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WO1997033792A1 - Procede de ravitaillement d'avion cargo et systeme de mise en oeuvre - Google Patents

Procede de ravitaillement d'avion cargo et systeme de mise en oeuvre Download PDF

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Publication number
WO1997033792A1
WO1997033792A1 PCT/RU1996/000059 RU9600059W WO9733792A1 WO 1997033792 A1 WO1997033792 A1 WO 1997033792A1 RU 9600059 W RU9600059 W RU 9600059W WO 9733792 A1 WO9733792 A1 WO 9733792A1
Authority
WO
WIPO (PCT)
Prior art keywords
gρuzοvοgο
aππaρaτa
glα
leτaτelnοgο
aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/RU1996/000059
Other languages
English (en)
Russian (ru)
Inventor
Konstantin Ivanovich Marx
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Afanasiev Vadim Nikolaevich
ENTIN ALEXEI BORISOVICH
KUZINA ARIETTA HIKOLAEVNA
PECHATNIKOV JURY TOVIEVICH
TSOI LJUDMILA ALEXANDROVNA
Original Assignee
Afanasiev Vadim Nikolaevich
ENTIN ALEXEI BORISOVICH
KUZINA ARIETTA HIKOLAEVNA
PECHATNIKOV JURY TOVIEVICH
TSOI LJUDMILA ALEXANDROVNA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Afanasiev Vadim Nikolaevich, ENTIN ALEXEI BORISOVICH, KUZINA ARIETTA HIKOLAEVNA, PECHATNIKOV JURY TOVIEVICH, TSOI LJUDMILA ALEXANDROVNA filed Critical Afanasiev Vadim Nikolaevich
Priority to PCT/RU1996/000059 priority Critical patent/WO1997033792A1/fr
Publication of WO1997033792A1 publication Critical patent/WO1997033792A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D39/00—Refuelling during flight

