This application relates to visors for helmets and, more particularly, to aviation helmets.
Many helmets include a visor to protect the wearer's eyes from wind and debris. A visor may also be tinted to protect the wearer's eyes from sunlight. A visor may be retractable in order to enable the wearer to access the wearer's eyes or to obtain an untinted view. In aviation or other applications there may be sudden gusts of wind that may unintentionally retract the visor, such as if a pilot ejects from an airplane.
It would be an advancement in the art to improve the functioning of a helmet visor.
In one aspect of the invention, an apparatus includes a helmet configured to encase a head of a wearer and including a face opening for exposing at least a portion of a face of the wearer when the helmet is worn. The apparatus includes a visor assembly including a visor and a first arm secured to the visor. The first arm is movably secured the helmet such that the visor is positionable over the face opening when the visor assembly is in a down position and positionable above the face opening when the visor assembly is in a retracted position. The apparatus may include one or more structures fastened to one or more of the helmet and the visor assembly and configured to engage automatically when the visor assembly is in the down position to prevent movement of the visor assembly to the retracted position upon application of the inward and upward force on the visor assembly. The one or more structures may remain disengaged and not hinder movement of the visor assembly to the retracted position in the absence of the inward and upward force.
In some embodiments, the one or more structures include a shoulder extending inwardly from an outer surface of the helmet around the face opening. The shoulder may be positioned such that the inward and upward force urges an upper edge of the visor assembly against the shoulder.
In some embodiments, a shelf extends outwardly from the shoulder having the shoulder positioned between the shelf and the outer surface of the helmet. The shelf may be positioned to engage an inner surface of the visor responsive to the inward and upward force.
In some embodiments, the visor assembly includes one or more inwardly extending tabs configured to engage the helmet responsive to the inward and upward force when the visor assembly is in the down position.
In some embodiments, a second arm is secured to the visor. The first arm may be pivotally secured on a first side of the helmet and the second arm may be pivotally secured on a second side of the helmet. The face opening may be positioned between the first arm and the second arm. A first slot may be formed in the first arm and a second slot may be formed in the second arm. A first post may be secured to the helmet and pass through the first slot. A second post may be secured to the helmet and pass through the second slot. The first post may be slidable within the first slot and the second post may be slidable within the second slot. The first slot and the second slot may be configured to enable the visor to be pressed inwardly against the shoulder responsive to the inward and upward force.
In some embodiments, the apparatus includes a first arcuate slot formed in the first arm around the first slot and a second arcuate slot formed in the second arm around the second slot. The apparatus may include a first radial slot formed in the first arm and extending outwardly from the first arcuate slot and a second radial slot formed in the second arm and extending outwardly from the second arcuate slot. A first guide pin may be mounted to the helmet and be positioned in the first arcuate slot when the visor assembly is in the retracted position. The first guide pin may be positionable in the first radial slot when the visor assembly is in the down position responsive to the inward and upward force. A second guide pin may be mounted to the helmet and positioned in the second arcuate slot when the visor assembly is in the retracted position. The second guide pin may be positionable in the second radial slot when the visor assembly is in the down position responsive to the inward and upward force.
In some embodiments, the one or more structures include a protrusion extending rearwardly from the visor assembly and a receptacle mounted to the helmet. The receptacle may be positioned to receive the protrusion responsive to the inward and upward force. The protrusion may be sized and positioned not to engage the receptacle in the absence of the inward and upward force. The protrusion may be a tapered protrusion.
In some embodiments, the apparatus further includes a latch pivotally secured to the first arm and defining a first latching surface. The latch may include a biasing member urging the latch into engagement with a second latching surface mounted to the helmet when the visor assembly is in the down position. The engagement of the first latching surface with the second latching surface may hinder movement of the visor assembly to the retracted position. The biasing member and the second latching surface may be formed as a single member.
In some embodiments, a method includes subjecting the visor assembly in the down position to airflow causing an inward and upward force. The inward and upward force may cause movement of the visor assembly toward the face opening and cause the engagement structures to prevent pivoting of the visor into the retracted position.
The method may include, in the absence of airflow over the visor, pivoting the visor assembly between the down position and the retracted position without the one or more engagement structures hindering the pivoting.
In some embodiments, the method further includes responsive to the inward and upward force, urging an upper edge of the visor assembly against the shoulder thereby preventing the visor assembly from moving from the down position to the retracted position.
The method may include in absence of the inward and upward force, pivoting the visor assembly from the down position to the retracted position without the upper edge of the visor assembly engaging the shoulder.
