WO1998007623A1

WO1998007623A1 - In-flight aircraft refuelling system

Info

Publication number: WO1998007623A1
Application number: PCT/RU1997/000263
Authority: WO
Inventors: Alexandr Serafimovich Karavaev; Anatoly Nikolaevich Kvochur; Dmitry Viktorovich Shulepov
Original assignee: Gosudarstvennoe Unitarnoe Predpriyatie 'pilotazhno-Issledovatelsky Tsentr'
Priority date: 1996-08-19
Filing date: 1997-08-18
Publication date: 1998-02-26
Also published as: RU2104229C1

Abstract

The present invention pertains to the field of aeronautics and more precisely to equipment for the in-flight refuelling of a an aircraft. This invention relates to an in-flight aircraft refuelling system that performs the autonomous search and guidance towards the meeting point of the tanker aeroplane and the aircraft to be refuelled in the absence of any ground navigation system. This system further ensures reliability and security when docking and refuelling in any weather conditions. The refuelling system of the present invention comprises a refuelling boom fitted with a cone and mounted on the tanker aeroplane as well as a refuelling boom onboard the aircraft to be refuelled. This system also uses satellite navigation system (SNS) receivers provided with SNS antennas, UHF radio stations, an additional SNS antenna mounted on the cone as well as a switch.

Description

SIσΤΕΜΑ ЗΑПΡΑΒΚИ СΑΜΟЛΕΤΑ τшжвом in ΠΟЛΒ Έ

Izοbρβτθniθ οτnοοiτοya K Aviation and bοlβθ κοnκρθτnο, K οbορudοvaniyu, οbθsπechivayuschθmu zaπρavκu τοπlivοm samοleτοv in ΠΟLΘΤΘ and ΜΟZHΘΤ byτ iοποlzοvanο in SIΟΤΘΜΘ οamοlθτοv-τanκθροv and dοzaπρavlyaθmvχ ΟΘΜΟDΘΤΟΒ the purpose ΠΟΒYSHΘΗIYA eφφθκτivnοοτi iχ

PRIJIA.

Ievβsτnο usτροyοτvο zaπρavκi in vοzduχθ for Lθτaτelnyχ aππaρaτοv φiρmn Μθβvegastϊ-yι-Βοϊkονg-vοnιya αshn (sm.za- yavκu Φρanπii & κl 2,569,652. Β64 1) 39/00 1986) Usτροyοτvο sοdθρ- zhiτ usτanοvlennuyu on οamοlθτe-τanκβρθ 8aπρavσchnuyu with shτangu οπβ- ρeniθm, vyποlnennuyu as ΤΘYAΘSΚΟΠYCHEΟΚIΧ ρazdvigaθmyχ τρub, πulτ uπρavlθniya zaπρavοchnοy shτangοy, οisτθmu daτchiκοv and ΒB- CHIΟLIΤΘLΗΟΘ usτροyοτvο, οπρθdθlyayuschθθ οπτimalnyθ πaρamθτρi and ρθguliρuyuschee ΠΟLΟZHΘΗIΘ shτangi πuτem ποdachi κοmand isποlniτel- nym mθχanizmam.

On the other hand, LOOKING FOR THE ELECTROMETER, inviting you to observe the process of parking. Οπθρаτορ у can be controlled by the frustrating - with the bar. Τaκοθ usτροysτvο, οdnaκο, n§ ΜΟZHΘΤ οbθsπechiτ HA DΘZHΗΟΘ ΟΟΘDIΗΘΗIΘ with πρiθmnοy shτangοy zaπρavlyaθmοgο οamοleτa and bθzοπaοnοsτ zaπρavκi, οοοbβnnο πρi πlοχi ποgοdnn ^x ^x ^x uοlοviya.

WELCOME THERE, THERE WOULD BE OTHERWISE TO OTHERWISE DEPARTURE TO BE CONSIDERED TO BE CONSIDERED TO BE CONSIDERABLE

IZZΤΗΟ far θ θ ви ΟΤΘΜ θ θ θ ΟΤΘΜ ΟΤΘΜ ΟΤΘΜ ΟΤΘΜ ΟΤΘΜ ΟΤΘΜ ΟΤΘΜ & & & & & & & & & & & & & & 34 & & & & &. Β64 D39 / 00, 1986). LONG-TERMINAL SUPPLY FOR USE ON THE INDIVIDUAL INFORMATION THAT IS USED BY A RADIATOR

LISΤ ΒЗΑΜΕΗ ЪΤΟΤΟΤΟΤΟ (ПΡΑΒИЛΟ 2β) \ νθ 98/07623 ΡСΤ / ΙШ97 / 00263

2

LΘΗII OF OXY AND ^χ Aircraft. In addition, there is a device for the purpose of repressing free and easy-to-use information for the pilot of a fired aircraft.

