Abstract
A magnetic motion detection method for a helmet system includes an internal body inside a helmet shell that emits magnetic flux and rotates independently. When the helmet shell undergoes rotational acceleration from impact, a magnetic field sensor on the internal body detects acceleration data of the magnetic flux. A controller processes this data to store it, transmit it, or generate triggering signals for airbag deployment when thresholds are exceeded. The airbag system rapidly inflates around the user's neck and subsequently exhausts gas based on predetermined delay or pressure increases.
Claims
1. A magnetic motion detection method of a sensor arranged in an internal body worn by a person's head, the internal body inside of a helmet shell, the helmet shell configuring to emit a magnetic flux, comprising the steps of: impacting the helmet shell tangentially causing rotational acceleration of the helmet shell; detecting acceleration data of the magnetic flux with a magnetic field sensor positioned on the internal body; performing at least one of the following actions in a controller using the acceleration data: storing the acceleration data, transmitting the acceleration data, generating a triggering signal to inflate an airbag when the acceleration data equals or exceeds a predetermined threshold value.
2. The method of claim 1, wherein the triggering signal causes an airbag inflator to rapidly inflate the airbag around the person's neck by generating inflator gas directed into the airbag, and after a predetermined delay, exhausting gas from the airbag.
3. The method of claim 1, wherein the triggering signal causes an airbag inflator to rapidly inflate the airbag around the person's neck by generating inflator gas directed into the airbag, and exhausting gas from the airbag when increased pressure in the airbag results from impact of the person's head or helmet shell with the airbag.
4. The method of claim 1, wherein the triggering signal causes an airbag inflator to rapidly inflate the airbag around the person's neck by generating inflator gas directed into the airbag, and exhausting gas from the airbag upon at least one of: a predetermined delay, or increased pressure in the airbag from impact.
5. A helmet system comprising: an internal body configured to be worn by a person's head; a helmet shell surrounding the internal body, the helmet shell configured to emit magnetic flux and able to rotate independently of the internal body; a magnetic field sensor positioned on the internal body and configured to detect acceleration data of the magnetic flux when the helmet shell undergoes rotational acceleration; a controller configured to perform at least one of: storing the acceleration data, transmitting the acceleration data, generating a triggering signal to inflate an airbag when the acceleration data equals or exceeds a predetermined threshold value.
6. The helmet system of claim 5, further comprising an airbag inflator configured to rapidly inflate an airbag around a person's neck by generating inflator gas directed into the airbag, and to exhaust gas from the airbag after a predetermined delay.
7. The helmet system of claim 5, further comprising an airbag inflator configured to rapidly inflate an airbag around a person's neck by generating inflator gas directed into the airbag, and to exhaust gas from the airbag when increased pressure in the airbag results from impact.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0029] FIG. 1A is an illustration of the invention, with cutaways to show each component therein.
[0030] FIG. 1B is a flowchart that shows how components of the invention are linked and nested.
[0031] FIGS. 2A & 2B are schematic illustrations of how magnetic flux induces torque that dampens the transmission of rotational acceleration to the internal body.
[0032] FIG. 3 is a schematic illustration of how non-magnetic metal rings surrounding internal magnetic force emitters dissipate kinetic energy.
[0033] FIGS. 4A & 4B illustrate an attachment system for magnetic force emitters.
[0034] FIG. 5 is an illustration of the invention, with a cutaway to show motion sensor configuration.
[0035] FIG. 6 is an illustration of the motion sensor configuration.
[0036] FIG. 7 is a schematic illustration of the motion sensor system operation.
[0037] FIG. 8 illustrates an airbag deployment.
[0038] FIG. 9 is a flowchart that shows the logic of the airbag deployment process.
[0039] FIGS. 10A & 10B illustrate the helmet restoration system.
[0040] FIG. 11 illustrates a mechanical response system.
[0041] It is to be noted, however, that the appended drawings are not to scale and illustrate only typical embodiments of this disclosure, and are therefore not to be considered limiting of its scope, for the apparatus, kits, and methods of the disclosure may admit to other equally effective embodiments.
