WO1995032894A1 - Semi-rigid dirigible aerostat - Google Patents

Semi-rigid dirigible aerostat Download PDF

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Publication number
WO1995032894A1
WO1995032894A1 PCT/RU1995/000100 RU9500100W WO9532894A1 WO 1995032894 A1 WO1995032894 A1 WO 1995032894A1 RU 9500100 W RU9500100 W RU 9500100W WO 9532894 A1 WO9532894 A1 WO 9532894A1
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WO
WIPO (PCT)
Prior art keywords
gas
external
secured
air
lighter
Prior art date
Application number
PCT/RU1995/000100
Other languages
French (fr)
Russian (ru)
Inventor
Jury Grigorievich Ishkov
Lev Mikhailovich Kuznetsov
Original Assignee
Jury Grigorievich Ishkov
Lev Mikhailovich Kuznetsov
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
Priority to AU25811/95A priority Critical patent/AU2581195A/en
Application filed by Jury Grigorievich Ishkov, Lev Mikhailovich Kuznetsov filed Critical Jury Grigorievich Ishkov
Publication of WO1995032894A1 publication Critical patent/WO1995032894A1/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships

Definitions

  • Managed aeronautical aerial vehicles - diariably - are widely known. 5 Lately, it is considered to be efficient diaphragms with a compact form, which have a range of advantages in comparison with the alternatives of a characteristic. ⁇ these benefits
  • Niz ⁇ aya ves ⁇ vaya ⁇ dacha and ⁇ a ⁇ yae You are a s ⁇ aya s ⁇ im ⁇ s ⁇ and sl ⁇ zhn ⁇ s ⁇ izg ⁇ vleniya and OPERATION.
  • the use of a pressure transmitter and a protective part of it is a soft forming element filled with lighter air or an external gas pressure: Separating the internal volume of the gas by the gas is lighter than the air and the volume of the heated gas: located in the upper part of the gas chamber. gas filled lighter than air; Reserved on a case by hand on the 5th day of hanging the gondola, the load compartment, a sedentary installation, and equipped with accessories.
  • the disadvantages of hosted di- arya are the relatively low stability of the body of the casing and the inability to pay for a non-profitable device.
  • the disadvantages are that the result of diarrhea is: a large mass of fossil fuels and hard domestic power. ⁇ ressivnyh _ reduction of its weighted ⁇ toy; Radial use of the auspicious interior elements of the internal suspension: the absence of accumulation and fixation of a balloon with gas is easier to escape: there is no danger of With all the necessary information, 5 the basic task is to create a user-friendly and portable air-borne versatile vehicle. equipped with a thermal system for generating lift, ballasting with a reduced cross section in the midsection at a constant speed and higher wind power.
  • the posed problem is solved in that, in the case of a user-friendly aerospace device, including: disk drive; The convenient location for quick and easy access to external casters;; ierible ierides;;;;;;; The well-equipped parking place is
  • the output of its height to the diameter was selected in the range from 0.30 to 0.45: a strong external power factor was calculated as a result of this, and 0 percent of this value was obtained; the height of the western part is not more than 0.5 -4- heights of the body of the flying device; A separate part of its own is secured on an external container; the lower part of its larger external battery is secured on the external side, and the lower large component is secured on the internal side; in the outer outdoor area, the diaphragm is made in the form of an external space. Allowed housing is not lower than the second quarter. dividing the indicated internal volume by the volume of gas located above the membrane is lighter than air and the volume of gas heated by the membrane. At the same time, the membrane is protected by its large external storage compartment.
  • the gas supply area is equipped with facilities for supplying and discharging the exhaust gas and exhaust air; in gas, the central outlet is lighter than the air. reserved by its upper part on the outside.
  • Another version of the performance of the amplification of the upper part of the site in the place of the accumulation of the central power supply can be performed in the form of a closed strong power. for example. a polygon or a ring, attached to the outer circle.
  • the option to implement the Central Resource is optional.
  • Well-developed natural elements for example. tapes or trusses, the outer ends are fastened to the upper part, and the end end is secured to the power elements of the familiar side. By the way, in the central region.
  • the balloons filled with gas are easier to use than air and store them on strong internal components.
  • One of the options for executing a hard external cas- ter is the presence of a belt of power consisting of power elements and a wiring harness
  • the owner of the vehicle which is stored on an external basis, is different in the form of a strong development-stabilization of the external condition and the independence of the device is inconvenient
  • the free-loading module should be executed in the form of a payment.
  • the proposed invention allows the construction of a proprietary aerostatic apparatus - ⁇ -
  • the rate was selected in the range ⁇ from 0.025 to 0.05. and the height of the internal space is no more than 0.5 height of the body of the aircraft.
  • the stated cases were calculated using the standard method and
  • the green shell is made in the form of two upper and lower shells and secured to the hard power ⁇ of the element ⁇
  • the internal volume of the body of the flying unit is separated by a flexible membrane located above the membrane, the gas is lighter than the air and the gas is completely free of charge
  • the membrane is made from an elastic material in the form of an inversion, formed by rotation of a
  • the membrane design makes it possible to change the volume ratio of gas volumes to a larger extent. It is easier to air and
  • the gas supply area is equipped with facilities for supplying heated gas and exhaust air to it and exhausting it into the atmosphere.
  • the source of the preheated gas is the pre-emptive propulsion system. Otherwise, as a result of the source of heated gas may
  • ⁇ ⁇ aches ⁇ ve nag ⁇ 'e ⁇ g ⁇ gas m ⁇ gu ⁇ by ⁇ is ⁇ lz ⁇ vany ne ⁇ s ⁇ eds ⁇ venn ⁇ vy ⁇ l ⁇ nye gases sil ⁇ v ⁇ y us ⁇ an ⁇ v ⁇ i or ⁇ - du ⁇ y g ⁇ eniya and ⁇ a ⁇ zhe v ⁇ zdu ⁇ nag ⁇ e ⁇ y in ⁇ e ⁇ l ⁇ bmenni ⁇ e, ⁇ b ⁇ g ⁇ evaem ⁇ m zy ⁇ l ⁇ nymi gases or ⁇ du ⁇ ami g ⁇ eniya.
  • Heated gas is supplied to the area of heated gas through the distribution system. Includes a collector, a ventilation unit, gas and air conditioning systems.
  • the flue gas outlet is free from exhaust ventilators. Discharge of heated gas and air from the heated area -8-
  • the gas is exhausted through exhaust valves; the operation is shorted from the control cubicle.
  • the supply of heated gas to the volume of heated gas due to the increase in the temperature and, accordingly, the increase in the volume of gas is increased
  • the aerodynamic lifting force decreases. In this way, in a separate manner, the device can be operated by flying without using a traditional ballast system.
  • a quick external power supply is secured by a live external power supply and is equipped with a free-standing membrane.
  • the large amount of space available for the internal use of the internal components makes it easier to regulate the tension and makes it more comfortable to use.
  • the regulation of the tension of the auxiliary elements of the internal suspension is carried out by means of hydraulic amplifiers-boosters. winch or screw connections. reserved for the power elements of internal facilities.
  • the gas area is lighter than the air and the central outlet is located. Secured in its upper part on the outside. and from the bottom, secured on the inside. Two options are available for the implementation of the central site. S ⁇ g- lasn ⁇ ' ⁇ e ⁇ v ⁇ mu va ⁇ ian ⁇ u tsen ⁇ alny ⁇ se ⁇ vy ⁇ lnen gaz ⁇ ne ⁇ - ⁇ nitsaemym of elas ⁇ ichn ⁇ g ⁇ ma ⁇ e ⁇ iala, na ⁇ ime ⁇ , anal ⁇ gichn ⁇ - g ⁇ ma ⁇ e ⁇ ialu na ⁇ uzhn ⁇ y ⁇ b ⁇ l ⁇ ch ⁇ i.
  • the central circuit is divided into the lower part of the gas-tight gas separator.
  • the central unit which is made from genuine natural elements • or a network, is filled with gas cylinders that are lighter than air. Short-circuited are secured to the power elements of the internal circuit.
  • a large gain is secured in the form of a tape from a medium with a small load and it is free of loading for example. polygon or ring.
  • ⁇ Brass ⁇ réelle gas areas are lighter than air; gas cylinders are located.
  • Gas cylinders are filled with gas easier than air, for example, helium, and in their lower part are secured to power elements inside the unit. and in the majority, they are registered on the outside in the most convenient way. that gas points can change their application.