Definitions

  • This product is generally not available, mainly for aviation, and more precisely for equipment and systems for the supply of cargo vehicles. There is a means of supplying a cargo machine and systems for their existence.
  • a disadvantage of this option is to save a plane for a passenger, which is equated with cargoes and a connected vehicle. Otherwise, the weight of the aircraft-carrier, which is not necessary, should be very significant for ensuring the safety, t. ⁇ . it has a cargo aircraft.
  • the unit has a dummy installation on the front panel / rail.
  • the cargo unit and the system indicated in this option are free of charge and the system is in danger of an inadvertent loss!
  • the conditions for securing the flow of fuel are also provided, ⁇ . ⁇ .
  • the delivery of the GLP is carried out on the active part of it (i.e., on the part of the ramp on high altitude), and not in the presence of the free car.
  • This system allows you to start shipping GLA immediately after taking off, reduce the initial reserve for GLN, but it is very small.
  • a forage system for the loading of a flying machine has been invented at the fungus.
  • GLP 1 - cargo unit
  • GSP ⁇ flexible fuel transmission system
  • the method of supplying the main parts of the system with its existing systems is related to the availability of products.
  • the user is shown to look at the surface in the socket of GL 1 and L2 2.
  • the appliance doesn’t take care of the appliance, it takes care of nothing
  • CHAPTER 1 n LZ2 2 4 take off from Zsmli. nalrpmsr, with airport, high and fast.
  • CHAPTER 1 is a quick transition to the field at the moment I ask the party.
  • CHAPTER 1 carries a useful load of 3, and the more costs that are incurred for a unit of weight, the more useful the load itself is, the more effective it is in the general case.
  • the unloading method for the delivery of cargo for the summer of the machine involves the execution of the following operations.
  • CHAPTER 1 and LHZ 2 have disposed, for example, for a single wide take-off 6 airport and for two parallel take-offs; CHAPTER 1 n LZ 2 has a take-off area so that you are next to “parallel” to each other; ⁇ azmeschayu ⁇ in ba ⁇ e 4 GL ⁇ 1 ⁇ a ⁇ e ⁇ lnches ⁇ v ⁇ to ⁇ liva, ⁇ to ⁇ e ne ⁇ b ⁇ dim ⁇ for vzle ⁇ a and ava ⁇ nin ⁇ n ⁇ sad ⁇ n and ⁇ a ⁇ zhe ⁇ azmeschayu ⁇ GL ⁇ 1 to 3.
  • P ⁇ sle ⁇ ds ⁇ ednneniya GSP ⁇ 5 ⁇ susches ⁇ vlyayu ⁇ sin ⁇ nnyG ⁇ n ⁇ a ⁇ allelnsh vzle ⁇ GL ⁇ L ⁇ Z 1 and 2 with ⁇ d ⁇ lyuchennym gn ⁇ im s ⁇ eds ⁇ v ⁇ m ⁇ e ⁇ edachn ⁇ lnva 5.
  • CHAPTER 1 and L2 2 have a parallel connection.
  • the entire subsidiary is located on the active site of the sector, i.e. A constant increase in altitude and speed of flight. If the engine in Chapter 1 is used, the dual fuel is flexible, but the flexible fuel transmission is 5, but it is used twice. fuel transfer equipment 10.
  • Engines may use various well-known fuel oils (D. Saton. Propulsion engines - ⁇ .: Industrial literature, 1952. - P. 126 - 140).
  • UPP 10 can be placed, for example, and not on LZ2, but on GL 1. It is less profitable, t. ⁇ . Correspondingly, try to reduce the weight of the truck.
  • the GPS-5 - may use well-known hoses that are used when airplanes are used in the air. Such hoses can include higher quality accessories for metal and / or metal rings. SHGP can also be performed in the form of a joint-negative connection of pipes, but the flexibility of the SHPX is slightly unreliable.
  • the accessories for connecting the hoses to the tanks of the tanks can be compared to the devices that are used for connecting the hoses to the hoses.
  • the unit is connected to the SHG 5 in the case of a formal acquisition at the airport.
  • SHG 5 must have remote controlled valves (valves) that interrupt the pipe after terminating the transmission if it is not necessary to do so 6 fuels after the hitch.
  • a medical device is a salver - LZ2 - it may be, for example, ordinary aircraft. Use in engines 2 using fuel.
  • the resulting fuel from CHP 1, as a result of the larger tanks of LZ 2, is increasing.
  • Dviga ⁇ el ⁇ L ⁇ Z 2 d ⁇ lzhny ⁇ bes ⁇ echnva ⁇ ⁇ yagu, ne ⁇ b ⁇ dimuyu ⁇ sh ⁇ a ⁇ alleln ⁇ g ⁇ ⁇ le ⁇ a L ⁇ Z 2 nabi ⁇ ayuschnm s ⁇ s ⁇ and vys ⁇ u GL ⁇ 1.
  • ⁇ izves ⁇ nym sis ⁇ emam u ⁇ avletsh m ⁇ gu ⁇ by ⁇ d ⁇ avleny sis ⁇ emy ⁇ n ⁇ ya vzanmn ⁇ go ⁇ as ⁇ l ⁇ zhennya le ⁇ a ⁇ elny ⁇ a ⁇ a ⁇ atov is ⁇ lzuemye, nal ⁇ ime ⁇ , ⁇ i s ⁇ y ⁇ v ⁇ e ⁇ smnches ⁇ i ⁇ al ⁇ a ⁇ atov and ⁇ a ⁇ zhe izves ⁇ nye sis ⁇ emy ⁇ n ⁇ lya vys ⁇ y sam ⁇ le ⁇ a above Earth ⁇ n ⁇ sad ⁇ e sam ⁇ le ⁇ a on ae ⁇ d ⁇ m.
  • plan of flight which may be different for different stages.
  • the first is the ready take-off.
  • the second step is to take off the GL 1 1 L2 2. This step takes place for starting the engine 11 GL 1 1 12 LZ 2, 1 ⁇ dn ⁇ v ⁇ smennyP and ⁇ a ⁇ allsly ⁇ y ⁇ ⁇ az ⁇ eg GL ⁇ 1 and L ⁇ Z 2 ⁇ d ⁇ s ⁇ a ⁇ chn ⁇ shn ⁇ P vzle ⁇ n ⁇ P ⁇ se 6 or ⁇ dn ⁇ v ⁇ smennyn s ⁇ a ⁇ with ⁇ yad ⁇ m s ⁇ yaschn ⁇ us ⁇ an ⁇ v ⁇ ve ⁇ n ⁇ aln ⁇ g ⁇ vzle ⁇ a, ⁇ dn ⁇ v ⁇ emennyn ⁇ yv GL ⁇ 1 ⁇ L ⁇ Z 2 ⁇ earth n s ⁇ vmes ⁇ iyP ⁇ le ⁇ GL ⁇ 1N L ⁇ Z 2 ⁇ ⁇ a ⁇ allelnym ⁇ ae ⁇ nyam, ⁇ e ⁇ e ⁇ ach ⁇ a to ⁇ liva NLZ 2 in CHL 1, therefore,
  • CHAPTER 1 and LZ2 are moving in parallel to complete the completed installation of the installed card. (The remaining cost in the tank 9 LZ 2 must be sufficient to return to Earth, if such a chance is granted.)
  • the automatic flight of the CHAPTER 1 is carried out on the basis of the assigned code.
  • the returning of GLV 1 to Earth is usually done in the usual way.
  • CHAPTER 1 and, inadvertently, part 2 have a loss of health and unavailable loss of health.
  • CHL 1 and LZ 2 can be made in the form of beta devices for better, ⁇ . e missile, as well as airborne-aerospace aircraft of a vertical Vela.
  • CHAPTER 1 and LZZ 2 it is disposed of on one or two separate land plots.
  • ⁇ General fuel tanks (4 and 9) have maximum fuel quality. P ⁇ sl ⁇ s ⁇ a ⁇ a ⁇ ach ⁇ a ⁇ liva of L ⁇ Z 2 GL ⁇ 1 nachinae ⁇ sya nemedlenn ⁇ 'ch ⁇ by dviga ⁇ li GL ⁇ L ⁇ Z 1 and 2 ea ⁇ ab ⁇ ali sch ⁇ ⁇ liva L ⁇ Z 2.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)

