Abstract:
A communications system includes a single stage, turbocharged, piston-powered aircraft that is positioned to fly in the lower stratosphere (41,000 ft.). A first link for the system is established between the aircraft and a subscriber on the ground, and a second link is established between the aircraft and a telecommunications base station. With the aircraft in position, communications between the subscriber and another party is then established over the first and second links, and through the base station.

Description:
FIELD OF THE INVENTION  
         [0001]    The present invention pertains generally to communications systems. More particularly, the present invention pertains to telecommunications systems that employ an airborne communications link. The present invention is particularly, but not exclusively, useful as an airborne communications link that is economically established by using a single stage, turbocharged, piston-powered aircraft which is flown in the lower stratosphere at an altitude of approximately forty-one thousand feet.  
         BACKGROUND OF THE INVENTION  
         [0002]    In addition to speed, reliability and sustainability, commercial communications systems need to be economical. Apart from the other considerations, the economics of installing a communications system is often the determinative factor in deciding whether to proceed. A consequence of this is that many areas of the world today, do not have an effective communications infrastructure. In particular, this is so in remote, isolated or hard-to-access locations, where terrestrial solutions are cost prohibitive.  
           [0003]    For an airborne solution, rather than a terrestrial solution, the economics involved rely primarily on the airborne platform (vehicle) that is used to carry the communications payload aloft. Many potential airborne platforms exist, and have been considered for this purpose. For example, U.S. Pat. No. 6,061,562 which issued to Martin et al. for an invention entitled “Wireless Communication Using an Airborne Switching Node” discloses a communication system that includes an airborne communications link. Typical of presently proposed systems, however, the disclosure in this U.S. patent considers stratospheric flight by aircraft well above the tropopause (e.g. between 52,000 and 60,000 feet). Vehicles (aircraft) that can effectively operate at such altitudes are not necessarily economical for implementing communications systems that employ airborne relay techniques. As noted by commentators, “. . . it remains to be demonstrated that placing a platform at stratospheric altitude and “fixing” it reliably above the coverage area is possible, and that it can be done in a cost-effective, safe, and sustained manner.” (see Djuknic et al. “Establishing Wireless Communications Services via High-Altitude Aeronautical Platforms: A Concept Whose Time Has Come?” IEEE Communications Magazine, September 1997)  
           [0004]    As indicated above, the airborne platform (vehicle, aircraft) that is used for an airborne communications link will profoundly affect the commercial economics of the overall system. Ideally, such a platform can fly, or be positioned, above normal airline traffic routes. Further, such a platform should be capable of avoiding most weather. These requirements effectively dictate that the platform be capable of operation above the tropopause (i.e. in the stratosphere). Further, these requirements also effectively preclude the use of tethered platforms. Consequently, conventional aircraft that only operate economically below the tropopause are effectively precluded from consideration. On the other hand, vehicles that are specifically designed for stratospheric flight are most economically operated only when flown well above the tropopause. A consequence here is the creation of a gap in the lower stratosphere (i.e. around 40,000 feet) where sustained, economical flight operations have not been thoroughly considered in the context of a communications system.  
           [0005]    The fact that an airborne platform does not need speed to be effectively used in a communications system is a consideration. The fact the platform does not need a high payload miles capability is also a consideration. What is really important, however, is that the airborne platform be capable of on-station endurance with the minimum fuel consumption required for safe flight operations. On balance, in comparison with turbine-powered aircraft, piston-powered aircraft are better suited for slow-flight operations. For high altitude operations, however, piston-powered aircraft require turbocharging. Heretofore, conventional thinking has been that such turbocharging requires use of the more expensive multi-stage turbochargers.  
           [0006]    In light of the above, it is an object of the present invention to provide a system and method for establishing a link for a communications system which economically uses a single stage, turbocharged, piston-powered aircraft flying in the lower stratosphere. Another object of the present invention is to provide a system and method for establishing a link for a communications system which services remote, isolated, hard-to-access areas where there is low subscriber density. Still another object of the present invention is to provide a system and method for establishing a link for a communication system that is easy to implement, simple to use, and comparatively cost effective.  
         SUMMARY OF THE INVENTION  
         [0007]    In accordance with the present invention, an economical communications system for transferring signals between separated ground-based stations, in a substantially rural environment, uses an airborne platform that is positioned in the lower stratosphere. Importantly, this airborne platform is a single stage, turbocharged, piston-powered aircraft. The aircraft may be either manned, or un-manned, and it may be either a single engine or a multi-engine aircraft. The economical aspects of the present invention are realized by using an airborne platform that is reliable in sustained operations above airline traffic and above most weather. For the present invention the preferred flight altitude is approximately forty-one thousand feet.  