DETAILED DESCRIPTION OF THE INVENTION
[0042] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term and/or includes any and all combinations of one or more of the associated listed items. As used herein, the singular forms a, an, and the are intended to include the plural forms as well as the singular forms, unless the context clearly indicates otherwise. In describing the invention, it will be understood that a number of techniques and steps are disclosed. Each of these has individual benefit and each can also be used in conjunction with one or more, or in some cases all, of the other disclosed techniques.
[0043] The present disclosure is to be considered as an exemplification of the invention, and is not intended to limit the invention to the specific embodiments illustrated by the figures or description below. In particular, the disclosure describes helmets used in U.S. football. The same problems can arise in other endeavors where helmets are used. These include ice hockey, particularly the position of goalie; motorcycle riding; and military use.
[0044] FIG. 1A illustrates a user wearing an RDH as disclosed. External magnetic force emitters 119 composed of arrays of tiny magnets are configured in pads 105 of the exterior shell 103, and internal magnetic force emitters composed of arrays of tiny magnets 123 are configurably attached to the interior cover 125, the illustration displaying magnetic force emitters as they are incorporated by reference from U.S. patent application Ser. No. 17/845,780 and prior U.S. patent application Ser. No. 16/689,086 which is now U.S. Pat. No. 11,464,270. The interior-facing magnet flux extending inwards of external magnetic emitters 119 and the interior magnet flux extending outwards of internal magnetic force emitters 123 are axially aligned 121 in a resting state. Magnetic flux interactions are further disclosed in FIGS. 2A & 2B. Magnetic energy dissipation rings 122 are attached around internal magnet force emitters 123 and are further disclosed in FIG. 3. A magnetic flux motion sensor system is composed of a motion sensor 115, and, as shown in dotted lines, a connection line 117 that communicates sensed motion data to a controller 127, which is connected to an airbag inflator 131 that is connected 135 to a chamber 137 with contents that inflate airbag 133. The magnetic flux motion sensor system is more fully disclosed in FIGS. 5, 6, & 7, and the airbag and airbag deployment process are more fully disclosed in FIGS. 8 & 9. The RDH post-collision restoration system is composed of tension absorbing components 107, with orfices 109 in which stretchable chords 113 are configured to connect the tension absorbing components 107 which are spread around cylinder 111 on the head cover 125. The RDH post-collision restoration system is disclosed in more detail in FIGS. 10A & 10B. Other methods to restore the helmet shell include mechanisms 139 located below the head, attached to the bottom of the helmet shell. These absorb energy, and may include motors to move the helmet shell. The RDH mechanisms below the head are disclosed in more detail in FIG. 11.
[0045] FIG. 1B is a flowchart of the current application, showing how various figures and embodiments are linked and nested in the disclosure. Magnetic force emitters produce magnetic flux; emitter configuration and magnetic flux are intrinsically linked yet can be distinctively articulated to best reveal nested configurations and processes. Magnetic force emitter configurations are disclosed in FIGS. 1A, 2A & 2B, 3, 4A & 4B, and 10A & 10B. Magnetic flux motion sensing processes, including sensor activated airbag deployment, are disclosed in FIGS. 1A, 5, 6, 7, 8, 9, and 11. FIG. 1B flowchart elements include the reference numbers that point to components on FIG. 1A as well as listing the figures in this application that disclose each component in detail.
[0046] FIG. 2A illustrates a side view schematic diagram of an exterior shell 203 and an internal body 205. In an embodiment external magnetic force emitter 207 attached to the exterior shell 203 emits magnetic flux 208 with N polarity axially towards an internal magnetic force emitter 215 attached to the internal body 205 emitting magnetic flux 216 with N polarity. External magnetic force emitter 209 adjacent to external magnetic force emitter 207 emits magnetic flux 210 with polarity S axially towards respective internal magnetic force emitter 217 attached to the internal body 205 that has magnetic flux 218 with polarity S facing out. A internal magnetic force emitter attached to the internal body may have a barrier 221 which is not permeable to magnetic fields.