  • the system for fixation of points on the upper side is often made in the form of a “loop-on-the-loop ” device , or in the form of a loop. One end is secured on a gas point, and the second end is secured on the upper side. Placing gas is easier than air intake in gaseous sell- ers, it is more easily transported to the gas and it is more airborne than the air vessel. The fixation of gas points.
  • each gas point is secured to the power elements of the internal external part of its external part.
  • the hard external force is made in the form of a good path, for example, from a commercially available material or metal.
  • the hard external external casing made in the ZID was performed tight and equipped with a device for changing the internal pressure. in particular, to create excessive pressure inside.
  • the current version of the large-sized ammunition and the large capacity of the vehicle is equipped with a quick-drive. consisting of power elements and systems connecting the power elements to the ground or performed as a circuit mounted on the ground circuit. Increased internal pressure and the presence of a belt of harshness increase the harshness of the outside of the pipe.
  • the body of the body of the flying device is executed in the form of development of a small-sized, strong external product,
  • the availability of stabilizing devices improves aerodynamic performance and increases the stability of the flying machine while it is in motion.
  • aerodynamic control systems direct power settings and power settings are reserved.
  • the internal hard drive is equipped with a separate load compartment and a separate load module. equipped with notifications for his order
  • a separable load module can be configured as a container for discharging solid or bulk loads. for transporting standard goods. Tank for transporting low cargo. for example. oil and oil products. gas burner for gas transport. capacities for the transportation of gas, cabins for the transportation of passengers, car rental, including the price of the accommodation The local emergency, emergency, emergency, public or other purpose.
  • the small appliance is equipped with a device for transporting loads on an external suspension, in particular, a large-sized unit that does not extend the division of loads.
  • the device for transporting loads on the outside is suspended from ropes mounted on power windings that are powered by power ⁇ ⁇ a ⁇ ⁇ ⁇ e ⁇ ⁇ and a nd e ⁇ ⁇ e
  • Fig. 1 shows a vertical section of the semi-active airborne aerospace device. according to the invention.
  • Fig. 2 - a horizontal section of a flying machine • with a shift in the central location, it was vertical.
  • FIG. 4 - version of the central network (from genuine items with gas cylinders).
  • Fig. 3 - a fragment of a transverse part of the rim of a flying device.
  • the ammunition includes an integrated and external storage compartment and a strong external enclosure I, made in the form of an empty compartment. For this reason, ⁇ has been completed in such a way. that it is eccentric in the range from 0.025 to 0.05. ⁇ sialn ⁇ ⁇ n ⁇ si ⁇ eln ⁇ vne ⁇ - neg ⁇ ⁇ a ⁇ asa 1 ⁇ as ⁇ l ⁇ zhen ⁇ ly ies ⁇ y sil ⁇ v ⁇ y vnu ⁇ en- Nij ⁇ s ⁇ v 2.
  • the unit has a shell, made of soft, gas-impervious material in the form of two - upper 4 and lower 5.
  • ⁇ e ⁇ nyaya 4 ⁇ b ⁇ l ⁇ ch ⁇ a sv ⁇ ey ⁇ m ⁇ y za ⁇ e ⁇ lena on yaes ⁇ m sil ⁇ v ⁇ m external ⁇ a ⁇ ase 1.
  • ⁇ izhnyaya 5 ⁇ b ⁇ l ⁇ ch ⁇ a sv ⁇ ey b ⁇ lshey ⁇ m ⁇ y ⁇ a ⁇ ne za ⁇ e ⁇ lena on the outer ⁇ a ⁇ ase 1.
  • the area of 8 heated gas is supplied with devices (not indicated) for the delivery of and removal of heated gas and foreign air from it.
  • the source of hot gas is an essential power plant, in particular. -thirteen-
  • the source of hot gas can be used for special purposes (not indicated).
  • the direct exhaust gases of high power plants or products of combustion are used.
  • the device for the supply of heated gas to the volume of 8 heated gas includes a distribution system (not specified), which is integrated in the gas unit, is ventilated.
  • the device for the delivery and release of the air inlet includes the fans and the valves mounted on the bottom 5. not indicated).
  • the internal suspension is located in the area of 8 heated gas.
  • ⁇ ⁇ aches ⁇ ve ⁇ is ⁇ s ⁇ bleny for ⁇ eguli ⁇ vaniya na ⁇ yaieniya ⁇ d ⁇ ln ⁇ yaes ⁇ - ⁇ i ⁇ elemen ⁇ v 3 is ⁇ lz ⁇ vany gid ⁇ avliches ⁇ ie usili ⁇ eli- ⁇ us- ⁇ e ⁇ y. Otherwise, as a part of the system for regulating the tension of the auxiliary elements of 3 internal suspensions, the winch or the screw may be used.
  • a gas area of 7 is lighter than air and a central compartment of 10 is located, most of which are secured on the outside of 4. and the bottom part is reserved for a hard internal power 2.
  • the central part 10 is made just one of two options. According to the first variant (Fig. 3), the central part 10 is made in the form of a gas-tight, closed capacitance from a material of the analogous to the old one.
  • the outer compartment of the central compartment 10 is secured to the upper 4 circuit, and its lower compartment is secured to the external circuit 2.
  • the central gas circuit is not connected to the -14-
  • an upper 12 part of the central 10 is filled with gas lighter than the air, and the other 13 part of the central 10 is a point.
  • the tank is equipped with a notification (not indicated) to change the pressure
  • the central part of 10 is all equipped with 14 solid elements, for example, ribbons or cables, or a network.
  • 14 solid elements for example, ribbons or cables, or a network.
  • the simple external force case 1 (Fig. 2) is made in the form of a complete staircase and is made from a multi-unit or from a combined between sections 18.
  • a strong external power supply unit 1 is equipped with a simple hardness (Fig. 5). consisting of a power element 19 and a power of 20. connecting parts of a power element 19 with an external shortcut 1. Variable performance is unavailable -15- secured in an external case of 1 Colombian force (not shown).
  • the case of the case of the flying device. Ig.1.2 is made in the form of development-stabilization of 21 and 22 days of a strong external case of 1, augmented by other non-existing and external parts.
  • the gondola 28 of the control is secured.
  • the arrangement for the transport of goods on the other hand is made in the form of natural elements. for example, ⁇ Mercedes availability. protected winch. FITTED ON POWER COMPONENTS OF INTERNAL OUTDOOR 2 AND ON FOREIGN CASE 1. AND LOADING UNIT.
  • the parking chassis 30 is secured.
  • Gas cylinders 17 and the upper 12 part of the central heating unit 10 or gas cylinders 15 of the central heating unit 10 are filled with helium or other gassed gases.
  • central step 10 is gas-impervious. delivers air ⁇ ballonet 13.
  • the portable linear size of the dispensable medical device with the compact disk is the length of the disk.
  • the ammunition is also balanced by increasing the aeronautical lifting force by the weight of the load due to the delivery of the fresh gas to the load 8. The unloading of the freezer.
  • the loading device is loaded with a portable device and is optional. More often, they increase aerospace lifting force by an amount that ensures the vertical transfer of the aircraft to the necessary altitude. Drive the engines of a power unit of 9 and a new manual power unit 23 and load a load in the place of unloading or. They recover the ammunition from the unloading area and stabilize its active components. and, in the event of an emergency, they take advantage of a flying machine at the place of unloading or installing them at the place of sewing. umenshayu ⁇ ae ⁇ s ⁇ a ⁇ iches ⁇ uyu ⁇ demnuyu force on g ⁇ uza weight value, or in case ⁇ deleniya g ⁇ uz ⁇ v ⁇ g ⁇ m ⁇ dulya 27.
  • ⁇ de- -17- loading module 27 may be removed to the loading section and secured in it.
  • the unit of the cargo module 27 is operated by the use of replaceable load modules. and also in the event of the filling of a separate module 27 in the form of a special function area: either a place of residence, a place of destination, or an ingo.
  • ⁇ azemnaya s ⁇ yan ⁇ a ⁇ lunes ⁇ g ⁇ u ⁇ avlyaem ⁇ g ⁇ ae ⁇ s ⁇ a ⁇ i- ches ⁇ g ⁇ le ⁇ a ⁇ eln ⁇ g ⁇ a ⁇ a ⁇ a ⁇ a s ⁇ glasn ⁇ iz ⁇ b ⁇ e ⁇ eniyu ⁇ su- sches ⁇ vlyae ⁇ sya ⁇ b ⁇ az ⁇ m follows: vy ⁇ us ⁇ ayu ⁇ gas from ⁇ l ⁇ s ⁇ i 8 nag ⁇ e ⁇ g ⁇ gas and umenshayu ⁇ na ⁇ yazhenie ⁇ d ⁇ ln ⁇ yaes ⁇ i ⁇ elemen ⁇ v 3 znu ⁇ enney ⁇ dves ⁇ i.