           [0008]    On-board the aircraft, the communications system payload includes at least one spot beam antenna. There may, of course, be more than one such antenna and, preferably, around six spot beam antennas will be used. A first link in the communications system is established between a subscriber on the ground and one of the spot beam antennas on the aircraft. Specifically, this first link is used for transferring signals between a first ground-based station (i.e. a subscriber) and the airborne platform. As envisioned for the present invention, this first link will use a carrier wave in a first frequency range that, preferably, includes radio frequencies (RF) between 1,850 MHz and 1,910 MHz.  
           [0009]    The airborne payload also includes an airborne microwave antenna that is used for establishing a second link in the communications system. For this second link, the airborne microwave antenna is mounted on the airborne platform to transfer signals between the platform and a second ground-based station (i.e. a base station). As envisioned for the present invention, this second link will use a carrier wave in a second frequency range that, preferably, includes microwave (MW) frequencies between 3.7 GHz and 18 GHz.  
           [0010]    An important component of the present invention is a communications relay unit that is carried on-board the aircraft. Specifically, the relay unit accomplishes two general tasks. For one, the relay unit is used for converting the signal carrier frequencies between the first frequency range and the second frequency range. For another, it is used for transferring the signal between the spot beam antenna in the first link and the airborne antenna in the second link. To do this transfer, the relay unit includes a stage for off-setting frequencies on the second link. Specifically, this is done to match each spot beam antenna on the aircraft with a transceiver at a base station on the ground.  
           [0011]    At a fixed location on the ground, such as at the airport where the aircraft is based, a base station is established for the communications system of the present invention. This base station includes: an interface with a public switched telephone network (PSTN), or with some other similar type network, that connects with various parties on the ground; a base antenna for establishing microwave (MW) communications with the aircraft, and a plurality of transceivers that interconnect the PSTN, or other network, with the base antenna. The base station may also include a stage for off-setting frequencies to match each transceiver at the base station with a spot beam antenna on the aircraft.  
           [0012]    In operation, a subscriber in a remote area (i.e. rural environment) directly communicates signals between his/her ground station and the airborne aircraft. This is done using a radio frequency (RF) carrier (i.e. first link). During this communication, a control channel in the aircraft&#39;s relay unit can be used for varying the signals to compensate for movement of the platform. In the aircraft the signals are then appropriately converted in frequency, and transferred between a spot beam antenna (first link) and a microwave antenna (second link) for transmissions to/from the base station. At the base station, the signals are processed by signal processing equipment, such as used in a conventional wireless cellular network. 
       
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0013]    The novel features of this invention, as well as the invention itself, both as to its structure and its operation, will be best understood from the accompanying drawings, taken in conjunction with the accompanying description, in which similar reference characters refer to similar parts, and in which:  
         [0014]    [0014]FIG. 1 is a schematic view of a communications system showing a deployment of the various components of the present invention; and  
         [0015]    [0015]FIG. 2 is a schematic view of the electronic components of the present invention that are carried aloft in the payload of the airborne platform that is used for the present invention and the electronic components that are used at a base station. 
     
    
     DESCRIPTION OF THE PREFERRED EMBODIMENTS  
       [0016]    Referring initially to FIG. 1 a communications system incorporating a stratospheric airborne link for transferring signals between ground-based stations is shown and generally designated  10 . As shown, the system  10  includes at least one aerial vehicle  12 , and possibly more, in operation at any one time. The aerial vehicles  12  and  12 ′ shown in FIG. 1 are only exemplary. Regardless how many aerial vehicles  12  are in operation for the system  10 , each aerial vehicle  12  is used to establish respective communications links between individual subscribers  14  and a central ground station  16  (subscribers  14   a - c  are exemplary).  
         [0017]    An important aspect of the system  10  is the aerial vehicle  12  that is used In detail, the aerial vehicle  12  is intended to be a piston-powered aircraft having a single stage, turbocharged engine, or engines. Further, the turbocharger on the engine(s) of aerial vehicle  12  preferably operates with a compression ratio of approximately 6.0:1. Flight envelope calculations indicate that an aerial vehicle  12  with this configuration is capable of loitering in the lower stratosphere (e.g. at around forty-one thousand: 41,000 feet) for extended periods of time. As intended for the present invention, aerial vehicle  12  must be capable of sustained flight above commercial traffic, and above most weather systems. It is envisioned for the system  10  that the aerial vehicle  12  may either be manned, or unmanned. In the case of a manned aircraft, the system  10  will include a demand oxygen system on-board the aerial vehicle  12 .  