However, such a system also does not provide a reliable connection of a fixed aircraft. Otherwise, there are no devices to make sure that you save money on the charge of the flight on the plane.

The United States Patent ^& 5ΙЗΙ438 ΜΚИ Β64 Д39 / 00 "Means and facilities for refueling an uninhabited aircraft in the gollet" is known.

The device is equipped with a pilot-operated retractable charging hose, equipped with a spare hose, and the hose is equipped with a plug-in adapter. Κροme τοgο, usτροysτvο snabzhenο πeρedagoschim sρedsτvοm, usτanοvlennym on τanκeρe and πρieshym sρedsτvοm, INSTALLS τanοvlθnnym on besπilοτnοm samοleτe, πρinimayuιschsh signals οτ πeρedayuschegο sρedsτva and uπρavlyagoschgol usτροysτvοm uπρavleniya shlan- gοm. In this case, the primary and secondary components are made in the form of self-excitation induction coils installed on the cone and the power supply.

Such a device does not interfere with the exit of aircraft to the point of collision and rapprochement. Κροme τοgο, sisτema sοzdaeτ bοl- Chiyah πsiχο-φizichesκie nagρuzκi on πilοτa τanκeρa, due οτsuτ- sτviya at negο τοchnyχ κοορdinaτ ο vzashlnοm ποlοzhenii κοnusa and shτangi, deysτvueτ τοlκο πρi malοm ρassτοyanii therebetween chτο snizhaeτ nadezhnοsτ and bezοπasnοsτ zaπρavκi.

Izvesτna "^ ϊzhροvοlnοvaya sisτema for vsτρechi and zaπρavκi samοleτοv in vοzduχe" - πaτenτ SSHΑ kyo 4763861 κl. Β64 D39 / 00, 1987

The system is equipped with a quick switch, installed on an airplane-tank, which ensures the transmission of signals in case of a failure ( ₂₆ ) ΡСΙ7ΙШ97 / 00263

3 in the rear at a distance of up to 20 miles. The drawbacks of this system are:

- sisτema not οbesπechivaeτ zsτρechu samοleτοz πρi increasing distance iχ dρug οτ dρuga on ρassτοyanii bοlee 20 miles: v πρi ποlβ- τaχ on vsτρechnyχ κuρsaχ;

- The system does not provide power for the self-loading aircraft with the information about the relative speed of convergence of the aircraft, which greatly intensifies the overload.

The systems of satellite navigation are known, which makes it easier to separate the location of aircraft, ships and other ships of a military vehicle. Such systems make it possible to solve the problems of the navigation of transport means, including in cases not connected with terrestrial accidents of the year 31/31, - 51/85; - 4Ι36Ι36, ΜΚИ-60Ι55 / 02, 1993) .0 days. well-known satellite systems are not designed to solve the problems of self-propelled aircraft in the air.

The closest analogue of the invention is “Installing fuel in the chamber” (see Patent No. 5223725 ^ ΜΚI Β64 D39 / 00, ΗΚI-Β7 (5).

The device includes mounted on an airplane-tanker, an optional hose with a cone, a device for installing a free hose and a free-ring. Κροme τοgο, IΜΘGOΤSYA daτchiκi πο- lοzheniya κοnusa and daτchiκ ΠΟLΟZHΘΗIYA zaggρavοchnοy shτangi, vyποl- nennye as isτοchniκοv svβτa, usτanοvlennyχ sοοτveτsτvennο "on κοnuse and zaπρavοchnοi shτange and vzaimοdeysτvuyuschie with πρiemnοi κameροi, usτanοvlennοy on samοleτθ-τanκeρe.

A simple camera is connected to a computer that selects a parameter _. mutual provisions of the cone and the power rod and

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26 ₎ \ νθ 98/07623 ΡСΤ / ΙШ97 / 00263

4 to the signal of the optimal position of the cone. Changing the position of the housing is possible due to the convenient installation of the exhaust hose, as well as the use of an aerodynamic hose.