Abstract

Cette invention concerne un procédé de ravitaillement d'un avion cargo, ainsi que son système de mise en oeuvre. Ce procédé est destiné à un avion cargo dont les moteurs utilisent un carburant liquide. On fait appel à un avion ravitailleur qui va transporter le carburant pour l'avion cargo, et le lui transférer lors du vol commun et en parallèle des deux aéronefs. Avant leur décollage, l'avion cargo et l'avion ravitailleur sont reliés au sol à l'aide d'une conduite flexible de transfert du carburant. L'avion cargo décolle en même temps que l'avion ravitailleur auquel il est connecté.
PCT/RU1996/000059 1996-03-15 1996-03-15 Procede de ravitaillement d'avion cargo et systeme de mise en oeuvre Ceased WO1997033792A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/RU1996/000059 WO1997033792A1 (fr) 1996-03-15 1996-03-15 Procede de ravitaillement d'avion cargo et systeme de mise en oeuvre

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU1996/000059 WO1997033792A1 (fr) 1996-03-15 1996-03-15 Procede de ravitaillement d'avion cargo et systeme de mise en oeuvre

Publications (1)

Publication Number Publication Date
WO1997033792A1 true WO1997033792A1 (fr) 1997-09-18

Family

ID=20129984

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU1996/000059 Ceased WO1997033792A1 (fr) 1996-03-15 1996-03-15 Procede de ravitaillement d'avion cargo et systeme de mise en oeuvre

Country Status (1)

