Aircraft Passenger Television System

This invention relates generally to on-board aircraft entertainment systems and the like. More specifically, this invention relates to an improved television system permitting individualized television program selection and viewing by aircraft passengers.

On-board video systems are known in the art for entertainment of aircraft passengers. Such video systems have become popular in recent years for providing movies and other video programming for entertaining passengers during the course of an aircraft flight. The inclusion of video entertainment during the flight has constituted an effective airline marketing tool and provides the further benefits of reducing passenger fatigue and maintaining many passengers in their seats during a flight.

In the past, video entertainment systems on aircraft have utilized a movie screen or television receiver of relatively large size installed within the aircraft cabin in a centralized location for simultaneous viewing by many aircraft passengers. In this regard, the use of on-board video entertainment systems has been restricted to relatively large aircraft having sufficient cabin volume to accommodate substantially unobstructed viewing of the video programming by many passengers. However, this arrangement does not provide alternative video entertainment for those passengers who do not wish to watch the video program selected by airline personnel. Moreover, no satisfactory video entertainment system has been provided for use with smaller aircraft of the type used for most relatively short range commercial flights and which do not have sufficient cabin volume to accommodate a traditional large movie screen or television receiver.

There exists, therefore, a significant need for an improved on-board video entertainment system adapted for use with aircraft of substantially any size and wherein each passenger is provided with alternative program selection capability. The present invention fulfills these needs and provides further related advantages.

In accordance with the invention, an improved video system is provided for on-baord entertainment of airline passengers. The improved system includes a plurality of compact television receiver modules mounted for individual viewing by aircraft passengers. The television modules are adapted to receive on different channels a plurality of different video programs, with each television module including channel selection means operable by the individual airline passenger.

In one preferred form of the invention, the television modules each include a compact televison receiver particularly such as a compact color television having a liquid crystal display screen and relatively low power requirements. The television receiver is installed within a lightweight chassis to form the module adapted for rapid and removable nested connection within a matingly shaped mounting bracket installed in a rearwardly opening position in front of an airline passenger, for example, by installation of the mounting bracket within an airline passenger seat immediately in front of the individual passenger. The television screen is angularly oriented within the chassis at a selected tilt angle which is generally complementary to the average reclined angle of the passenger seat thereby orienting the screen at or near a substantially vertical attitude for passenger viewing.

Each television module includes one or more plug-in fittings for rapid engagement with connector fittings on the mounting bracket to couple the receiver to a power source and multiple video program signals broadcast on different channels. When seated within the mounting bracket, the module is adapted to support one or more cushion members to reduce risk of passenger injury upon impact therewith and further to blend with conventional seat fabric in an attractive manner. The cushion members and seat fabric cooperatively define a central opening exposing the recessed television scree and adjacent controls, such as channel selection, volume and/or brightness controls. An audio headset including lightweight earphones is provided with each television module for plug-in connection thereto to provide individualized audio signals to each passenger.

A central broadcast station on the aircraft is coupled by one or more appropriate cables to each of the plurality of television modules. This broadcast station provides an appropriate power source for each module and further includes means for supplying a plurality of different program signals on different channels. These program signals may be obtained by playback of prerecorded video cassettes or the like and/or locally received programs broadcast in the geographical vicinity of the aircraft. Each passenger may optionally select one of these multiple programs for individualized viewing substantially without disturbing other passengers.

Further advantages and features of the invention will become more apparent from the following detailed description, taken in conjunction with the accompanying drawings, which illustrate, by way of example, the principles of the invention.

The accompanying drawings illustrate the invention. In such drawings:

FIG. 1 is a fragmented top plan view illustrating, in somewhat schematic form, an improved aircraft passenger television system embodying the novel features of the invention;

FIG. 2 is a rear perspective view illustrating a row of aircraft passenger seats each including a television receiver module according to the invention;

FIG. 3 is an enlarged fragmented rear elevation view of the television module installed within a passenger seat;

FIG. 4 is an enlarged, exploded, fragmented vertical sectional view taken generally on the line 4--4 of FIG. 3;

FIG. 5 is an exploded fragmented perspective view illustrating mounting of the television module within a passenger seat;

FIG. 6 is an enlarged fragmented horizontal sectional view taken generally on the line 6--6 of FIG. 3;

FIG. 7 is an enlarged fragmented vertical sectioanl view corresponding with the encircled region 7 of FIG. 4;

FIG. 8 is a schematic diagram illustrating one preferred arrangement for coupling a plurality of the television modules with a central broadcast station; and

FIG. 9 is a schematic diagram illustrating one of the television modules and operation thereof for individual channel selection by each passenger.