[0047] FIG. 2B illustrates a side view schematic diagram of an embodiment wherein helmet shell 203a has received a tangential blow 230 that accelerates helmet shell 203a to rotate and translate in the direction of the impact force impulse. External magnetic force emitter 209a has a rotated and translated position such that it approaches internal magnetic force emitter 215a, with magnetic flux 210a and magnetic flux 216a inducing magnetic attraction 243, which causes internal magnetic force emitter 215a to move in the opposite direction of the tangential blow. Simultaneously, magnetic flux 208a from external magnetic force emitter 207a generates magnetic repulsion 245 with magnetic flux 216a below the level of barrier 221a. This drives internal magnetic force emitter 215a further in the opposite direction. All magnetic force emitters attached to helmet shell 203a move together. Magnetic flux 210a which rotates towards magnetic force emitter 215a generates magnetic repulsion 247 with magnetic flux 218a that pushes internal magnetic force emitter 217a in the opposite direction, amplifying the negative torque on the internal body 205a.
[0048] FIG. 3 illustrates how magnetic force energy displacements dampen transmission of rotational motion to the internal body. When a magnetic field quickly moves towards copper (or other metals) it sets up electrical eddy currents, which dissipate kinetic energy. For each individual metal ring 327, 329, and 331 the eddy currents are small. But as all magnetic force emitters 305 attached to the helmet shell 301 move as an ensemble, although individual magnetic force emitters 307 and 309 are separated by 4, 5, 6 or more cm's, the aggregate energy dissipation from the ensemble of metal rings 311 is significant. As the helmet shell 301 rapidly rotates in the direction of the arrow 313, helmet shell magnetic force emitter 307 and magnetic flux 314 and magnetic force emitter 309 and magnetic flux 316 rapidly move from initial positions 308 and 310 respectively. Magnetic fluxes 314 and 316 intersect magnetic fluxes 315, 317, and 319 from magnetic force emitters 321, 323 and 324 respectively, attached to internal body 325. As neighboring magnetic fluxes 314 and 316 alternate in their polarity facing the internal body 325, and as neighboring magnetic fluxes 315, 317, and 319 alternate in their polarity facing the helmet shell 301, the magnetic fluxes intersecting metal rings 327, 329, and 331 induce counter-clockwise eddy currents 333, 335, and 337. The ensemble of eddy currents 339 dissipate the kinetic force of the helmet shell 301 movement.
[0049] The dissipation can be measured using the electromotive force , which is calculated with the change in magnetic flux that occurs as the helmet shell magnetic emitters move across the internal body magnetic emitters, =/t. Helmet rotations are fast, which increases value. is thus the magnetic flux area B(L) change in a period t. The current I that is generated from the resistance to is:
[00001]
where v is the voltage of the current that rises in opposition, and R is the resistance of the metal. Kinetic energy E.sub.k dissipated in the resistance:
[00002]
As an example, consider a helmet shell magnetic force emitter that moves from position 0.04 cm to 0.07 cm in 0.05 s.
[00003]
[0050] where R (0.002) is twice the resistance of a 0.01 m.sup.2 cooper ring. This generates very little electricity. The aggregated current of an ensemble of 12 metal rings remains small. However, because it occurs over a brief period, 0.05 s, the kinetic energy dissipated is not negligible. This adds to the negative torque delivered to the helmet cover, which dissipates even more energy.
[0051] FIGS. 4A & 4B illustrate an embodiment with a rotary housing to reduce rotational force transmission to the head of a user of an RDH helmet. FIG. 4A shows the rotary housing comprising at least one first unit 405 configured with an external magnetic force emitter 407 that rotates on a spindle in a cylindrical structure 409 which is attached via a housing 411 to the interior 413 of the helmet shell 401, and at least one second unit 415 with a barrier 417, quasi-spherical shaped, that is attached to the internal body 403, and under the barrier an internal magnetic force emitter 419 is attached at a base 421 (visible as dotted lines) to the internal body 403, the base 421 capable of rotating and thereby pushing on the internal body 403. The external magnet magnetic force emitter 407 with a polarity facing the head cover 403 that is opposite of the polarity of the internal magnet force emitter 419 polarity facing the helmet shell 401, and the external magnetic force emitter 407 and the internal magnetic force emitter 419 are aligned in a resting condition. The cylindrical structure 409 and the barrier 417 each have outside surfaces composed of a material such as polytetrefluoroethylene to slide with very little friction. The base shown in dotted lines 421 is illustrated at 441 composed of a thrower link 443 that connects to the internal magnet force emitter 419, the thrower link 443 being connected at 445 to an impeller 447 configured with impeller contacts 449 which are positioned in the internal body 403 such that when the impeller 447 moves it pushes the internal body 403.