  • P ⁇ me ⁇ e dalneisheg ⁇ reduce ae ⁇ s ⁇ a ⁇ iches ⁇ y ⁇ demn ⁇ y strength and s ⁇ ascheniya ⁇ bema ⁇ l ⁇ s ⁇ i 8 nag ⁇ e ⁇ g ⁇ for gas-le ⁇ a ⁇ elny a ⁇ a ⁇ a ⁇ zs ⁇ ae ⁇ s ⁇ yan ⁇ chnye on the chassis 30.
  • P um p a r i n g a n g a n t h a n t a nce a unit may be sold as a universal product for the use of a load.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

The proposed semi-rigid dirigible aerostat has a discus-shaped hull and comprises a rigid heavy-duty outer frame (1) around the circumference of the hull and forming the edge thereof; a hollow rigid heavy-duty inner frame (2) attached to the outer frame (1) by an inner suspension member made of longitudinally rigid elements (3); an outer skin formed in two skin sections, namely an upper skin section (4) and a lower skin section (5); gas balloons (17) configured in the inner space and filled with a lighter-than-air gas; a cargo capsule inside the inner frame (2); a deflector secured to the outer frame (1) and forming a relatively sharp hull edge; a control cabin; a propulsion system and control systems. According to the invention, the relative thickness of the hull is chosen between 0.30 and 0.45; the outer frame is designed as rigid heavy-duty torus with an eccentricity of between 0.025 and 0.050; the height of the inner frame (2) is no greater than 0.5 the height of the hull; a membrane (6) is provided in the interior hull space in the form of a surface formed by rotation of a curve of at least the second order; this membrane is attached to the outer frame (1) and inner frame (2) and divides the interior hull space into a chamber for lighter-than-air gas and a chamber for heated gas. The heated gas chamber is provided with devices for introducing and discharging heated gas and outside air. A central capsule (10), provided with a receptacle for lighter-than-air gas, is mounted inside the chamber for the lighter-than-air gas; this central capsule is attached to the upper skin (4) and inner frame (2). The upper skin section (4) has a reinforcement (16) at the site where the central capsule (10) is attached; the gas balloons (17) are secured to heavy-duty elements of the inner frame (2) and attached to the upper skin section (4); longitudinally rigid elements (3) of the inner suspension member are attached in pairs at one end to the outer frame (1) and attached at the other end to the heavy-duty elements of the inner frame (2) along tangents to the frame surface at diametrically opposite points.

Description

ПΟЛУЖΕСΤΚйй УПΡΑΒЛЯΕΜЫИ ЙЗΡΟСΤΑΤИЧΕСШ ЛΕΤЙΤΕЛЬΚΗЙ ΑППΑΡΑΤ PΟLUZHΕSΤΚy UPΡΑΒLYAΕΜY YZΡΟSΤΑΤICHΕSSH LΕΤΕΤΤΕΤΕΚΗ ΑППΑ
0 б л а с τ ь τ е χ н и κ и йзοбρеτение οτнοсиτся κ уπρавляемым азροсτаτичесκим0 more accurate
5 леτаτельным аππаρаτам, а бοлее τοчнο - κ диρииаблям с дис- κοοбρазнοй φορмοй κορπуса, в часτнοсτи - κ диρинаблям πο- лужесτκοй сисτемы с τеρмичесκим балласτиροванием. П ρ е д ш е с τ в у и щ и й у ρ ο в е н ь τ е χ н и κ и5 medical devices, and more precisely - for spare parts with a discrete partition, in particular - for a radial system with a radial disruption. P r later on t ue and ρ в е τ е е е и
Ю Уπρавляемые аэροсτаτичесκие леτаτельные аππаρаτы - диρияабли - шиροκο извесτны. 5 ποследнее вρемя счиτаюτся πеρсπеκτивными диρияабли с κορπусοм дисκοοбρазнοй φορмы, имешщие ρяд πρеимущесτв πο сρавнению с диρинаόлями τρади- циοннοй сигаροοбρазнοй Φορмы. Κ эτим πρеимущесτвам диρи-Managed aeronautical aerial vehicles - diariably - are widely known. 5 Lately, it is considered to be efficient diaphragms with a compact form, which have a range of advantages in comparison with the alternatives of a characteristic. Κ these benefits
15 жаблей дисκοοбρазнοй φορмы οτнοсяτся: снинение сτοимοсτи леτаτельнοгο аππаρаτа и цены ποτρебления за счеτ униφиκа- ции κοнсτρуκциοнныχ элеменτοв и τеχнοлοгичесκиχ προцессοв изгοτοвления; увеличения весοвοй οτдачи - οτнοшения веса κοммеρчесκοгο гρуза κ сοбсτвеннοму весу леτаτельнοгο аππа- 0 ρаτа; вοзмοжнοсτь ρабοτы в ρежиме висения на малοй высοτе, в τοм числе за счеτ эκρаннοгο эφφеκτа: удешевление сρед.сτв .шваρτοвκи и ποсадοчныχ πлοщадοκ.15 jabs of the distributed form are not available: decrease in the cost of the economical apparatus and the cost of the consumptions due to the unification of the electrically operated elements and the process; increase in weight yield - weight ratio of commercial cargo to the total weight of the summer flight rate 0; The possibility of working in the mode of hanging at low altitude, including due to the electronic effect: cheaper environment . Sewing facilities and landscaping areas.
Β κачесτве газа легче вοздуχа в аэροсτаτичесκиχ леτа- τельныχ аππаρаτаχ, в τοм числе в диρияабляχ, исποльзуиτся 5 вοдοροд, гелий, свеτильный газ. а τаκже ρазмещенные ρаз- дельнο οдин из газοв легче вοздуχа, наπρимеρ гелий и наг- ρеτый вοздуχ, в часτнοсτи, за счеτ οτχοдящегο τеπла силο- вοй усτанοвκи. Исποльзοвание ποдъемнοй силы газа легче вοздуχа и вοздуχа нагρеτοгο за счеτ οτχοдящегο τеπла дви- 0 гаτелей ποзвοляеτ снизиτь ρасχοд газа легче вοздуχа и οсу- щесτзляτь τеρмичесκοе балласτиροвание леτаτельнοгο аππаρа- τа.Газа The quality of gas is easier for aerosol in aeronautical devices χ , including in diarium, 5 hydrogen, helium, and light gas are used. and also one separate from the gases is lighter than air, for example helium and heated air, in particular, due to the fact that it is free of heat. The use of gas lift is easier for air and air due to the exhaust heat of the 0-heater being used, which reduces gas consumption and is easier to clean
Исποльзοвание κορπуса дисκοοόρазнοй φορмы в сοчеτании с τеρмичесκим όалласτиροванием даеτ зοзмοннοсτь сοздания 5 уπρавляемοгο аэροсτаτичесκοгο леτаτельнοгο аππаρаτа уни- веρсальнοгο назначения дοсτаτοчнοй гρузοποдъемнοсτи. πρи- гοднοгο κаκ для οсущесτвления длиτельныχ ποлеτοв. τаκ и -2-The use of a discrete housing in combination with a thermal distribution allows the use of a 5 optional aerosol The best way to make long trips. τak and -2-
для исποльзοвания в κачесτве леτаищегο κвана.for use in the quality of the summer shroud.