As shown in the exemplary drawings, an on-board television system referred to generally by the reference numeral 10 is installed within an aircraft 12 to provide individualized video entertainment for a plurality of aircraft passengers. As shown in FIGS. 1 and 2, the television system 10 includes a central broadcast station 14 on the aircraft 12 and adapted to supply multiple video program signals on different channels to each of a plurality of compact television receiver modules 16 mounted for individual selection and viewing by the aircraft passengers.

The on-board television system 10 of the present invention provides each aircraft passenger with a broad range of video program options which can be selected and controlled by the individual passenger. The system 10 thus improved significantly upon prior art aircraft video systems wherein the video entertainment is restricted to a single program or movie which normally does not meet the taste preferences and is therefor enot observed by many passengers. Moreover, by providing the individual compact television modules 16, the present invention avoids the need for a large movie or television screen at a centralized location within an aircraft cabin and accompanying umimpaired sight lines for passenger viewing, wherein these requirements have limited previous video systems to relatively large aircraft. Instead, the compact television modules 16 are located at each passenger seat location for close range, individualized viewing to permit use of the system on passenger-carrying aircraft of virtually any size.

As shown generally in FIG. 1, the improved television system 10 includes the central broadcast station 14 located at a convenient on-board position for access by aircraft personnel. The broadcast station 14 includes means for supplying a plurality of different video program signals on different channels to one or moer cables 18 which carry the signals to each passenger seat location, for example, by branching off at each row 20 of seats. As shown in FIG. 2, each seat row 20 commonly includes a plurality of side-by side passenger seats 22, with each seat 22 having one of the compact television modules 16 mounted therein in a rearwardly facing position for close-range viewing by the passenger seated in the seat and row immediately therebehind. For passengers seated in a row 20 at the front of the aircraft (FIG. 1), additional cable branches can be provided for connection to additional television modules (not shown) mounted within a bulkhead wall 24 at the front of a passenger cabin.

In one preferred form, each television module 16 is sized and shaped for rapid, removable installation into a respective one of the aircraft passenger seats 22 in an otherwise out-of-the-way position, such as within the headrest portion of the seat, as shown in FIG. 2. Each module 16 includes a compact television receiver 25 designed for relatively low power consumption and for signal requirements compatible with aircraft use and without interfering with required aircraft radio and navigational functions. A preferred television receiver comprises a receiver having a color liquid crystal display (LCD) screen 26 of generally rectangular shape with a diagonal screen measurement of about two to four inches, and most preferably about two and one-half inches.

As shown in FIGS. 2-7, the television receiver 25 is securely mounted within a relatively lightweight housing or chassis 28 adapted for rapid removable nested attachment into a rearwardly open mounting bracket 30 within the passenger seat 22. More particularly, the seat 22 includes an interanl frame 32 covered by appropriate cushion and outer fabric materials to comfortably support a passenger without significant unpadded protrusions of the like which could result in passenger injury upon impact therewith. The upper rear side of the seat headrest portion is normally open to define a chamber for reception of the mounting bracket 30 which is securely fastened to the seat frame 32 by rivets 34 or other suitable fastening means. The mounting bracket in turn defines a rearwardly open can for nested reception of one of the television modules 16.

Each television module 16 including the chassis 28 is sized and shaped for smooth and easy sliding reception into the rearwardly open mounting bracket 30, as shown in FIG. 4. Prior to such reception, however, one or more plug-in fittings 36 on the television receiver 25 are mated with appropriate connector fittings 38 within the mounting bracket to couple the receiver to a power source and the signal-carrying cable 18 (FIG. 1) Fasteners 40 are provided on the chassis 28 for locking with sockets 42 on the mounting bracket 30 to lock the module in place. These fasteners may take different forms, although quick-connect fasteners are preferred, such as the fastener marketed under the name CAMLOC by Rexnord Specialty Fastener Division, Hasbruck Heights, N.J.

