherein the difference in density and stiffness between the solid skin layers (230, 234) and the foam core (232) of the diaphragm or cone increases the cross-sectional stiffness of the cone and increases internal damping due to shear between the rigid skin layers and the flexible foam core (232).

9. 1. A method of providing a transducer cone or diaphragm for a loudspeaker, comprising the steps of: molding or fabricating a transducer diaphragm or cone for use in a host loudspeaker system to be driven over a selected frequency range or bandpass range, wherein the diaphragm (e.g., 201, 301, or 401) is molded or fabricated in an odd number with a plurality of radial arrays of distally projecting protrusions (e.g., 210, 310, or 410) formed as equally spaced convex surfaces or channel-like protrusions extending in curved arcs from a central region (e.g., 204, 304, or 404) of the cone to near a peripheral edge of the cone; the transducer diaphragm or cone has a foam core encapsulated in solid skin layers on one and opposite surfaces; The diaphragm or cone (e.g., 201) includes an array of seven equally spaced distally projecting turbine airfoil or petal-shaped convex protrusions, the convex protrusions projecting distally from the frusto-conical facing (230) of the cone by a protrusion projection distance (e.g., 240) greater than the thickness of the cone.

10. wherein the diaphragm (e.g., 201, 301, or 401) is molded from a plastic material with a polystyrene foaming agent by introducing the foaming agent into an open mold assembly configured to produce a one-piece cone or diaphragm having a plurality of radially arrayed distally projecting protrusions (e.g., 210, 310, or 410) formed as equally spaced, curved arc-extending convex surfaces or channel-like protrusions extending from a central region (e.g., 204, 304, or 404) of the cone to near a peripheral edge of the cone, the method comprising:

10. The method of claim 9, further comprising the step of closing the mold assembly to compress and cure the plastic, thereby providing a one-piece foam core or diaphragm having imperforate proximal and distal facings and a substantially uniform thickness.

11. the mold is comprised of mold halves with convex features and mating concave features, the convex and concave features together forming the molded protrusions 210, the mold having an open state and a closed state, and into the mold is injected molten plastic containing a blowing agent; The injection pressure (tons) of the injection step initially prevents the blowing agent from creating bubbles (e.g., foam / burbuja), and the mold surface is kept cool relative to the plastic by water flowing through strategically placed cooling tubes / channels formed within the mold; The molten plastic in and against the surface of the mold rapidly solidifies and becomes a solid skin (and ultimately a solid skin surfacer 230, 234) while the core of the cone is still in a molten state; The method of claim 10, wherein the mold is then slightly opened, thereby reducing the pressure on the molten plastic and allowing foam / gas bubbles to form the core (232) of the cone.

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