Извесτны προеκτы диρиκаблей бοльшοй гρузοποдъемнοсτи . κορπусοм дисκοοбρазнοй φορмы: προеκτ "ΤЬегвοδкνδϊπρ ' Βе- лиκοбρиτания ( йτοги науκи :. τеχниκи. Сеρия 'ΒοздушныйLarger load capacities are known. κορπusοm disκοοbρaznοy φορmy: προeκτ "Τegvοδkνδϊπρ 'Βe- liκοbρiτaniya (yτοgi nauκi:. τeχniκi Seρiya.' Βοzdushny
5 τρансπορτ" τ.18, 1989г..ЗИΗИΤИ.Μοсκва.Г.Д. йρалοв. С.Г.Εли- сеенκο 'Исποльзοвάние сοвρеменныχ аэροсτаτичесκиχ леτаτе- льныχ аππаρаτοв" ,см.с. 5.86 \ προгρамма 'Αϋаз". Φρанция СΗοвοе в жизни, науκе ;<. τеχниκе, Сеρия Τρансπορτ" л 11, 1977 г, Οбщесτвο "Знание", Μοсκва.Г.С.Ηесτеρенκο. Β.И.Ηа-5 τρansπορτ "τ.18, 1989g..ZIΗIΤI.Μοsκva.G.D. Yρalοv. S.G.Εli- seenκο 'Isποlzοvάnie sοvρemennyχ aeροsτaτichesκi χ leτaτe- lnyχ aππaρaτοv" sm.s. 5.86 \ π ρ ρ ам ам """"""""""""""""""" . Αϋ """""""" Αϋ """"""""""""""""""""""" Η Η Η Η Η Η Η Η Η Η Η 5. Β.I.Η-
Ю ρинсκий " Сοвρеменные аэροсτаτичесκие леτаτельные аππа- ρаτы, см. с.56,57). Ρазρабοτанные πο зτим προгρаммам леτа- τельные аππаρаτы являюτся диρияаблями иесτκοй сисτемы. Иχ недοсτаτκами являюτся: низκая весοвая οτдача, а τаκяе вы- сοκая сτοимοсτь и слοжнοсτь изгοτοвления и эκсπлуаτации.Yu ρinsκy "Sοvρemennye aeροsτaτichesκie leτaτelnye aππaρaτy see s.56,57) Ρazρabοτannye πο zτim προgρammam leτaτelnye aππaρaτy yavlyayuτsya diρiyaablyami iesτκοy sisτemy Iχ nedοsτaτκami yavlyayuτsya:... Nizκaya vesοvaya οτdacha and τaκyae You are a sοκaya sτοimοsτ and slοzhnοsτ izgοτοvleniya and OPERATION.
15 Извесτен τаκже мягκий диρияаοль с κορπусοм дисκοοб- ρазнοй φορмы ι£Β, Β, 117 28) вκлючающий наρужную οбοлοч- κу; ρасποлοженный πο πеρиφеρии κορπуса и οбρазуищий егο τορцевую часτь мягκий φορмиρующий элеменτ, заποлненный га- зοм легче вοздуχа или вοздуχοм ποд избыτοчным давлением: 0 цилиндρичесκую или κοничесκуи уπρугуи газοнеπροницаемуи πеρегοροдκу; ρазделяющую внуτρенний οбъем κορπуса на πο- лοсτь.газа легче вοздуχа и ποлοсτь нагρеτοгο газа: ρасπο- лοженный в Беρχней часτи κορπуса заллοн. заποлненный газοм легче вοздуχа; заκρеπленные на сόοлοчκе πρи ποмοши ьнуτ- 5 ρеннеκ ποдвесκи гοндοлу, гρузοвοй οτсеκ, сидοвчю усτанοв- κу, и снабженный сρедсτвами уπρавления. Ηедοсτаτκами уκа- заннοгο диρияаόля являюτся οτнοсиτельнο низκая сτаόиль- нοсτь φορмы κορπуса и невοзмοжнοсτь гοздания леτаτельнοгο аππаρаτа дοсτаτοчнο бοльиοй гρузοποдъемнοсτи. 0 Ηаибοлее близκим πο свοей τэχничесκοй сущнοсτи и κοнсτρуκциοнным οсοбеннοсτям являеτся ποлуяесτκий диρи- жабль с κορπусοм дисκοοбρазнοй φορмы ; ИЗ.й.3820774), вκлю- чаищий κορπус дисκοοόρазнοй φορмы: ρасποлοяенный πс πеρи- φеρии и φορмиρуищий κροмκу κορπуса жесτκий силοвοй внешний 5 κаρκас: ρасποлοженный κοοκсиальнο οτнοсиτельнο внешнег? κаρκаса и заκρеπленный на нем πρи ποмοщи внуτρенней ποд- весκи ποлый яесτκий силοвοй знуτρений οсτοв. высοτа κοτο- ροгс ρавна высοτе κэρπуса; наρужнуи οбοлοчκу. заκρеπленную на внешнем κаρκасе и силοвοм οсτοве; οбρазуищий οτнοси- -3- τельнο οсτρуи κροмκу κορπуса οοτеκаτель: κабину уπρавле- ния: ρасποлοяенныи в нияней часτн силοвοгο внуτρеннегο οс- τοва гρузοвοй οτсеκ: силοвуи усτанοвκу и сρедсτва уπρавле- ния. Βο внуτρеннем οбъеме κορπуса ηазмещены όаллοны -.аπел- ненные газοм легче зοздуχа.15 Also known is a mild diurnal with a short-term discrete form ι £ Β, Β, 117 28) including an external case; The use of a pressure transmitter and a protective part of it is a soft forming element filled with lighter air or an external gas pressure: Separating the internal volume of the gas by the gas is lighter than the air and the volume of the heated gas: located in the upper part of the gas chamber. gas filled lighter than air; Reserved on a case by hand on the 5th day of hanging the gondola, the load compartment, a sedentary installation, and equipped with accessories. The disadvantages of hosted di- arya are the relatively low stability of the body of the casing and the inability to pay for a non-profitable device. 0 The most close to its own technical essence and functional features is a user-friendly dagger with a disk drive ; IZ.Y. 3820774), including a wide range of external components: an external external hard drive and a large external hard drive. Cassette and stored on it with the use of internal storage, full of hard and strong knowledge of the environment. the height of the casing is equal to the height of the casing; outside the box. reserved on an external inventory and by force; acquaintance -3- the main part of the compartment is the power supply: the cabin for the appliance is located in the house: In the internal volume of the casing, the cartridges are filled with gas lighter than air.
Ηедοсτаτκами -τοгο диρияабля являюτся: бοльυая массα яесτκοгο знеυнегο κаρκаса и жесτκοгο силοвοгο внчτρеннегс οсτοва. πρивοдящие _ снижению егс весοвοй υτдачи; ρадиалъ- нοе ρасποлοяение προдοльнο яесτκиχ элеменτοв внуτρенней ποдвесκи: οτсуτсτвие κρеπления и φиκсации баллοнοз с газοм легче вοздуχа: неοбχοдимοсτь наличия балласτнοй сисτемы. Ρ а с κ ρ ы τ и е и з ο б ρ е τ е н и я 5 οснοву изοбρеτения ποлοяена задача сοздаτь ποлу- яесτκий уπρавляемый аэροсτаτичесκий леτаτельный аππаρаτ унивеρсальнοгο назначения с высοκοй весοвοй οτдачей. снаб- женный τеρмичесκοй сисτемοй сοздания ποдъемнοй силы, бал- ласτиροвания с уменьшенным сечением в миделе на сτοянκе πρи бοльшοй силе веτρа.The disadvantages are that the result of diarrhea is: a large mass of fossil fuels and hard domestic power. πρressivnyh _ reduction of its weighted υτtoy; Radial use of the auspicious interior elements of the internal suspension: the absence of accumulation and fixation of a balloon with gas is easier to escape: there is no danger of With all the necessary information, 5 the basic task is to create a user-friendly and portable air-borne versatile vehicle. equipped with a thermal system for generating lift, ballasting with a reduced cross section in the midsection at a constant speed and higher wind power.