Ηedοsτaτκοm πρivedennοy above sisτemy zaπρavκi yavlyaeτsya το, chτο at πilοτa zaπρavlyaemοgο samοleτa οτsuτsτvueτ τοchnaya inφορma- tion ο πaρameτρa ^χ vzaimnοgο ποlοzheniya κοnusa and zaπρavοchnοy shτan- thrust in chasτnοsτi, οb οτnοsiτelnοy sκοροsτi convergence, chτο οchen vazhnο πρi vyποlnenii eτaπa sτyκοvκi. In this case, the pilot is required to operate the aircraft for visual information. In addition, the reliability of the system is reduced in unfavorable weather conditions and in the dark.

All this leads to an increase in psychological load per year, a decrease in the speed and security of the connection and the entire process of the backup. More than that, it is obvious that to solve the problems you have _. Yes κ mesτu vsτρechi and vsτρechi samοleτοv, πilοτam samοleτa - τanκeρa and zaπρavlyaemοgο samοleτa οsτaeτsya nadeyaτsya on shτaτnye ρadiοnavigatsiοnnye sρedsτva, κοτορye not οbesπechivagoτ ποlucheniya nadezhnοy inφορmatsii ο vzaimnοm ποlοzhenii saνyuleτοv οsοbennο on ρassτοyaniyaχ szyshe 300 κm or vsτρechnyχ κuρsaχ not ρeshayuτ ποs- τavlennuyu task conditions of the absence of terrestrial and navigational disasters (for example, over the oceans, widespread arctic regions). This leads to an increase in the time of search and rapprochement of the fuel, in the case of fuel, and in the end, as a result of a decrease in the efficiency of the air supply.

Β οsnοvu dannοgο izοbρeτeniya ποlοzhena task sοzdaniya avτο- nοmnοy sisτemy dοzaπρavκi samοleτοv τοπlivοm in ποleτe, κοτορaya would οbesπechivala ποisκ and vsτρechu samοleτοv all ^χ ^χ κuρsa and ρassτοyanii least 300 κm and κροme τοgο would οbesπechivala eφφeκ- τivnοe vyποlnenie eτaπa sτyκοvκi κοnusa samοleτa -tankera so fox ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ ₂ 6) 5 shtangelnaya gratitude to the plane due to the measurement and issuance of the pilot to the gambling information of the house for a good proximity and mutual benefit.

Otherwise, the system must be able to operate in good condition;

More than that, the system must ensure that the process of delivery is completed with minimum time costs for saving fuel and increasing the efficiency of the supply. Sοglasnο izοbρeτe- NIJ, ποsτavlennaya task dοsτigaeτsya τem, chτο in sisτemu zaπρavκi samοleτa τοπlivοm in ποleτe, vκlgochagoschugo zaπρavοchny hose κοnu- sοm, usτanοvlenny on samοleτθ-τanκeρe, usτροysτvο vyπusκa-ubορκi zaπρavοchnοgο hose zaπρavοchnuyu shτangu, usτanοvlennugo on zaπ- ρavlyaθmοm samοleτe, daτchiκi ποlοzheniya κοnusa and zaggρavοchnοy shτangi, sρedsτva οπρedeleniya οτnοsiτelnοy sκοροsτi convergence and vzaimnοgο ποlοzheniya κοnusa and zaπρavοchnοy shτangi, sοdeρzhaschie You are a chisliτel, introduced πeρvy and vτοροιϊ πρiemniκi sπuτniκοvοy navi- Gatsi The external system (CCS) with CCC antennas, the first and second radio stations of the ultra-wide range (7ΚΒ) installed by the aircraft itself is installed on the aircraft. Pρi eτοm, πeρvy πρiemniκ SΗS associated with svοim vyχοdοm vχο.dοm πeρvοy ρadiοsτantsii UΚΒ and vχοdοm ποdsοedinen κ anτenne SΗS πeρvοgο πρiemniκa SΗS, vychisliτel connected πeρvym and vτορym vχοdοm with vyχοdοm vτοροgο πρiemniκa SΗS and vyχοdοm vτοροy ρadiοsτantsii UΚΒ sοοτveτsτvennο as well. exit - with an indicator installed in the cockpit of a controlled airplane.

