Patent Abstract:
An improved vehicle glareshield having a structural body having a predetermined size and shape adapted to protect an instrument panel in a vehicle from glare; and a plurality of controlled strength members carried in said structural body which collapse in a controlled manner upon high force impact by an occupant in order to reduce a deceleration force experienced by an occupant upon impact with said instrument panel.

Full Description:
This application claims the benefit and filing date of U.S. Provisional Patent Application No. 60/177,317, filed Jan. 21, 2000, titled, “Crash Energy Absorbing Glareshield and Method of Protecting Against Head Injury in Aircraft Crashes.” 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The present invention relates in general to glareshields for use in vehicles, particularly in fixed and rotor wing aircraft. More particularly, in particular to glareshields that enhance safety during aircraft crashes. 
     2. Description of the Prior Art 
     While significant progress has been made to increase the safety of fixed wing and rotor wing aircraft, a significant number of crashes still occur. However, the survivability of aircraft crashes has increased with incremental advances in the engineering of the aircraft and of the aircraft components. Head injuries, in particular, must be avoided in order to further increase the overall survivability. 
     This has been demonstrated in automobile safety advances, such as the implementation of air bag safety equipment, which protect the head and upper body of the driver and passenger in the front seats. A comparable situation arises in aircraft. The pilot and copilot are restrained by safety belts and safety harnesses. In longitudinal crashes, the restrained crew member experiences significant forward head motion which sometimes causes the head to strike the glareshield and/or instrument panel. This can cause severe injury or death in a crash which would have been otherwise survivable. 
     SUMMARY OF THE INVENTION 
     The present invention is directed to an improved glareshield for use in vehicles, particularly in fixed wing and rotary wing aircraft, or in combination or hybrid aircraft, such as an aircraft with tilting rotor assemblies which allow both a fixed wing mode of flight and a rotor wing mode of flight, i.e., a tiltrotor aircraft. 
     More particularly, the present invention is directed to an improved glareshield which includes multiple portions of varying strength which allow the glareshield to fold or collapse in a controlled manner when it is struck by the head or helmet of a crew member during a crash, thus reducing the deceleration force experienced by the head, and thereby enhancing safety and increasing survivability. 
     Still more particularly, the present invention is directed to an improved glareshield which includes an array of high strength segments oriented within the glareshield in a predetermined pattern which defines a plurality of portions of the glareshield which, in effect, act as “hinges” to allow the controlled folding or collapsing of the glareshield when struck. This folding process absorbs kinetic energy from the occupant&#39;s head and helmet at controlled levels below the injury threshold. 
     During impact, the improved glareshield of the present invention folds down over the instrument panel, which is underneath it, allowing the energy-absorbing padded top surface of the glareshield to protect the head from a high force impact with the hard portion of the instrument panel. 
     In accordance with the preferred embodiment of the present invention, the glareshield includes a layer of foam pad which has a nonlinear stiffness and a low coefficient of restitution to maximize the amount of energy absorbed by the head. 
     The improved glareshield of the present invention functions somewhat like a pre-deployed air bag to protect the from head injury during a crash. However, it is entirely a passive device, which does not need to be instantaneously deployed at the moment of impact. It is a relatively low-cost and fail-safe means for reducing head injury that requires no moving parts and no deployment mechanisms. 
     The above as well as additional objectives, features, and advantages will become apparent in the following description. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     The novel features believed characteristic of the invention are set forth in the appended claims. The invention itself however, as well as a preferred mode of use, further objectives, and advantages thereof, will best be understood by reference to the following detailed description of the preferred embodiment when read in conjunction with the accompanying drawings, wherein: 
     FIG. 1 is a fragmentary pictorial representation of one preferred embodiment of the improved glareshield of the present invention in a top or plan view; 
     FIG. 2 is a cross-sectional view of the improved glareshield of FIG. 1 as seen along section line III—III; 
     FIG. 3 is a view of the improved glareshield of the present invention in an exemplary installed position; and 
     FIG. 4 is a view of the glareshield of the present invention from III—III in FIG.  3 . 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     FIG. 1 is a fragmentary view of the preferred, but not exclusive, embodiment of the improved glareshield of the present invention. The view is “fragmentary” since a number of internal components, which would not ordinarily be visible, are depicted. Glareshield  11  is preferably symmetrical about center line  13 , defining a left side portion  15  and a right side portion  17 . A plurality of generally longitudinal stiffening beads  19  and lateral stiffening beads  21  are depicted in this view. These components would not be visible during use. They are depicted in this view to define the orientation of the longitudinal and lateral stiffening beads  19 ,  21  relative to the glareshield  11 . The stiffening beads  19 ,  21  represent regions having a greater bending strength in one axis and weaker in the transverse axis relative to the remaining and surrounding portions of the glareshield  11 . 