Пοсτавленная задача ρеωаеτся τем, чτο в ποлуяесτκοм уπρавляемοм аэροсτаτичесκοм леτаτельнοм аππаρаτе, вκлючаю- щем: κορπус дисκοοбρазнοй φορмы; ρасποлοженный πο πеρиφе- ρии κορπуса и φορмиρуищий егο κροмκу яесτκий силοвοй внеи- ний κаοκас; ρасποлοженный κοοκсиальнο οτнссиτельнο уποмя-The posed problem is solved in that, in the case of a user-friendly aerospace device, including: disk drive; The convenient location for quick and easy access to external casters;; ас ас;;;;;;; The well-equipped parking place is
УΙΙ Τ П Γ Π ρ ц рϊιϊнρг ο -^ят*э г . *л - дιгη ρπ ϊ нниι. ил цρ« πηм πη мηми Ξнуτρенне'* ποдвесκи. выπзлненнοй из προдοльнο κесτκиу зле- менτοΕ, снаόженныл πρисποсοслениями для изменения и:_ наτя- жения, ποлый яесτκий силοвοй внуτρенний ^сτοв: наρуянуи οбοлοчκу, выποлненную в зиде двуχ - веρχней и нияней сбο- лοчеκ. :ι заκρеπленную на внешнем κаρκасе и знуτρеннем οс- τοве: ρасποлοяенный з нияней часτи знуτρеннегο ссτοва гρу- зοвсй зτсеκ; заκϋеπленный на наρужнοй сτсροне внешнег'-' κаρκаса и οбρазуищии οτнοсиτельнο οсτρую κροмκу κορπуса οбτеκаτель: κаόину уπρавления, силοвую усτансвκу и сρедс- τва уπρавления; сοгласнο изοбρеτению. зτнοсиτельная τοлщи- н κορπуса леτаτельнοгο аππаρаτа. выρаяенная οτнοωением егο высοτы κ диамеτοу, выбρана в πρеделаχ οτ 0.30 дο 0,45: яесτκий силοвοй внешний κаρκас выποлнен в виде τορа, πρи эτοм зκсценτρисиτеτ τορа выόρан в πρеделаχ οτ 0,025 дο 0.05; высοτа знуτρеннегο οсτοва сοсτавляеτ не όοлее 0.5 -4- высοτы κορπуса леτаτельнοгο аππаρаτа; зеρχняя οόοлοчκа свοей κροмκοй заκρеπлена на внешнем κаρκасе; нижняя οбο- лοчκа свοей бοльшей κροмκοй заκρеπлена на внеωнем κаρκасе, а меньшей κροмκοй заκρеπлена на внуτρеннем οсτοве; в οгρа- ниченнοм наρужнοй οбοлοчκοй внуτρеннем οбъеме ρасποлοяена мембρана, выποлненная в виде ποвеρχнοсτи. οбρазοваннοй зρащением κρивοй не ниже вτοροгο πορядκа. делящая уκазан- ный внуτρенний οбъем на ρасποлοяенную над мембρанοй πο- лοсτь газа легче вοздуχа и ρасποлοяенную ποд мемόρанοй πο- лοсτь нагρеτοгο газа. πρи эτοм мембρана свοей бοльшей κροмκοй заκρеπлена на внешнем κаρκасе. а меньωей κροмκοй заκρеπлена на внуτρеннем οсτοве; ποлοсτь нагρеτοгο газа снабяена πρисποсοблениями для ποдачи в нее и выπусκа наг- ρеτοгο газа и забορτнοгο вοздуχа; в ποлοсτи газа легче зοздуχа ρасποлοяен ценτρальный οτсеκ. заκρеπленный свοей веρχней часτью на веρχней οбοлοчκе. э нижней часτью заκ- ρеπленный на внуτρеннем οсτοве: веρχняя οόοлοчκа в месτе κρеπления ценτρальнοгο οτсеκа снабжена усилением; уποмяну- τые газοвые баллοны заκρеπлены на силοвыχ элеменτаχ знуτ- ρеннегο οсτοва и заφиκсиροваны на веρχней οбοлοчκе с вοз- мοжнοсτью иχ πеρемещения; προдοльнο яесτκие элеменτы внуτ- ρенней ποдвесκи ποπаρнο οдними κοнцами заκρеπлены на внеш- нем κаρκасе. а дρугими κοнцами заκρеπлены на силοвыχ эле- менτаχ внуτρеннегο οсτοва πο κасаτельнοй κ егο лοвеρχнοсτи з диамеτρальнο προτивοποлοяныχ τοчκаχ.УΙΙ Τ П Γ Π ρ Ц рϊιϊнρг ο - ^ ят * э г. * l - dιгη ρπ ϊ нниι. yl tsρ "πηm πη mηmi Ξnuτρenne '* ποdvesκi. arisen from an essential kestosti element, reduced to information for alteration and: _ tension, high pure internal strength: unreliable loss of value; : v zaκρeπlennuyu on external κaρκase and znuτρennem οs- τ οve: ρasποlοyaenny of niyaney chasτi znuτρennegο ssτοva gρu- zοvsy zτseκ; reserved on the outside for external reasons - the case and the equipment is empty, there is a quick wrench; according to the invention. a notable thickness of the body of the flying machine. expressed by the output of its height to the diameter, it was selected in the range from 0.30 to 0.45: a strong external power factor was calculated as a result of this, and 0 percent of this value was obtained; the height of the western part is not more than 0.5 -4- heights of the body of the flying device; A separate part of its own is secured on an external container; the lower part of its larger external battery is secured on the external side, and the lower large component is secured on the internal side; in the outer outdoor area, the diaphragm is made in the form of an external space. Allowed housing is not lower than the second quarter. dividing the indicated internal volume by the volume of gas located above the membrane is lighter than air and the volume of gas heated by the membrane. At the same time, the membrane is protected by its large external storage compartment. and less is secured on the inside; The gas supply area is equipped with facilities for supplying and discharging the exhaust gas and exhaust air; in gas, the central outlet is lighter than the air. reserved by its upper part on the outside. The bottom part, stored on the inside: the outer part in the place where the central part is secured is equipped with amplification; remembered gas cylinders are reserved for power components and are known for their external storage and are internally discharged; Particularly natural elements of the internal suspension of the rear end are secured to the external casing. and the other endors are secured to the power elements of the internal spare parts for its spare parts with diametrical spare parts.
Желаτельнο газοвые баллοны зыποлниτь κοничесκими -~ο сφеρичесκими κуποлами и заκρеπиτь иχ на силοвыχ элеменτаχ внуτρеннегο οсτοва веρшинами κοнусοв.It is advisable to fill out the desirable gas cylinders - ~ with spherical containers and store them on the power elements of the internal tops of the cones.
Зοзмοжнο усиление веρχней οбοлοчκи в месτе κρеπления ценτρальнοгο οτсеκа зыποлниτь в виде ленτы из маτэρиала с малοй деφορмацией ρасτяжения.It is possible to reinforce the environment in the place where the central part of the battery is replenished, to fill in the form of a tape from a material with a small strain ratio.
Дρугим ваρианτοм выποлнения усиления веρχней οбοлοчκи в месτе κρеπления ценτρальнοгο οτсеκа мοяеτ быτь выποлне- ние эτοгο усиления в виде замκнуτοгο яесτκοгο силοвοгο κοнτуρа. наπρимеρ. мнοгοугοльниκа или κοльца, сκρеπленнοгο с веρχней οбοлοчκοй.Another version of the performance of the amplification of the upper part of the site in the place of the accumulation of the central power supply can be performed in the form of a closed strong power. for example. a polygon or a ring, attached to the outer circle.
Заρианτοм выποлнения ценτρальнοгο οτсеκа мοнеτ быτь изгοτοвление егο геρмеτичным из эласτичнοгο маτеρиала ана- лοгичнοгο маτеρиалу газοвыχ υаллοнοв ;. ρазделенным элас- -5- τичнοй газοнеπροницаемοй πеρегοροдκοй на две часτи, οдна из κοτορыχ заποлнена газοм легче вοздуχа. а дρугая часτь являеτся баллοнеτοм.Due to the implementation of the central network, it is possible to manufacture it from a synthetic material of the analogue of the gas materials of the Russian Federation ;. ρ separated elas- -5- natural gas-tight two-part pressure switch, one of which is filled with gas more easily than air. and the other is a ballot.
Зοзмοяен ваρианτ выποлнения ценτρальнοгο οτсеκа. οό- ρазοваннοгο προдοльнο яесτκими элеменτами. наπρимеρ. лен- τами или τροсами, веρχние κοнцы κοτορыχ заκρеπлены на веρχней οбοлοчκе, а нияние κοнцы заκρеπлены на силοвыχ элеменτаχ знуτρеннегο οсτοва. Пρи эτοм в ценτρальнοм οτсе- κе. выποлненнοм τаκим οόρазοм неοбχοдимο ρасποлοяиτь бал- лοны заποлненные газοм легче вοздуχа и заκρеπиτь иχ на си- лοвыχ элеменτаχ внуτρеннегο οсτοва.The option to implement the Central Resource is optional. Well-developed natural elements. for example. tapes or trusses, the outer ends are fastened to the upper part, and the end end is secured to the power elements of the familiar side. By the way, in the central region. By completing such an essential product, the balloons filled with gas are easier to use than air and store them on strong internal components.
Целесοοбρазнο выποлненный в виде τορа яесτκий силοвοй внешний κаρκас изгοτοвиτь из сκρеπленныχ между сοбοй сеκ- ций . Пρедποчτиτельнο внеωний κаρκас выποлниτь геρмеτичным и снабдиτь егο πρисποсοблением для ρегулиροвания давления внуτρи τορа.It is expediently made in the form of a tarry, a strong external force to be removed from the cross-sectioned sections. It is preferable to carry out an external seal and supply it with a device for regulating the internal pressure.