[0052] FIG. 4B illustrates the result of a tangential motion 431 that causes helmet shell 401a to rotate and translate on the RDH user's head, the first unit 405a cylindrical structure 409a moves down the side of the barrier 417a, causing the magnet flux of the external magnetic force emitter 407a and the magnetic flux of the internal magnetic force emitter 419a to form an magnetic attraction dipole which rotates the internal magnetic force emitter 419a such that the base 421a pushes the head cover 403a in a negative torque direction 433 opposite to the helmet shell's tangential motion 431, thereby transmitting negative torque as an energy damping force to the internal body 403a in response to tangential motion 431 of the helmet shell 401a. In a further embodiment illustrated in FIG. 4A, the cylindrical structure 409 itself rotates, and is attached via housing 411 to the interior 413 of the helmet shell 401, with the external magnetic force emitter 407 in the cylindrical structure 409 moving in accordance with the cylindrical structure 409 rotation.
[0053] FIG. 5 illustrates a helmet shell 501 cut open, to reveal an embodiment with an internal body 503 on which a motion sensor 513 is configured below an external magnetic force emitter 507 that is embedded in a cushion pad 505 attached in the helmet shell 501. Also shown is an internal magnetic force emitter 509 located on an internal body 503 which will torque negatively to the helmet shell 501 motion, with a metal ring 511 that dissipates transmitted magnetic force. When the helmet shell 501 moves tangentially the magnetic flux associated with the external magnetic force emitter 507 moves across the motion sensor 513 which detects a rate of acceleration of the magnetic flux. The motion sensor 513 transmits data in a data line 515 through a connection 517 to a controller 519 that can record, process, and trigger a response to the data. In another embodiment the motion sensor transmits data wirelessly to a controller or receiver on the player or elsewhere.
[0054] Using Hall effect sensors, magnetic fields can be continuously measured. A sudden surge due to tangential collision will have an established pattern. The sensor can immediately trigger a response to an extreme rotation situation. The output signal from a Hall effect sensor is the function of a magnetic field density around the device. The velocity at which a magnetic flux moves is measured by the frequency of the magnetic field density amplitude changes. When the magnetic field density around the sensor reaches or exceeds a predetermined risk level, the frequency reaches or exceeds a predetermined threshold, and the sensor generates an output voltage called the Hall Voltage. Hall effect sensors are more reliable than mechanical switches, and do not suffer from environmental impacts, a key attribute in a helmet that receives severe contact. They can be flat, have no moving parts, and are highly sensitive to magnetic fields. This provides a tool for medical professionals and scientific researchers to monitor, assess, and address helmet shell movement.
[0055] FIG. 6 illustrates an embodiment with an omnidirectional motion sensor. In the embodiment the sensor is configured with three more or less orthogonal coils and electronics to integrate the coil signals. As the helmet shell rotates over the orthogonal axes, spherical harmonics ( which measures rotation from apex down, which measures rotation around the equatorial plane) are solved. The general solution V.sub.H of a spherical helmet's movement is a linear combination of the spherical harmonic functions multiplied by an appropriate scale factor (the helmet shell radius.)
[00004]
where c.sub.lm are constants and the factors r.sub.l and Y.sub.lm are regular solid harmonics, expanded below.
[00005]
[0056] Y.sub.lm scales with the radius of the helmet. P represents a set of orthogonal polynomials, often Legendre polynomials, which do not require differential equations. The polynomials are complete, and all coefficients can be predetermined. Because the helmet is not a ball, there are non-linear effects. Precision of 10.sup.4 requires sensor cards to handle up to 200 parameters per sensor card, although many of these are constant, common, or depend on others. Cards such as Siemens KSY44 are sufficient, robust, extremely thin, and can be rapidly calibrated.