         [0018]    In FIG. 2 it is shown that the aerial vehicle  12  includes in its payload, a plurality of spot beam antennas  18  (antennas  18   a  and  18   b  are exemplary) as well as an airborne antenna  20 . As shown in FIG. 1, the plurality of antennas  18  that are on-board the aerial vehicle  12  are intended to collectively service a respective plurality of subscribers  14 . Specifically, these subscribers  14  will be located within a determinable footprint  22  (area) below the orbit of the aerial vehicle  12 . As indicated in FIG. 1, the footprint  22  will be generally circular, and will have a radius that is in a range between about fifty miles to one hundred and twenty miles (i.e. 50-120 miles). More specifically, and using the subscriber  14  shown in FIG. 1 as an example, a communications link  24  can be established between the spot beam antenna  18  on-board the aerial vehicle  12  and the subscriber  14  on the ground. Communications back to the ground station  16  is then established over a communication link  26  that goes between the antenna  20  on-board the aerial vehicle  12  and an antenna  28  at the ground station  16 .  
         [0019]    Although many different communications schemes can be used for the system  10 , it is preferred that the link  24  between a subscriber  14  and the aerial vehicle  12  use a frequency range that includes radio (RF) frequencies between 1,850 MHz and 1,910 MHz. On the other hand, it is also preferred that the link  26  between the aerial vehicle  12  and the ground station  16  use a frequency range that includes microwave (MW) frequencies between 3.7 GHz and 18 GHz. The change from one frequency range to another is accomplished in the aerial vehicle  12  by a relay/conversion unit  30 , and the change back to the original frequency range is accomplished at the ground station  16  by another relay/conversion unit  32 . Then, as shown, communication signals can be passed from the ground station  16  to a wireless switch  34  and on to a public switched telephone network (PSTN)  36 , or to some similar type communications network. Alternatively, the communication can be passed from the ground station  16  back to another aerial vehicle  12  (e.g. aerial vehicle  12 ′) and from there to another subscriber  14  (e.g. subscriber  14   c ).  
         [0020]    In detail, a communication connection between a subscriber  14  on the ground, from inside the footprint  22 , and the ground station  16  (most likely outside the footprint  22 ), is best discussed with reference to FIG. 2. To begin, the subscriber  14  connects with a spot beam antenna  18  on the aerial vehicle  12  over the communications link  24 . The communication signal is then sent through a low noise amplifier (LNA)  38  to the relay/conversion unit  30  onboard the aerial vehicle  12 . There it is converted from a radio frequency (RF) signal into an intermediate frequency (IF) signal. The communication signal is then converted from the IF signal into a micro-wave (MW) signal and this MW signal is then sent from the relay/conversion unit  30  through a multi-carrier linear power amplifier (MCLPA)  40 . After leaving the MCLPA  40 , the MW signal is transmitted from the airborne antenna  20 , via the communications link  26 , to the antenna  28  at the ground station  16 . The communication signal is then passed through LNA  42  and to the relay conversion unit  32  where it is appropriately converted for further transmission through the wireless switch  34  to the PSTN  36 , or some similar type network.  
         [0021]    For communications from the ground station  16  to a subscriber  14 , a communications signal is first sent to the ground station  16 . At the ground station  16 , it is passed through the relay/conversion unit  32 , and through the MCLPA  44  for transmission as a MW signal from the antenna  28  onto communications link  26 . This communications signal is then received by the airborne antenna  20 , passed through the LNA  46 ; and converted into an IF signal. As an IF signal, the signal is sent through the relay/conversion unit  30  for conversion into an RF signal. This RF signal is then passed through the MCLPA  48  and transmitted by the spot beam antenna  18  via communications link  24  to the subscriber  14  on the ground.  
         [0022]    While the particular Communications System Using High Altitude Relay Platforms as herein shown and disclosed in detail is fully capable of obtaining the objects and providing the advantages herein before stated, it is to be understood that it is merely illustrative of the presently preferred embodiments of the invention and that no limitations are intended to the details of construction or design herein shown other than as described in the appended claims.