     The stiffening beads  19 ,  21  and the weaker surrounding material which forms the glareshield  11  function as multiple and alternating portions of varying strength which allow the glareshield  11  to fold or collapse in a controlled manner when it is struck by the head of a crew member during a crash, thus reducing below injury levels the deceleration force experienced by the head, and thereby enhancing safety and increasing survivability. 
     Characterized another way, glareshield  11  includes an array of high strength segments oriented within the glareshield  11  in a predetermined pattern which defines a plurality of portions of the glareshield  11  which, in effect, act as “hinges” to allow the controlled folding or collapsing of the glareshield when struck. During impact, the improved glareshield of the present invention folds down over the instrument panel (not visible in this view) which is underneath it allowing the padded top surface of the instrument panel to protect the head from a high force impact with the hard portion of the instrument panel. 
     Referring once again to FIG. 1, a number of longitudinal stiffening beads  19  are present within glareshield assembly  11  including stiffening beads  23 ,  25 ,  27 ,  29 ,  31 ,  33 ,  35 ,  37 , and  39 . Additionally, there are a number of individual stiffening beads  21  which are oriented generally orthogonal to the longitudinal stiffening beads  19 . In the view of FIG. 1, lateral stiffening beads  41 ,  43 , and  45  are depicted. Together the lateral and longitudinal stiffening beads  19 ,  21  define a sort of skeletal structure within glareshield assembly  11  which provide controlled strength in particular portions of glareshield assembly  11 . A number of fasteners  47  are utilized to secure glareshield assembly  11  to instrument panel  49 . 
     FIG. 2 depicts a longitudinal section view as taken through glareshield assembly  11  of FIG.  1 . As is shown, the glareshield assembly  11  is composed of a number of overlapping materials which are secured and bonded together. The top layer is a cover  51  which is preferably a layer of artificial leather material. Underneath cover  51 , there are two layers of energy-absorbing foam padding  53 ,  55 . Adhesive layers  57 ,  59 ,  61  are applied between the cover  51  and foam padding  53 ,  55  to secure these layered components together. In the preferred embodiment, glareshield assembly  11  further includes a stiffening rod  65  that provides additional stiffness primarily to maintain the shape of the glareshield. This stiffening rod is covered by the foam padding layer  55  and provides a small degree of assistance in absorbing kinetic energy from the head during deformation. The lateral stiffening beads  41 ,  43 ,  45  are embedded in and surrounded by the foam padding layer  55 . They are spaced apart in a predetermined geometric configuration within foam padding  55  and define effective hinge lines within glareshield assembly  11 . The view of FIG. 2 also depicts fastener  47  securing glareshield assembly  11  to instrument panel  63 . 
     FIG. 3 is a pictorial representation of the installation of glareshield  11  of the present invention in a helicopter or tiltrotor cockpit mounted above instrument panel  63  in a position which is convenient to the pilot and other crew members. 
     FIG. 4 is a view of the glareshield of the present invention from III—III in FIG.  3 . Some typical dimensions are shown. 
     In the preferred embodiment of the present invention, the stiffening beads are formed from polycarbonate plastic material sold under the trade name “LEXAN” which is manufactured by GE Plastics. 
     Although the invention has been described with reference to a particular embodiment, this description is not meant to be construed in a limiting sense. Various modifications of the disclosed embodiments as well as alternative embodiments of the invention will become apparent to persons skilled in the art upon reference to the description of the invention. It is therefore contemplated that the appended claims will cover any such modifications or embodiments that fall within the scope of the invention.

Technology Classification (CPC): 1