[0057] In the FIG. 6 embodiment an internal body 601 worn by a user 603 is configured with internal magnetic force emitters such as 605 and an omnidirectional orientation sensor 607 which is composed of a container 609 and, viewed in cutaway, X-axis 611, Y-axis 613, and Z-axis 615 coils and easily calibrated sensor cards 617. Integrated electronics 619 process input signals transmitted through connector 621 to controller 623. Internal magnetic force emitters such as 605 are positioned to torque orthogonally to the interior-facing magnetic fluxes during a collision. In this embodiments the linear output is directly proportional to the applied magnetic field. Orientation sensor 607 may be further configured with amplification material that enhances measurements. Orientation sensor 607 can rapidly detect the external shell's acceleration in at least three orthogonal directions. Orientation sensor 607 may be a magnetic field sensor, such as a Hall effects sensor, or other sensors such as position, velocity, accelerometer, or gyroscopic devices. Uninflated airbag neck component holder 625 snaps around the user's neck, and contains the uninflated airbag component. Gas generators or compressed gas, which may comprise tablet formulations and other compositions known in the art, are incorporated into inflator unit 627. Hybrid and pressurized gas inflators may also be employed in a known manner. From the time the orientation sensor 607 detects the collision to the time the air bag is fully inflated is only 30 milliseconds, or 0.03 second. In 0.03 second, about 1.3 inches of rotational movement may occur. This is less than the rotational distance of an ordinary collision, and significantly less than the distance induced by a severe collision. In a further embodiment a sensor 629 is located below the head, at its base, such as on the shoulder area close to the neck. The sensor detects an interior-facing magnetic flux from an external magnetic emitter attached to the helmet shell in a position proximate to the sensor location, such as beneath the helmet shell ear slot. If a tangential impact causes the entire head to pass a threshold of rotational acceleration, the sensor below the head may detect this, leading to a process that triggers the airbag inflator.
[0058] FIG. 7 is a schematic illustration of an embodiment in which a CMOS sensor 707 is used because of its sensitivity and low cost. The sensor 707 has a rotation invariant geometry, with an N-well 709 in a P-substrate 711. Because stress changes the electrical resistance of Silicon [Si] by changing its resistivity, deformations of the sensor can induce mechanical stress that may change the magnetic sensitivity. To prevent this, the sensor 707 rests on a solid base 713, to prevent sensor 707 from bending. Sensor 707 output voltage is directly proportional to the applied magnetic field. In the CMOS setup, the output voltage equation is:
[00006]
[0059] G is the geometrical correction factor, .sup.rH of Si=1.15 (the scattering factor), n is the doping factor, h is the thickness of the n-well, and B is the applied magnetic field.
[0060] Helmet shell 701 external magnetic force emitter 715 has interior-facing magnetic flux 720 polarity N 719 facing the internal body 705 directly over sensor 707 in resting state T1 719. This corresponds to sensor 707 detected field D1 731. During a tangential collision, the helmet shell 701 rotates to position 701a as the external magnetic force emitter 715 accelerates at a given rate to position T2 721, reaching position 715a as interior-facing magnetic flux moves to 720a, the acceleration corresponding to detected field density D2 733, and at position T3 723 interior-facing magnetic flux 720b has rotated at a given acceleration rate that corresponds to detected field density D3 735. The rate of change of density fields D2 and D3 is compared to predetermined acceleration rates and may trigger a compensation method, data recording, and/or data transmission.
[0061] FIG. 8 illustrates an embodiment in which a concussive acceleration is detected, and controller 809 triggers airbag inflator 807 positioned proximate to a helmet, connected to a neck yoke 805 composed of airbag 811. At resting state 801 airbag 811 is uninflated. At beginning state 802 airbag 811a begins to inflate. At filled state 803 airbag 811b is filled, prior to deflation. This fills the empty space between a user and the helmet's elements, and prevents neck muscles from twisting, or in other ways maintains a user's head from moving rapidly.
[0062] FIG. 9 schematically depicts a flow chart which illustrates by way of example an operation of the sensor embodiment. The helmet shell's independent motion is detected by sensors as a data of a magnetic flux acceleration rate. The data may be recorded and/or transmitted, or not. This may complete the action of the sensor embodiment. In a further embodiment, a controller may activate an airbag and/or expansion mechanisms.