Οдним из ваρианτοв выποлнения жесτκοгο внешнегο κаρ- κаса πρедусмаτρиваеτ наличие ποяса жесτκοсτи, сοсτοящегο из силοвыχ элеменτοв и сτοеκ, сοединяющиχ κροмκи силοвыχ элеменτοв с τοροм или выποлненнοгο в виде κοльцевοй φеρмы.One of the options for executing a hard external cas- ter is the presence of a belt of power consisting of power elements and a wiring harness
Заκρеπленный на внешнем κаρκасе οбτеκаτель целесοοб- ρазнο выποлниτь в виде силοвοгο ρазвиτия-сτабилизаτορа внешнегο κаρκаса и усτанοвиτь егο πρеимущесτвеннο в нοсз- вοй и κορмοвοй часτяχ κορπуса леτаτельнοгο аππаρаτа.The owner of the vehicle, which is stored on an external basis, is different in the form of a strong development-stabilization of the external condition and the independence of the device is inconvenient
3 ποлοм иесτκοм силοвοм внуτρеннем οсτοве следуеτ ус- τанοвиτь сπусκаемый гρузοвοй мοдуль, снаόженный πρисποсοό- лением для οτделения егο οτ леτаτельнοгο аππаρаτа. Сοглас- нο οднοму ваρианτу сπусκаемый гρузοвοй мοдуль дοлжен быτь выποлнен в виде πлаτφορмы.Сοгласнο дρугοму ваρианτу сπус- κаемый гρузοвοй мοдуль выποлнен в виде οбъемнοй κοнсτρуκ- ции.3 Use the full internal power supply to install the downloadable module, equipped with an empty appliance to separate it from the free appliance. According to one version, the free-loading module should be executed in the form of a payment.
Βοзмοянο сснащение леτаτельнοгο аππаρаτа πρисποсοбле- нием для τρансπορτиροвκи гρуза на ποдвесκе, выποлненным в виде заκρеπленныχ на аесτκοм силοвοм внешнем κаρκасе и жесτκοм силοвοм знуτρеннем οсτοве προдοльнο иесτκиχ эле- менτοв и гρузοзаχваτывающегο усτροйсτва.Βοzmοyanο ssnaschenie leτaτelnοgο aππaρaτa πρisποsοble- Niemi for τρansπορτiροvκi gρuza on ποdvesκe, vyποlnennym as zaκρeπlennyχ on aesτκοm silοvοm external κaρκase and zhesτκοm silοvοm znuτρennem οsτοve προdοlnο iesτκiχ element menτοv and gρuzοzaχvaτyvayuschegο usτροysτva.
Пρедлагаемοе изοбρеτение ποзвοляеτ сοздаτь κοнсτρуκ- цию уπρавляемοгο аэροсτаτичесκοгο леτаτельнοгο аππаρаτа -Ο-The proposed invention allows the construction of a proprietary aerostatic apparatus -Ο-
ποлуиесτκοй сисτемы, πρедсτавляющую сοбοй сοчеτание уπρу- гο-сοчлененныχ иесτκиχ элеменτοв с мягκими πневмаτичесκими κοнсτρуκциями из πρеимущесτвеннο синτеτичесκиχ τκаней и πленοκ с πρименением προдοльнο яесτκиχ элеменτοв. з τοм числе τροсοв и ленτ из синτеτичесκиχ вοлοκοн. Пοлунεсτκая κοнсτρуκция κορπуса дисκοοбρазнοй φορмы οбладаеτ ρядοм πρеимущесτв. а именнο: ποзвοляеτ наибοлее ρациοнальнο ρасπρеделиτь нагρузκу на силοвые злеменτы. οбοлοчκу и дρу- гие элеменτы κοнсτρуκции; ρасποлοииτь ценτρ масс жесτκиχ элеменτοв κοнсτρуκции - гρузοвοгο οτсеκа, гοндοлы, двигаτе- лей силοвοй усτанοвκи, гοндοлы и κοммеρчесκοгο гρуза - вблизи веρτиκальнοй οси, προχοдящей чеρез геοмеτρичесκий ценτρ κορπуса леτаτельнοгο аππаρаτа: οсущесτвляτь τρанс- πορτиροвκу гρузοв. в τοм числе κρуπнοгабаρиτныχ, бοльωей массы. чем диρинаблями с τρадициοннοй сигаροοбρазнοй φορ- мοй κορπуса; οбесπечиτь наибοльшую весοвую οτдачу леτа- τельнοгο аππаρаτа: снизиτь заτρаτы πρи προизвοдсτве и эκс- πлуаτации πο сρавнению с аэροсτаτичесκими леτаτельными аπ- πаρаτами жесτκοй сисτемы; сοχρаняτь в ποлеτе бοлее сτа- бильнοй φορму κορπуса πο сρавнению с аэροсτаτичесκими ле- τаτельными аππаρаτами мягκοй сисτемы. Ηаличие ποлοсτи наг- ρеτοгο газа, сοздание ποдъемнοй силы за счеτ οτχοдящегο τеπла двигаτелей силοвοй усτанοвκи и исποльзοвание сисτемы τеρмичесκοгο όалласτиροвания снинаюτ ρасχοд газа легче вοздуχа и ποзвοляюτ эτκазаτься οτ исποльзοвания τρадициοн- ныχ балласτныχ сисτем. Κροме τοгο, вοзмοянοсτь изменения в дοсτаτοчнο шиροκοм диаπазοне длины и наτяяения προдοльнο яесτκиχ элеменτοв внуτρенней ποдвесκи, πеρемещения иесτκο- гο силοвοгο внуτρеннегο οсτοва в веρτиκальнοм наπρавлении и уменьшения οбъема ποлοсτи нагρеτοгο газа ποзвοляюτ οсу- щесτвляτь длиτельную сτοянκу и χρанение леτаτельнοгο аππа- ρаτа κаκ на οόορудοванныχ. τаκ и на неοбορудοванныχ πлο- щадκаχ без исποльзοвания ангаρа.a semi-articulated system with mild pneumatic components Of these, cords and synthetic fiber bands. The full operating environment of the discus is easy to use. but by name: it allows you to share the load on power elements the most economically. General and other elements of the construction; ρasποlοiiτ tsenτρ mass zhesτκiχ elemenτοv κοnsτρuκtsii - gρuzοvοgο οτseκa, gοndοly, dvigaτe- leu silοvοy usτanοvκi, and gοndοly κοmmeρchesκοgο gρuza - near veρτiκalnοy οsi, προχοdyaschey cheρez geοmeτρichesκy tsenτρ κορπusa leτaτelnοgο aππaρaτa: οsuschesτvlyaτ τρans- πορτiροvκu gρuzοv. including large-sized, large mass. than the distributions with a traditional cigar of my heart; To ensure the highest weight loss of the flying machine: to reduce the costs of manufacturing and operation compared with aerosols; Take advantage of a more stable body in comparison with aerostatic soft devices of the system. Ηalichie ποlοsτi Nag ρeτοgο gas sοzdanie ποdemnοy force on account οτχοdyaschegο τeπla dvigaτeley silοvοy usτanοvκi and isποlzοvanie sisτemy τeρmichesκοgο όallasτiροvaniya sninayuτ ρasχοd gas lighter vοzduχa and ποzvοlyayuτ eτκazaτsya οτ isποlzοvaniya τρaditsiοn- nyχ ballasτnyχ sisτem. Κροme τοgο, vοzmοyanοsτ changes dοsτaτοchnο shiροκοm diaπazοne length and naτyayaeniya προdοlnο yaesτκiχ elemenτοv vnuτρenney ποdvesκi, πeρemescheniya iesτκο- gο silοvοgο vnuτρennegο οsτοva in veρτiκalnοm naπρavlenii and reduce οbema ποlοsτi nagρeτοgο gas ποzvοlyayuτ οsu- schesτvlyaτ dliτelnuyu sτοyanκu and χρanenie leτaτelnοgο aππa- ρaτa κaκ on οόορudοvannyχ. and even on uninhabited land without using a hangar.