Country Link
WO (1) WO1997033792A1 (fr)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7188807B2 (en) 2005-03-11 2007-03-13 The Boeing Company Refueling booms with multiple couplings and associated methods and systems
US7213787B2 (en) 2005-06-07 2007-05-08 The Boeing Company Valves for annular conduits including aircraft fuel conduits and associated systems and methods
US7219857B2 (en) 2005-06-20 2007-05-22 The Boeing Company Controllable refueling drogues and associated systems and methods
US7293741B2 (en) 2005-06-09 2007-11-13 The Boeing Company System and methods for distributing loads from fluid conduits, including aircraft fuel conduits
US7309047B2 (en) 2005-02-25 2007-12-18 The Boeing Company Systems and methods for controlling flexible communication links used for aircraft refueling
US7458543B2 (en) 2005-06-10 2008-12-02 The Boeing Company Aerial refueling system
US7469863B1 (en) 2005-03-24 2008-12-30 The Boeing Company Systems and methods for automatically and semiautomatically controlling aircraft refueling
US7472868B2 (en) 2005-09-01 2009-01-06 The Boeing Company Systems and methods for controlling an aerial refueling device
US7533850B2 (en) 2005-06-09 2009-05-19 The Boeing Company Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems
US7581700B2 (en) 2005-06-09 2009-09-01 The Boeing Company Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods
US7637458B2 (en) 2005-06-08 2009-12-29 The Boeing Company Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4398685A (en) * 1981-03-11 1983-08-16 The United States Of America As Represented By The Secretary Of The Air Force Aerial day/night refueling stations
FR2568852A3 (fr) * 1984-05-12 1986-02-14 Babeurs Jean Dispositif de ravitaillement pour helicopteres et avions a decollage vertical en vol stationnaire
FR2569652A1 (fr) * 1984-09-04 1986-03-07 Messerschmitt Boelkow Blohm Dispositif de ravitaillement en vol pour appareils volants
FR2627452A1 (fr) * 1988-02-19 1989-08-25 Whittaker Controls Inc Systeme de ravitaillement en carburant en vol
US5131438A (en) * 1990-08-20 1992-07-21 E-Systems, Inc. Method and apparatus for unmanned aircraft in flight refueling

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4398685A (en) * 1981-03-11 1983-08-16 The United States Of America As Represented By The Secretary Of The Air Force Aerial day/night refueling stations
FR2568852A3 (fr) * 1984-05-12 1986-02-14 Babeurs Jean Dispositif de ravitaillement pour helicopteres et avions a decollage vertical en vol stationnaire
FR2569652A1 (fr) * 1984-09-04 1986-03-07 Messerschmitt Boelkow Blohm Dispositif de ravitaillement en vol pour appareils volants
FR2627452A1 (fr) * 1988-02-19 1989-08-25 Whittaker Controls Inc Systeme de ravitaillement en carburant en vol
US5131438A (en) * 1990-08-20 1992-07-21 E-Systems, Inc. Method and apparatus for unmanned aircraft in flight refueling

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7309047B2 (en) 2005-02-25 2007-12-18 The Boeing Company Systems and methods for controlling flexible communication links used for aircraft refueling
US7188807B2 (en) 2005-03-11 2007-03-13 The Boeing Company Refueling booms with multiple couplings and associated methods and systems
US7469863B1 (en) 2005-03-24 2008-12-30 The Boeing Company Systems and methods for automatically and semiautomatically controlling aircraft refueling
US7213787B2 (en) 2005-06-07 2007-05-08 The Boeing Company Valves for annular conduits including aircraft fuel conduits and associated systems and methods
US7637458B2 (en) 2005-06-08 2009-12-29 The Boeing Company Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft
US7293741B2 (en) 2005-06-09 2007-11-13 The Boeing Company System and methods for distributing loads from fluid conduits, including aircraft fuel conduits
US7533850B2 (en) 2005-06-09 2009-05-19 The Boeing Company Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems
US7581700B2 (en) 2005-06-09 2009-09-01 The Boeing Company Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods
US7458543B2 (en) 2005-06-10 2008-12-02 The Boeing Company Aerial refueling system
US7665479B2 (en) 2005-06-10 2010-02-23 The Boeing Company Aerial refueling system
US7219857B2 (en) 2005-06-20 2007-05-22 The Boeing Company Controllable refueling drogues and associated systems and methods
US7472868B2 (en) 2005-09-01 2009-01-06 The Boeing Company Systems and methods for controlling an aerial refueling device

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