Tselesοοbρaznο vyποlniτ sisτemu with πeρeκlgochaτelem, usτanοv- lennym on samοleτe-τanκeρe and dοποlniτelnοy anτennοy SΗS, ^A ISΤ ΒZΑΜΕΗ IZYAΤΟGΟ (PΡΑΒILΟ ₂₆₎ \ νθ 98/07623 ΡСΤ / ΙШ97 / 00263

6 mounted on the cone of the inlet hose. In addition, the output of the switch is connected to the input of the auxiliary switch of the SSC, a. The front end of the switch is connected to the CCC antenna, and the second input of the switch is connected to the optional CCC antenna.

More conveniently, the system must be connected to the output of the front panel of the controller with the input of the charger and the device for the elimination of the load

The use of the claimed fuel system in the flight allows you to:

- Ensure that the exit of the aircraft-tanker is high and that the aircraft is operated at the place of collision, in the absence of ground-based navigation systems,

- Ensure high reliability and reliability of the junction of the aircraft,

- reduce the physical load on the home.

Θ еч φ φ на на

The invention is illustrated in the drawings, in brief: Fig. - shows a block diagram of the process of acquiring an airplane-tanker; Fig. 2 - shows a block diagram of the equipment for the maintenance of a plane; FIG. 3 - shows the best block option for treating the summer itself; Fig. 4 - shows the interaction of an aircraft-tanker and a guided aircraft in the process of leaving the place of collision and rapprochement of aircraft.

LISΤΒZΑΜΕΗIZYAΤΟGΟ (ПИЛΟ ₂₆ ) \ УΟ 9/07623 ΡСΤ / ΙШ97 / 00263

INFORMATION PERMITTING THE POSSIBILITY OF THE INVENTION

The system of refueling a plane with a fuel, made in accordance with the invention, includes the equipment installed on a free-of-charge basis.

The formation of aircraft-tank I includes (see figure 1):

- Charging hose 2 with cone 3;

- HANDLING HOSE 4;

- the first receiver of the CCS (satellite navigation system 5;

- the first radio station of the UZS (ultra-long range) - 6;

- Antenna СΗС - 8;

- Antenna УΚΒ-9 of the first radio station УΚΒ-6. The delivery of the delivered aircraft 19 includes (see figure 2):

- emergency bar 12;

- the second receiver ΟΗС-ϊЗ;

- the second radio station UΚΒ-14;

- calculator-15;

- indictat-ιb;

- Antenna ССС-ι ?;

- Antenna УΚΒ-18. ϋ The SYSTEM uses known receivers intended for receiving information from the satellites, processing it, and processing ^β -communications of the process and the disintegration systems.

Radio stations are also well-known to the consumer, including the receiver, transmitter. and anτennu UΚΒ, svyazannugo with anτennym in ^χ οdοm anτennym κabelem and πρednaznacheny for πρiema and πeρetsachi tsiφρο-

LISΤ Β ^Z ΑΜΕΗ IZYAΤΟGΟ (PΡΑΒILΟ 2 ₆ ) 98/07623 ΡСΙ7ΙШ97 / 00263

8 HARVESTING THE HOSE-RELEASING HOSE INCLUDES:

- remote control;

- a slag winch with a drum, a hitching ladder, a unit for winch operation and an emergency transfer device - a lang;

- automatic control unit for the release and disposal of fuel;

- hydraulic, fuel systems;

- power supply and alarm system;

- Cone illumination system;

- a replacement hose with a cone (not shown on the drawing). Κοnus sοsτοiτ (on cheρτezhaχ not ποκazanο) of shaροvοgο naκο- nechniκa, χvοsτοviκ κοτοροgο zaκρeπlen on shτanτe, usτanοvlennοy on zaπρavοchnοm hose zemκοv zalρavοchnοi shτangi with gidροtsilind- ρami uπρavleniya, οbesπechivayuschiχ nadezhnοsτ sοedineniya zaπρgvοch- ΗΟY ιggangi dοzaπρavlyaemοgο samοleτa with κοnusοm samοleτa-τanκeρa πρi uslοvii Findings of the speed of approaching aircraft (relative to the speed of the aircraft) with a direct predetermined price (0.8-1, 5 / s). Exiting from a given tsialazona will give an advantage to the release of fuel from the satellite-tanker, Τ. Θ. for an emergency.

The first receiver of ССС 5 is connected with the antenna ССС 8, and the output is connected with the input of the radio transmitter УУ-6, connected with the antenna outlet with antenna У 9.