[0063] If an airbag is available, the controller determines a concussion risk corresponding to the data. If a concussion risk threshold is reached, the controller may activate the air bag inflator circuit. The airbag inflation occurs in 30 milliseconds or less, which is the current tolerance for side curtain air bag deployments in vehicles. The RDH helmet user's head, or the helmet shell, impacts the airbag which increases pressure in the airbag, or a predetermined delay occurs, either of which causes a relief valve to open and exhaust inflation gases.
[0064] If expansion or energy absorbing mechanisms are available, a controller logic element
[0065] determines if helmet shell motion can be modified by one or more mechanisms, and if so, a power source changes their configuration. The mechanisms help reduce the helmet shell motion and/or restore the helmet shell to a resting state.
[0066] FIGS. 10A & 10B illustrate a preferred embodiment with a helmet shell restoration system which serves to return the helmet shell to its resting state position after a tangential impact causes the helmet shell to rotate and translate.
[0067] FIG. 10A illustrates the helmet shell in a resting position, not during a tangential impact. Helmet shell 1001 is configured with container insert 1011 that contains component 1019 and is attached in the helmet shell 1001 at 1013, component 1019 connecting tension absorbing elements 1002, 1003, 1004, and 1005 each with stretchable chords 1017 via orifices 1015. Each of the tension absorbing elements 1002, 1003, 1004, and 1005 have a spring-like element 1007 seen in cutaways. The base of each element is constrained in movement by cylinder 1009 on the internal body.
[0068] FIG. 10B illustrates the embodiment after a tangential impact in direction of arrow 1031. Stretchable cords 1017a connecting tension absorbing elements such as 1003a and 1005a are placed under tension sufficient to cause spring-like elements such as 1021 to expand. As helmet shell 1001a moves tangentially, container 1011a moves correspondingly and pushes down, and tension absorbing elements such as 1003a contain a spring-like element 1007a that compresses. The cylinder 1009a is employed to prevent forward motion of elements such as 1005a. When tangential motion ceases, the tension stored by spring-like elements such as 1007a is released, and the stretchable chords such as 1017a recover their resting states, returning container 1011a to its resting position.
[0069] Other methods may be used to urge the helmet shell to return from a second state in which it has been moved by external impact to the first, resting state. These include an embodiment with a spring assembly biased to maintain the helmet shell in the first resting state. When the helmet shell is tangentially impacted with force to overcome the biased state and the helmet shell moves relative to the head cover, the spring assembly acts to return the helmet shell back to the first, resting state. Another embodiment uses a toothed wheel, which is engaged with a finger from the helmet shell in a first, resting state, and which rotates to a second state when the helmet shell moves relative to the head cover, and the wheel is configured to return to the first resting state. In a further embodiment, as illustrated in FIG. 11, mechanisms 1103a, 1103b, and 1103c may restore the helmet shell to the first, resting state after helmet shell movement.
[0070] FIG. 11 illustrates an embodiment wherein mechanisms 1103a, 1103b, and 1103c, composed of materials such as polymers able to perform rapid conformational changes, are configured to dampen helmet shell motion to limit head movement injury, and/or return the helmet shell to a resting state. In other embodiments mechanisms 1103a, 1103b, and 1103c may be hinges, pistons, or other structures capable of compression and expansion. In an embodiment, when a tangential impact causes the helmet shell to rotationally accelerate, mechanisms 1103a, 1103b, and 1103c dampen the motion. In another embodiment, motors 1105a, 1105b, and 1105c, or in other embodiments an electromagnetic source, power a change in the configuration of one or more mechanisms 1103a, 1103b, and 1103c to move one or more attachment units 1107a, 1107b, and 1107c, attached to the helmet shell 1109, thereby changing the distance between the helmet shell 1109 and one or more plates 1111a, 1111b, and 1111c. This may dampen the rotational acceleration of the helmet shell 1109, or return the helmet shell 1109 to the resting state. Mechanism 1103a is shown in an expanded state, while mechanism 1103b is shown in a retracted position. The controller and power source are in the pack 1113 worn by the player 1115, and are connected to each motor 1105a, 1105b, and 1105c via conduits 1117a, 1117b, and 1117c. The controller includes a logic element that determines mechanism response.