In some embodiments, the method further includes sliding the first and second arms rearwardly relative to the first post and the second post responsive to the inward and upward force.
In some embodiments, the method further includes, while the visor assembly is in the down position, urging the second radial slot rearward over the first guide pin and urging the second radial slot rearward over the second guide pin responsive to the inward and upward force.
In some embodiments, the method further includes, with the visor assembly in the down position and responsive to the inward and upward force, urging the protrusion into the receptacle thereby preventing the visor assembly from moving to the retracted position.
In some embodiments, the method includes, with the latching assembly in the down position, pressing the latch and pivoting the latch such that the first latching surface moves out of engagement with the second latching surface.
Preferred and alternative examples of the present invention are described in detail below with reference to the following drawings:
Referring to
Retractability of the visor 14 may include arms 16 secured to either side of the visor 14 and extending to pivots 18 securing the arms 16 to the helmet 10 on either side of the face opening 12. Note that in the figures that only the right side of the helmet 10, visor 14, and other structures is shown in detail. Unless expressly indicated, the left side may be a mirrored configuration of the illustrated embodiments. The arms 16 may secure directly to the visor 14 or secure to a frame 20 extending completely or partially around the visor 14. For example, as shown, the frame 20 may extend around the top of the visor 14 and partially along the sides of the visor 14. The visor 14, arms 16, and frame 20 may be understood as being a visor assembly. The visor assembly may have a down position in which the visor 14 is positioned over and at least partially covering the opening 12 (see
When a pilot ejects from an airplane, the visor 14 is battered by high velocity air. A component of the velocity is typically directed inward, e.g., normal to the visor 14, urging the visor 14 into the opening 12. However, in many instances there is also an upward component that would tend to force the visor 14 into the retracted position. This can leave the pilot's eyes unprotected and subject to injury. Various structures are disclosed herein to prevent unintentional retraction of the visor 14.
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Each arm 16 may define an arcuate slot 28 having opposing sides that are substantially (e.g., within 2 mm of) concentric. A guide pin 32 that is fixed relative to the helmet 10 may insert within the slot 28 and be slidable within the slot 28. The guide pin 32 may be positioned such that when the guide pin 32 is positioned in the slot 28, the sides of the slot 28 are substantially (e.g., within 2 mm of) concentric with the a round part of the post 22 engaging the opening 24 in the arm 16.
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In the illustrated embodiment, pivotal securement may be provided by two pivot tabs 62 protruding outwardly from the lever 60. The tabs 62 may pass through openings 64 in the arm 16 such that openings 66 in the tabs 62 are positioned on an opposite side of the arm 16 from the lever 60. A pin 68 may be inserted through the openings 66 to retain the lever 60. The arm 16 may define a groove 70 into which the pin 68 seats.
A biasing member 72 may urge a first portion of the lever 60 away from the arm 16. In the illustrated embodiment, the biasing member is formed by a portion of the lever 60 that is cut away and having a protrusion 74 formed thereon and extending inwardly toward the arm 16. Accordingly, the first portion of the lever 60 may be urged toward the arm 16, thereby engaging the protrusion 74 with the arm 16 and deflecting the biasing member 72. The biasing member 72 will thereafter exert a biasing force urging the first portion the lever 60 urging the first portion away from the arm 16.
A second portion of the lever 60 on an opposite side of the pin 68 from the biasing member 72 may have a latching surface 76 formed thereon on a surface facing the arm 16 and the helmet 10. Accordingly, the biasing force of the biasing member 72 will urge the latching surface 76 toward the arm 16 and the helmet 10.
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As is apparent in the above description, resistance of unintentional retraction of the visor 14 may be provided by all of (a) the slot 30 engaging the guide pin 32, (b) the rim 48 and/or tabs 44, and (c) the protrusion 80 engaging the receptacle 82. All, any two of, or any one of (a), (b), and (c) may be used alone to resist unintentional retraction of the visor 14. For example, rather than use of a elongate opening 24 and radial slot 30, the opening 24 may be circular. Deflection of the visor 14 itself in response to an inward force may be sufficient to engage the shoulder 40, shelf 42, and/or recesses 46 sufficient to prevent unintentional retraction of the visor 14.
While the preferred embodiments of the invention have been illustrated and described, as noted above, many changes can be made without departing from the spirit and scope of the invention. Accordingly, the scope of the invention is not limited by the disclosure of the preferred embodiment. Instead, the invention should be determined entirely by reference to the claims that follow.