Ηa zaπρavlyaθmοm samοlθτe 19 vyχοdy vτοροy ρadiοsτantsii UΚΒ 14 and 13 vτοροgο πρiemniκa SΗS ποdsοedineny κο in ^χ οdam You are a chisliτelya 15 πeρvyi and vτοροz vyχοdy κοτοροgο ποdsοedineny κ κοmandnοmu vχοdu vτοροy ρadiοsτantsshι UΚΒ 14 and indiκaτορu Ιδ sοοτveτsτvennο.

The active input-output of the entrance to the radio station USS 14 is connected to

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) 9 shielded cable with antenna УУ 18, located on the external part of the free space of the company. The CCC 13 receiver terminal is connected by an antenna cable with the CCC 17 antenna, located on the external circuitry of the vicinity. bar 12 and is the essence of the provision of the bar 12 for the saglet to be omitted.

The case of the housing of 3 for measuring the parameters of the recipient is the antenna CCC 8, mounted on an airplane.

The system works with the tracking device. When removing an airplane, I left the aircraft 19 (see Fig. 4) for more than 3 km of housing 3 with hose 2 located at the end of the amulet.

The first and second speakers of the CEC through the antennas 8 and 17 take advantage of 20 satellites, based on the calculation of the total time

Paρagleτρy movement samοleτa τanκeρa-1 (πsevtsοdalnοsτi and πsevdοsκοροsτi) chβρez ρadiοκanal, vκlyuchayuschy πeρvuyu ρadiοsτan- tsigo UΚΒ 6 anτennοi 9 and vτορuyu ρadiοsτantsiyu UΚZ 14 anτennοi 18 ποsτuπayuτ on zχοd vychisllτelya ο.dnοvρemennο with 15 mi analοgichny- πaρameτρami calculated vτορym πρiemniκοm ССС 13, installed on the loaded aircraft 19.

Βychisliτel 15 οbρabaτyvaya shφορmatsigo ο πsevdοdalnοsτya ^χ and πsevdοsκοροsτyaχ samοleτοv vychislyaeτ iχ οτnοsiτelnye κοορdina- τy (οτnοsiτelnοe ποlοzhenie) and sκοροsτi (sκοροsτ convergence) and vydaeτ indiκaτορ to 16, in usτanοvlenny κabine zaπρavlyaemοgο samοleτa 19.

In the process of approaching aircraft in the calculator 15, the process ^χ ο-

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) 98/07623 ΡСΤ / ΚШ7 / 00263

10 days of continuous comparison of conditions

Χ "000 m

(Loss - ^ 500 m where βηch. "Ζ _τ ν ^ - the distance between the aircraft was increased, the side ζ is the vertical speed ratio of the metrics.

In order to achieve this condition (that is, when approaching aircraft), the calculator will receive a signal to release the normal hose with a cone. Eτοτ signal vτοροy ρadiοsτanπii UΚΒ cheρez anτennu UΚΒ 18 πeρedaeτsya on bορτ samοleτa τanκeρa-I, where πρinimaeτ- Xia cheρez anτennu UΚΒ 9 πeρvοy ρadiοsτantsiey UΚΒ 6 on vyχοde κοτοροy φορmiρueτsya uπρavlyayuschy signal for sρabaτyvaniya alarms on πulτe οπeρaτορa usτροysτva vyπusκa-ubορκi Hose Replacement 4. At the command of the manufacturer _. Replacing the replacement hose with a hose.

Β eτοm case vychisliτel 15 zychislyaeτ vzaimnοe ποlοzhenie (οτnοsiτelnye κοορdinaτy) and sκοροsτ sbdiζeniya (οτnοslτelnuyu sχοροsτ) λϊezhdu κοnusοιl 3 and zaπρavοchnοy schτangοϊ 12 zaπρazlyaemο- gο samοleτa 19 and vydaeτ this inφορmatsiyu πilοτu indiκaτορ to 16.

BEST MODE FOR CARRYING OUT THE INVENTION

It is advisable to equip an aircraft-tanker with an optional antenna antenna and a switch. Dοποlniτelnaya anτenna SΗS 10 (sm.φig.Z and 4) on usτanοvlena κοnuse 3 anτen- nym κabelem II, usτanοvlennym on zaπρavοchnοm shdange2.Αnτenny κabel II ποdsοe.dinen κ πulτu οπθρaτορa usτροδsτva vyπusκa- ubορκi zaπρavοchnοgο hose 24. Peρeκlyuchaτel 21 πρedsτavlyaeτ

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) 3

II sοbοy eleκτροmeχanicheοκοe usτροysτvο on οsnοve ρele, uπρavlyago- schaya οbmοτκa κοτοροgο associated with uπρavlyayushim vχοtsοm πeρeκlgochaτelya and two ρabοchiχ κοnτaκτa ρele svyaeany sοοτveτsτzenκο with πeρ- vym and vτορmi vχοdami πeρeκlgochaτelya and vyχοdnοy κοnτεκτ ρele yavlyaeτsya vyχοdοm πeρeκlyuchaτelya (on cheρτezhaχ not ποκazanο) .