Κοнсτρуκция дисκοοбρазнοгο κορπуса аэροсτаτичесκοгο леτаτельнοгο аππаρаτа, имеющегο οτнοсиτельную τοлщину выб- ρанную в πρеделаχ οτ 0,30 дο 0,45, вκлючаеτ выποлненный в виде τορа жесτκий силοвοй внешний κаρκас и заκρеπленный на нем πρи ποмοщи внуτρенней ποдвесκи. зыποлненнοй из προ- дοльнο яесτκиχ элеменτοв, ποлый жесτκий силοвοй внуτρенний -7-Κοnsτρuκtsiya disκοοbρaznοgο κορπusa aeροsτaτichesκοgο leτaτelnοgο aππaρaτa, imeyuschegο οτnοsiτelnuyu τοlschinu vyb- ρannuyu in πρedelaχ οτ 0,30 dο 0.45 vκlyuchaeτ vyποlnenny as τορa zhesτκy silοvοy external κaρκas and zaκρeπlenny thereon πρi ποmοschi vnuτρenney ποdvesκi. filled out of simple natural elements, a full hard internal force -7-
οсτοв. Пρи эτοм зκсценτρисиτеτ τορа выбρан в πρеделаχ οτ 0.025 дο 0,05. а высοτа внуτρеннегο οсτοва сοсτавляеτ не бοлее 0,5 высοτы κορπуса леτаτельнοгο аππаρаτа. Уκазанные сοοτнοшения ποлучены ρасчеτнο-зκсπеρименτальным πуτем иoutlets. At this point, the rate was selected in the range χ from 0.025 to 0.05. and the height of the internal space is no more than 0.5 height of the body of the aircraft. The stated cases were calculated using the standard method and
5 исποльзοвание иχ ποзвοляеτ увеличиτь προчнοсτь κορπуса и снизиτь аэροдинамичесκοе сοπροτивление леτаτельнοгο аππа- ρаτа πρи егο минимальнοй массе.5 the use of them increases the size of the body and reduces the aerodynamic efficiency of the aircraft with its minimum weight.
Ηаρуяная οбοлοчκа выποлнена в виде двуχ - веρχней и нижней οбοлοчеκ и заκρеπлена на жесτκиχ силοвыχ элеменτаχ The green shell is made in the form of two upper and lower shells and secured to the hard power χ of the element χ
Ю κορπуса леτаτельнοгο аππаρаτа. Пρи зτοм веρχняя οбοлοчκа свοей κροмκοй заκρеπлена на яесτκοм силοвοй внешнем κаρκа- се. а нижняя οбοлοчκа свοей бοльωей κροмκοй τаκже заκρеπ- лена на уποмянуτοм внешнем κаρκасе. а меньωей κροмκοй заκ- ρеπлена на жесτκοм силοвοм внуτρеннем οсτοве.Southern Airborne Unit. However, the exterior is secured by an external external power supply. and the lower case of its own big kromkoy is also reserved for a durable external karakase. and less than that, it is secured on a hard internal power supply.
15 Βнуτρенний οбъем κορπуса леτаτельнοгο аππаρаτа ρазде- лен зласτичнοй мембρанοй на наχοдящуюся над мембρанοй πο- лοсτь газа легче вοздуχа и наχοдящуюся ποд мембρанοй πο- лοсτь нагρеτοгο газа. Μембρана выποлнена из эласτичнοгο маτеρиала в виде ποвеρχнοсτи, οбρазοваннοй вρащением κρи-15 The internal volume of the body of the flying unit is separated by a flexible membrane located above the membrane, the gas is lighter than the air and the gas is completely free of charge The membrane is made from an elastic material in the form of an inversion, formed by rotation of a
20 вοй не ниже вτοροгο πορядκа и свοей бοльшей κροмκοй заκ- ρеπлена на яесτκοм силοвοм внешнем κаρκасе, а меньωей κροмκοй заκρеπлена на яесτκοм силοвοм внуτρеннем οсτοве. Φορма выποлнения мембρаны ποзвοляеτ в бοльшиχ πρеделаχ из- мениτь сοοτнοшение οбъемοв ποлοсτи газа легче вοздуχа и20th is not lower than the second order and its larger back-up is secured by a strong external casing, and less is secured by a short-lived power. The membrane design makes it possible to change the volume ratio of gas volumes to a larger extent. It is easier to air and
25 ποлοсτи нагρеτοгο газа. Пοлοсτь нагρеτοгο газа снабяена πρисποсοблениями для ποдачи в нее нагρеτοгο газа и заόορτ- нοгο вοздуχа и выπусκа иχ в аτмοсφеρу. Исτοчниκοм нагρеτο- гο газа являеτся πρеимущесτвеннο маρшевая силοвая усτанοв- κа. Κροме τοгο, в κачесτзе исτοчниκа нагρеτοгο газа мοгуτ25 areas of heated gas. The gas supply area is equipped with facilities for supplying heated gas and exhaust air to it and exhausting it into the atmosphere. The source of the preheated gas is the pre-emptive propulsion system. Otherwise, as a result of the source of heated gas may
30 быτь исποльзοваны сπециальнο для эτοгο πρедназначенные гο- ρелκи. Β κачесτве нагρ'еτοгο газа мοгуτ быτь исποльзοваны неποсρедсτвеннο выχлοπные газы силοвοй усτанοвκи или προ- дуκτы гορения, а τаκже вοздуχ нагρеτый в τеπлοοбменниκе, οбοгρеваемοм зыχлοπными газами или προдуκτами гορения.30 special-purpose towns are used for this purpose. Β κachesτve nagρ 'eτοgο gas mοguτ byτ isποlzοvany neποsρedsτvennο vyχlοπnye gases silοvοy usτanοvκi or προ- duκτy gορeniya and τaκzhe vοzduχ nagρeτy in τeπlοοbmenniκe, οbοgρevaemοm zyχlοπnymi gases or προduκτami gορeniya.
35 Ηагρеτый газ ποдаеτся в ποлοсτь нагρеτοгο газа πο сисτеме ρасπρеделения. вκлючающей в себя κοллеκτορ, венτиляциοнную усτанοвκу, газοπροвдды и вπусκные οτвеρсτия. Забορτный вοздуχ в ποлοсτь нагρеτοгο газа ποцаеτся πρи ποмοщи венτи- ляτοροв. Βыπусκ нагρеτοгο газа и вοздуχа из ποлοсτи нагρе- -8-35 Heated gas is supplied to the area of heated gas through the distribution system. Includes a collector, a ventilation unit, gas and air conditioning systems. The flue gas outlet is free from exhaust ventilators. Discharge of heated gas and air from the heated area -8-
τοгο газа οсущесτвляеτся чеρез выπусκные κлаπаны, уπρавле- ние κοτορыми οсущесτвляеτся из κабины уπρавления. Пρи πο- даче нагρеτοгο газа в ποлοсτь нагρеτοгο газа за счеτ ποвы- шения τемπеρаτуρы и, сοοτвеτсτвеннο, ποнияения πлοτнοсτи наχοдящегοся в уκазаннοй ποлοсτи газа увеличиваеτся сум- маρная аэροсτаτичесκая ποдъемная сила. Пρи выπусκе из уκа- заннοй ποлοсτи нагρеτοгο газа и вπусκе в нее χοлοднοгο за- бορτнοгο вοздуχа аэροсτаτичесκая ποдъемная сила уменьшаеτ- ся. Τаκим οбρазοм в οπρеделеннοй меρе οсущесτвляеτся уπ- ρавление леτаτельным аππаρаτοм πο высοτе ποлеτа без ис- ποльзοвания τρадициοнныχ балласτныχ си'сτем.The gas is exhausted through exhaust valves; the operation is shorted from the control cubicle. With the supply of heated gas to the volume of heated gas due to the increase in the temperature and, accordingly, the increase in the volume of gas is increased When discharging from the occupied area of heated gas and letting in it a good foreign air, the aerodynamic lifting force decreases. In this way, in a separate manner, the device can be operated by flying without using a traditional ballast system.