[0071] Given the disclosure of the present invention, one versed in the art would appreciate that there may be other embodiments and modifications within the scope and spirit of the invention. Accordingly, all modifications attainable by one versed in the art from the present disclosure within the scope and spirit of the present invention are to be included as further embodiments of the present invention. The scope of the present invention is to be defined as set forth in the following claims.
DISPOSITION OF SUBJECT MATTER
[0072] This is a continuation-in-part application submitted more than one year after the parent application (U.S. patent application Ser. No. 17/845,780) and after the grandparent application, now a patent (U.S. Pat. No. 11,464,270). The following disclosures and claims are either: 1) provided in a manner as described in the first paragraph of 35 U.S.C. 112 in the prior-filed applications, and therefore have the benefit of grandparent application priority date, marked as A; or 2) are supported by the parent and grandparent applications and disclose nonobvious configurations and mechanisms to further enable them, and therefore have the priority data of this current submission, marked as B.
TABLE-US-00001 Claim Status 1 A 2 B 3 B 4 A 5 B 6 B 7 B 8 B 9 B 10 A 11 A 12 A 13 A 14 A 15 A 16 A 17 B 18 B
[0073] The grandparent application provided detailed disclosures of tiny magnets assembled as three-dimensional arrays that amplify magnetic flux in a single polar direction. It showed how these assemblies may be configured in a helmet and on a head cover. Both the parent and grandparent applications disclose how magnetic flux interactions induced by assemblies in a helmet and on a head cover cause negative torque through repulsive magnetic flux interactions that dampen rotational acceleration. This application provides new configurations of the parent and grandparent disclosures to maximize their effect. The compound magnetic emitters in the previous applications can be arranged to amplify negative torque by harnessing both magnetic flux attraction and repulsion; they may be spread apart at certain distances. As this involves the grandparent disclosure arranged in a more effective pattern, it is anticipated that these claims 1, 10, 11, & 12 will have the same priority date as in the grandparent application.
[0074] A novel, nonobvious modification of the parent and grandparent applications is also included in this application, namely a non-magnetic metal ring that may surround an internal magnetic emitter to dissipate energy transmitted by an interior-facing magnetic flux generated by an external magnetic emitter. It is anticipated that this claim 2 will have a priority date concurrent with the submission date of the current application. Also included is a novel, nonobvious housing for the external magnetic emitters and an associated novel, nonobvious attachment for the internal magnetic emitters, which allows a counterintuitive use of magnetic attraction interaction to directly transmit negative torque motive force to the internal body. It is anticipated that this claim 3 will have a priority data concurrent with the submission date of the current application.
[0075] The grandparent and parent applications disclosed the limitation that the helmet shell, after being moved relative to the internal body, returned to a first, resting state. This application provides a configuration, namely a biased spring, that expresses the functions described in earlier applications. It is anticipated that this claim 4 will have the same priority date as in the grandparent application. Novel, nonobvious systems and methods to perform this function are also introduced, in claims 5, 6, & 7. It is anticipated these claims will have a priority data concurrent with the submission date of the current application.
[0076] A novel, nonobvious system and method to dampen rotational acceleration uses energy-absorbing structures. It is anticipated that claims 8 & 9 will have a priority date concurrent with the submission date of the current application.
[0077] A previously disclosed subject matter in the parent and grandparent applications, in their specifications and claims, described magnetic sensor systems and methods to use the sensor data to trigger an airbag about the user's head, including figures. Claims concerning the sensors and airbags were withdrawn after a restriction requirement. They are herein reintroduced in claims 13, 14, 15, and 16. It is anticipated that these claims will have the same priority date as when they were introduced in the grandparent application.
[0078] A novel, nonobvious use of the magnetic sensor system is also included in this application, namely the sensor data is used to restore and reposition the helmet shell to its first, resting state after it has been moved by an impact. The sensor data is also used in a similar system to dampen the movement of the helmet shell or the internal body with a structure that can rapidly change conformation. These uses may incorporate a small motor to power the restoration or damping. It is anticipated that these claims 17 & 18 will have a priority date concurrent with the submission date of the current application.