Peρvy πρiemniκ SΗS 22 szοim zχοdοm associated with vyχοdοm πe- ρeκlgochaτelya 21 and vyχοdοm - with vhοdοm πeρvοy ρadiοsτantsii UΚΒ 23 svyazannοy anτennym vyχοtsοm with anτennοy UΚZ 9. Peρeκlyu- chaτel 21 svοim πβρvsh vχοdοm associated with anτennοy SYAΟ 8 πeρvοgο πρiemniκa SΗS and vτορym vχοdοm - with dοποlniτelnοπ εnτennοy SΗS 10 usτanοvlennοy on κοnuse 3. Pρi eτοm, anτennyZ κabel II, usτanοvlenny on zaπρavlyaemοm hose 2 ποdsοedinen κ πulτu οπeρaτορa usτροysτva vyπusκa-ubορκi zaπρavοchnοgο hose 24 vyχοd κοτοροgο ποdsοe.dinen κ vτοροmu vχοdu πeρeκlyuchaτelya 21. TsβlesοοbρaznοAlso, the command output of the front radio transmitter must be connected to the control unit via the key switch and the alarm system of the remote control.

With this case, the housing of the casing 3 for measuring the drive and the external housing of the casing and the charging rod is an optional antenna mounted on the remote control unit 10, installed on the third.

In this case, the system works as follows. When you remove the aircraft plane, I have turned on the airplane 19 (see FIG. 4) for a distance of more than 3 km; the body 3 has a hose; 2 In the case of the first part of the ССС 22 receiver, it is connected via the key switch 21 with the antenna ССС 8, mounted on the airplane fuselage, the system operates in the same way as above. When approaching aircraft, the calculator will receive a signal to release the usual hose with

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) \ νθ 98/07623 ΡСΤЛШ97 / 00263

12 inc. This signal is transmitted to the aircraft plane, where it is received through the antenna of the 9th front radio unit 23, and the output is transmitted to the signal There is no need to release a normal hose to the outlet with a pressure switch.

Pοsle vyπusκa hose κοnusοm πeρvy πρiemniκ SΗS 22 HA chinaeτ ρabοτaτ with dοποlniτelnοy anτennοy SΗS 10 κοτορεya πρi- nimaeτ signals οτ sπuτniκοv 20. eτοm in case οτnοsiτelnye κο- ορdinaτy and sκοροsτ convergence shτangi and κοnusa οπρedelyayuτsya with ποvyshennοy τοchnοsτgo.

Blagοdaρya presence on eκρane vysοκοτοchnοn inφορmatsii ο mutually imnοm ποlοzhenii and sκοροsτi sblineniya κοnusa and shτangi πilοτ zaπ- ρavlyaemοgο samοleτa προizvοdiτ uπρavlenie samοleτοm dο ποπada- Nia zaπρavοchnοy shτangl in κοnus and προizvοdsτva sτyκοvκi.

The measurement of the positive dynamics and speed between the available aircraft and the self-propelled tank is carried out as follows.

Peρvy πρiemniκ SΗS 5 usτanοvlenny on samοleτe-τanκeρe izmeρyaeτ πsevdοdalnοsτi 70 οτ dannοgο samοleτa dο sπuτniκοv 20. Β zavisimοsτi οτ τila πρiemniκa SΗS, izmeρenie πsevdοdal- nοsτey s - mοzheτ προizvοdiτsya data πρiemniκοm οdnοvρemen- nο οτ 12 τi sπuτniκοv, τ.e. in this case / = 14-12.

Κροme τοgο, sο sπuτniκοv on πρiemniκ SΗS ποsτuπaeτ sledugo- schaya inφορmatsiya οb iχ πaρameτρaχ: X ^*, Vy, - £ - κοορdinaτy sπuτniκοv in πρyamοugοlnοκ geο- tsenτρichesκοy sisτeme κοορdinaτ l have Θl "ϊ _£ - corners and mesτa azimuτa, οπρedelyaemye of SISΤΘ- me κοορdynam U?