A relatively thick foam cushion or pad 44 is mounted over the rear face of the modular chassis 28 to provide a resilient structure protecting against passenger injury in the event of impact with the module. As shown best in FIGS. 5 and 7, this foam pad 44 includes a central opening 45 sized to expose the compact receiver 25 including the screen 26 and a closely adjacent control panel 46 which will be described in more detail. The foam pad can be mounted onto the chassis 28 in any suitable manner, such as by use of the illustrative pressure-sensitive adhesive 47 on the side of the pad facing the chassis. Importantly, the pad 44 has sufficient thickness to recess the receiver 25 substantially from the rear plane of the seat which generally coincides with the rear plane of the pad to further minimize risk of injury-causing impact with a passenger.

For optimum appearance, the central opening 45 of the foam pad is adapted for attachment with overlying seat fabric 48. As shown in FIGS. 5 and 7, a flap of the seat fabric 48 is draped over the television module 16 and the foam pad 44, with a rectangular fabric opening 49 aligned with the pad opening 45 to expose the television screen 26 and adjacent control panel 46. The fabric 48 includes short cut slits 50 at the corners of the opening 49 to define narrow fabric flaps to fold inwardly over the margins of the central pad opening 45. Fastening means such as interlocking Velcro strips 51 and 52 on the fabric 48 and the pad 44 securely attach the seat fabric 48 onto the pad.

A bezel 54 of relatively rigid yet somewhat resilient foam is also provided and fits closely through the fabric opening 49 and the pad opening 45. This bezel 54 locks onto the rear side of the module in a position bordering the screen 26 and adjacent control panel 46. Appropriate fastening means such as additional Velcro strips 55 and 56 on the bezel 54 and module 16 securely lock the bezel in place for providing a stury support bordering the fabric and pad openings.

When installed into the passenger seat 22, the television module 16 advantageously supports the television screen 26 at a tilt angle relative to the rear plane of the seat. More particularly, as shown best in FIG. 4, the screen 26 is tilted upwardly and forwardly from its lowermost margin at an angle of about fifteen degrees. With this orientation, the screen 26 is tilted to complement an average range of seatback reclining to maintain the scren sufficiently in a vertical attitude for easy passenger viewing. That is, throughout a normal range of seatback reclining, the viewing screen 26 of the television receiver will be tilted slightly forwardly in the upright seatback position to slightly rearwardly in a fully reclined seatback position, with a nearly vertical attitude at an average partially reclined seatback position.

In operation, a plurality of different video programs are sent by the broadcast station 14 over the cable 18 to each passenger seat 22, with six different programs being referred to by the letters A through F in the schematic diagram of FIG. 8. At each passenger seat, the program signals are coupled to the receiver 25 of the television module. As depicted in FIG. 9, each receiver 25 includes a tuner 58 for coupling a selected one of the program signals for display on the screen 26, in accordance with passenger-activated depression of one of a plurality of channel selector pushbuttons 60 exposed on the control panel 46. Accordingly, each passenger can individually select one of the programs for viewing, or alternate between programs, as desired.

Additional passenger controls for enhanced enjoyment of the video programming are also provided on the control panel 46. For example, a rotatable volume control dial 62 is provided for controlling the volume of an audio signal. This audio signal is supplied via an audio jack 64 on the control panel for plug-in reception of a standard headset 66 (FIG. 2) including earphones 68 for private listening enjoyment without disturbing nearby passengers. A separate control dial 70 for brightness control of the picture displayed on the screen 26 may also be provided, as well as an on-off switch 72.

The television system 10 of the present invention thus provides a highly versatile video entertainment system for individualized passenger selection and viewing. The system thus provides an airline with a significant marketing tool by virtue of the availability of multiple programs. Moreover, by providing more passengers with video entertainment, a higher proportion of passengers on a flight will tend to remain seated for longer periods of time, resulting in greater overall safety. Still further, the system is adapted for use with virtually any size of aircraft and can thus be used on relatively small aircraft on whcih video entertainment has not heretofore been available.

A wide variety of modifications to the system described herein will be apparent to those skilled in the art. For example, the broadcast station 14 can be adapted to supply multiple programs by playback of multiple prerecorded cassettes. Alternatively, the station 14 can be designed to supply multiple programs of local broadcast origin within the geographical vicinity of the aircraft, or, if desired, a combination of prerecorded and local programming. Still further, the system is readily adapted to pilot or crew interruption for announcements and the like, as required during the course of a flight. Moreover, the modules can be adapted to receive power from a separate power supply 71, as viewed in FIG. 9, or they may receiver power directly from the central broadcast station 14.

Accordingly, no limitation on the invention is intended by way of the description herein, except as set forth in the appended claims.