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) \ νθ / 623 ΡСΤ / ΚШ7 / 00263

thirteen

'- signal ratio κ to noise; ^s * - Moscow time; - room of the satellites.

The information listed above with the CJC receiver is installed at the entrance of the front radio station, has it been installed? in an airplane and with an optional transmitter, the transmitter is on board an amusement aircraft.

This information is provided by the second radio unit, which is mounted on an available aircraft and, when it is released, it is installed on the computer. 15

One-day, i.e. in mοmenτ vρemeni ^ ^'vτορym πρiemni- κοm SΗS, usτanοvlennοm on dοzaπρavlyayuschemsya samοleτe, izmeρyayuτ- camping πsevdοdalnοsτi Α) / ΟΤ dannοgο samοleτa dο sπuτniκοv. Τaκzhe on vχοd dannοgο πρiemniκa ποsτuπaeτ inφορmatsiya ο κοορdi- naτaχ sπuτniκοv-Χ ^', * y>] uglaχ mesτa and aziιluτa & m, κ signal υlz οb οτnοshenii noise (S / N) glοsκοvsκοm vρemeni £ _l and nο- meρaχ sπuτniκοv. The indicated information with the second receiver of the CSC will also run through the calculator 15.

Β in calculator 15, in the first place, a selection of satellites is produced, i.e. common satellites are selected with simple one-time functions of the CCS receiver.

After the selection of the satellites, the average household components in the geocentric system of the dynamite are calculated.

The calculation of the constituency of an airplane-tanker, U ^, and the reign of a deceased airplane Λ. , U, ^ - are based on the expression:

LISΤΒZΑΜΕΗIZYAΤΟGΟ (ПИЛΟ ₂₆ ) 98/07623 ΡСΤЛШ97 / 00263

14

/ 2.

- the satellites are connected to the geocentric system, which means that the index is л - which means the common messenger, and the indi- cator does not mean

_"M vannοe vρemya;

- д ο д д д ина ина ина ина д д д д д д д д д д д

^χ ϊ, 1 & CLEAN SYSTEM κοορdynam;

- The components of the available aircraft in the geocentric system of the unit;

Λν * ₁ Τ Лϊ - the complete range of the aircraft-tanker and the remaining aircraft, measured to the total satellite "L"".

Then, the following are shared:

where Λ Y ^' ^ Ι _Δ ^ s - is the difference of the geocentric ^χ κ ο д д dynamic.

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) Ρ Τ / ΙШ97 / 00263

fifteen

With a view to reducing the outright error, the calculation of the other-weekly output is produced in the following way :! The κοορ-system has one of the following for which the following path of destruction is used:

3 expressions χ (3) - (5) the following expressions: * 1 * η- - a long term of business; »- geocentric latitude of the processor; _* >. D- _t - geοtsenτρichesκaya ορτο, dροmichesκaya shiρsτa and dοlgοτa samοleτa-τayaκeρa; ^> _g 7 ^s ,% - positive components of the available aircraft in the city _. regal system κοορ.dinata 3> Us <? *

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) 98/07623 ΡСΤ / ΙШ97 / 00263

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The back-up of the available salted salad is not available to the small-tank, it is shared in the system of the industrial system.

In this case, the system is compatible with ^ ^ _{≠ ≠ ≠} - - ⁽ ^ 7 ^children have the following system taxes:

- the% ^ coincides with the rear path of the ν ^, and is aimed at the plane of the aircraft;

- the axis 0 is directed towards the geo-vertical, on top; ^

- οs with / + naπρavlena πο πeρπendiκulyaρu κ πlοsκοsτi '"*/" ^and ° ^ ρazueτ πρavuyu sisτemu κοορdinaτ.

Ηzchalο sisτemy ^ // '/ sοvπadaeτ with anτeκnοy πeρvοgο πρieshiκa SΗS, usτanοvlennοy on φyuzelyazhe samοleτa-τan- κeρa πρi removing samοleτοv bοlee 3000 m and πρi distance of less than 3000 m nachalο dannοy sisτemy κοορdinaτ budeτ sοvmeschenο with dοποl- niτelnοy anτennοy SΗS, usτanοvlennοy on Cone 3.

In this case, the relative large-scale components will be shared on the basis of the following expressions:

Where

Χ Expressions χ (6) - (8) take the following meanings:

LISΤ ΒЗΑΜΕΗ ЪΤΟΤΟΤΟΤΟ (ПΡΑΒИЛΟ 2β) ΡСΤЛШ97 / 00263

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- Reliable accessories for the mutual use of the fully-equipped self-propelled airborne aircraft system in the vehicle system.

^ - The angle of the plane-tanker, counted by the private sector at the time of the flight. ^ - _s - _s y

Calculation Methods of Relative Velocities α _*; r? The algorithms for calculating the relative positive dynamics are similar, with the exception of the fact that the measurement by the CJC receivers is based on an exclu- sive device.

Having found that it is easy to measure, it is possible to install 15

the thunder of the plane is a non-aircraft aircraft. This information is used for the production of a digital and digital display on a display of the aircraft that is available.

In order to make it possible to clarify the actual charac- teristics of the declared system of the defenses of a simple aircraft in the shells, it was possible to carry out amicable tests. How to remove the friend from another friends that are at a distance of 50 m. Errors of change of the claimed system have made:

- The positive dynamic - 0.5 m (L &

“Relative ^χ speed - 0.003 m / s (£ 6).”

For this reason, the application of the claimed system for loading aircraft by aircraft will allow the following:

- Increase the security of the connection at the connection stage;

- To ensure the search and the flight of planes on the territory of the ^χ kursa ^χ ι: a distance of at least 300 km;

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26) \ УΟ 98/07623 ΡСΤ / Κϋ97 / 0026Э

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- Significantly reduce the physical load of the arms;

- Save time for fuel and fuel.

LISΤ ΒЗΑΜΕΗ ЫЗЯΤΟГΟ (ПИЛΟ 26)

Claims

νθ 98/07623 ΡСΤ / ΙШ97 / 0026319ΦΟΡ'Г / ЛΑ ЛЗΟБΕΞΤΞΗЯЯ

1. Sπsτema zaπρavκi samοleτa τοπlivοm in ποleτe, zκlyuchayu- schaya zaπρavοchnΕy hose κοnusοm, usτanοvlennny on saιlοleτe-τan- κeρe, usτροysτvο vyπusκa.-ubορκi zaπρεvοchnοgο hose zaπρavοch- hydrochloric 'lτangu, usτanοvlennugo on zaπρavlyaemοm samοleτe daτchiκi πο- dοzheniya κοnusa and zaπρavοchnοy shτangi, sρedsτva οπρedeleniya mutually imnοgο ποlοzheniya κοnusa and zaπρavοchnοy ιπτangi, sοdeρzhaschie You are a chisliτel, οτlichayuschayasya τem, chτο sisτema provided πeρvym and vτο- ρym πρiemniκami sπuτniκοvοy navigatsiοnnοy sisτemy (SΗS) with anti τennami SΗS, and πeρvοy vτοροy ρadiοsτantsiyami y τρaκοροτκοvοlnο- vοgο diaπazοna (ZHΒ) usτanοvlennymi sοοτveτsτvennο on samοleτe-τanκeρe and zaπρavlyaemοm samοleτe, πρi eτοm πeρvy πρiemniκ SΗS associated with svοim vyχοdοm vχοdοm πeρvοy ρadiοsτantsii UΚΒ and vχοdοm ποdsοedinθn κ anτenne SΗS πeρvοgο πρiemniκa SΗS, calculated liτel connected πeρvym and secondly, with the output of a second time, the SSC has been connected to a second radio station, but the output is free of charge;

2. Sisτema zapρavκi samοleτa τοπlivοm in ποleτe πο π.Ι, οτ- τem Leach, chτο snabzhβna πeρeκlyuchaτelem, usτanοzlennym on samοleτe-τanκeρe ζ dοποlniτelnοπ znτennοy SΗS, usτanοvlennοy on κοnuse zaπρavοchnοgο shdanga, πρi eτοm, vyχοd πeρeκlyuchaτelya sοedinen sο vχοdοm πeρvοgο πρiβmniκa SΗS, and the first input of the switch is connected to the ССС antenna, and the second input of the switch is connected to the ССС optional antenna.

3. The sagulet refueling system in the industry is characterized by the fact that the outlet is connected with an emergency

LISΤ ΒЗ ΑΜΕΗ ЗЫЯΤΟГΟ (ПИЛΟ 26) \ УΟ 98/07623 ΡСΤ / ΚШ7 / 00263

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It doesn’t require the input of the control unit and the remote control unit of the exhaust pipe release.

LISΤΒZΑΜΕΗIZYAΤΟGΟ (ПИЛΟ26)