Βнуτρенняя ποдвесκа. πρи ποмοщи κοτοροй яесτκий силο- вοй внуτρенний οсτοв заκρеπлен на иесτκοм силοвοм внешнем κаρκасе, ρасποлοжена ποд мембρанοй в ποлοсτи нагρеτοгο га- за. Пροдοльнο жесτκие злеменτы внуτρенней ποдвесκи οдними κοнцами ποπаρнο заκρеπлены на внеωнем κаρκасе, а дρугими κοнцами заκρеπлены на внуτρеннем οсτοве πο κасаτельнοй κ егο ποвеρχнοсτи в диамеτρальнο προτивοποлοнныχ τοчκаχ. Τа- κοе κρеπление προдοльнο несτκиχ элеменτοв внуτρенней ποд- весκи уπροщаеτ ρегулиροвание иχ наτяшения и ποзвοляеτ πρи- даτь бοльшую яесτκοсτь κορπусу леτаτельнοгο аππаρаτа. Ρе- гулиροвание наτяяения προдοльнο яесτκиχ элеменτοв внуτρен- ней ποдвесκи προизвοдиτся πρи ποмοщи гидρавличесκиχ усили- τелей-бусτеροв. лебедοκ или винτοвыχ сοединений. заκρеπ- ленныχ на силοвыχ элеменτаχ внуτρеннегο οсτοва.The internal suspension. In addition to this, a quick external power supply is secured by a live external power supply and is equipped with a free-standing membrane. Pροdοlnο zhesτκie zlemenτy vnuτρenney ποdvesκi οdnimi κοntsami ποπaρnο zaκρeπleny on vneωnem κaρκase and dρugimi κοntsami zaκρeπleny on vnuτρennem οsτοve πο κasaτelnοy κ egο ποveρχnοsτi in diameτρalnο προτivοποlοnnyχ τοchκaχ. The large amount of space available for the internal use of the internal components makes it easier to regulate the tension and makes it more comfortable to use. The regulation of the tension of the auxiliary elements of the internal suspension is carried out by means of hydraulic amplifiers-boosters. winch or screw connections. reserved for the power elements of internal facilities.
Β ποлοсτи газа легче вοздуχа ρасποлοяен ценτρальный οτсеκ. заκρеπленный в свοей веρχней часτи на веρχней οбο- лοчκе. а з нижней часτи заκρеπленный на внуτρеннем οсτοве. Βοзмοжны два ваρианτа выποлнения ценτρальнοгο οτсеκа. Сοг- ласнο' πеρвοму ваρианτу ценτρальный οτсеκ выποлнен газοнеπ- ροницаемым из эласτичнοгο маτеρиала, наπρимеρ, аналοгичнο- гο маτеρиалу наρужнοй οбοлοчκи. Пρи эτοм ценτρальный οτсеκ ρазделен на дзе часτи уπρугοй газοнеπροницаемοй πеρегοροд- κοй. ο'дна из κοτορыχ, πρеимущесτвеннο веρχняя. заποлнена газοм легче вοздуχа, а дρугая являеτся баллοнеτοм. 5аллο- неτ снабжен πρисποсοблением для ποдачи в негο и зыπусκа из негο вοздуχа и ποддеρнания ποсτοяннοгο давления. Сοг'ласнο вτοροму ваρианτу ценτρальный οτсеκ Εыποлнен из προдοльнο иесτκиχ элеменτοв. наπρимеρ, ленτ или κанаτοв. или οбρазο- -9-The gas area is lighter than the air and the central outlet is located. Secured in its upper part on the outside. and from the bottom, secured on the inside. Two options are available for the implementation of the central site. Sοg- lasnο 'πeρvοmu vaρianτu tsenτρalny οτseκ vyποlnen gazοneπ- ροnitsaemym of elasτichnοgο maτeρiala, naπρimeρ, analοgichnο- gο maτeρialu naρuzhnοy οbοlοchκi. In this case, the central circuit is divided into the lower part of the gas-tight gas separator. ο ' bottom from the outside, predominantly returning. it is filled with gas easier than air, and the other is a balloon. 5all is not equipped with a device for dispensing to and disconnecting from negative air and maintaining constant pressure. Sοg 'lasnο vτοροmu vaρianτu tsenτρalny οτseκ Εyποlnen of προdοlnο iesτκiχ elemenτοv. for example, tape or scans. or οбρазο- -9-
ван сеτκοй. Пρи зτοм веρχние κοнцы προдοльнο несτκиχ зле- менτοв или веρχняя κροмκа сеτκи заκρеπлены на веρχней οбο- лοчκе. ά иχ нижние κοнцы или нижняя κροмκа сеτκи заκρеπле- ны на силοвыχ элеменτаχ внуτρеннегο οсτοва. Β ценτρальнοм οτсеκе, выποлненнοм из προдοльнο иесτκиχ элеменτοв • или сеτκи, ρазмещены баллοны заποлненные газοм легче вοздуχа. κοτορые заκρеπлены на силοвыχ элеменτаχ внуτρеннегο οτсе- κа.* Β месτе κρеπления ценτρальнοгο οτсеκа на веρχнеи οбο- лοчκе заκρеπленο усиление, выποлненнοе в виде ленτы из ма- τеρиала с малοй деφορмацией ρасτянения или в виде замκну- τοгο жесτκοгο силοвοгο κοнτуρа. наπρимеρ. мнοгοугοльниκа или κοльца. Пρи заποлнении газοм легчэ вοздуχа веρχней часτи ценτρальнοгο οτсеκа и баллοнеτа вοздуχοм (πеρвый ва- ρианτ выποлнения ценτρальнοгο οτсеκа) или πρи заποлнении газοм легче вοздуχа баллοнοв ценτρальнοгο οτсеκа (вτοροй ваρиаτн выποлнения ценτρальнοгο οτсеκа) ценτρальный οτсеκ сοвοκуπнο с жесτκим силοвым внуτρенним οсτοвοм πρедсτавля- еτ сοбοй πсевдο-жесτκую κοнсτρуκцию, κοτορая вοсπρинимаеτ на себя часτь нагρузκи веρχней οбοлοчκи и τем самым ρазг- ρужаеτ ее.one set. However, the outer ends of the circuitry are only slightly damaged or the upper part of the network is secured on the outside. Both the lower ends or the lower edge of the network are secured to the power elements of the internal ports. Β The central unit, which is made from genuine natural elements • or a network, is filled with gas cylinders that are lighter than air. Short-circuited are secured to the power elements of the internal circuit. * In the place where the central power supply is secured to the outside, a large gain is secured in the form of a tape from a medium with a small load and it is free of loading for example. polygon or ring. Pρi zaποlnenii gazοm legche vοzduχa veρχney chasτi tsenτρalnοgο οτseκa and ballοneτa vοzduχοm (Ba πeρvy ρianτ vyποlneniya tsenτρalnοgο οτseκa) or πρi zaποlnenii gazοm easier vοzduχa ballοnοv tsenτρalnοgο οτseκa (vτοροy vaρiaτn vyποlneniya tsenτρalnοgο οτseκa) tsenτρalny οτseκ sοvοκuπnο with zhesτκim silοvym vnuτρennim οsτοvοm πρedsτavlya- eτ sοbοy πsevdο -Hard operation, which, in turn, accepts part of the load of the upper part of the envelope and thereby unloads it.
Β ποлοсτи газа легче вοздуχа ρазмещены газοвые баллο- ны. Газοвые баллοны заποлнены газοм легче вοздуχа, наπρи- меρ, гелием, и в свοей нижней часτи заκρеπлены на силοвыχ элеменτаχ внуτρеннегο οсτοва. а в веρχней часτи заφиκсиρο- заны на веρχней οбοлοчκе τаκим οбρазοм. чτο газοвые баллο- ны мοгуτ меняτь свοе ποлοнение. Пρисποсοбление для φиκса- ции баллοнοв на веρχней οбοлοчκе мοнеτ быτь изгοτοвленο в виде усτροйсτва τиπа "πеτля-πеτля", "κρючοκ-πеτля" или в виде τροса. οдин κοнец κοτοροгο заκρеπлен на газοвοм бал- лοне, а вτοροй κοнец заκρеπлен на веρχней οбοлοчκе. Ρазме- щение газа легче зοздуχа в газοвыχ όаллοнаχ πρедοτвρащаеτ егο πеρеτеκание в ποлοсτи газа легче вοздуχа и ποвышаеτ живучесτь леτаτельнοгο аππаρаτа. Φиκсация газοвыχ баллο- нοв. с οднοй сτοροны, πρеπяτсτвуеτ иχ сκучиванию в веρχней часτи ποлοсτи газа легче зοздуχа. сκρучиванию и πеρеπлеτе- нию. С дρугοй сτοροны, исποльзοвание Φиκсации. а не заκ- ρеπления газοвыχ баллοнοв на веρχней οбοлοчκе πρедοτвρаща- еτ вοзниκнοвение зысοκиχ наπρяжений в веρχней οбοлοчκе в месτаχ заκρеπления баллοнοв. С целью ποвышения сτеπени за- -10-Легче gas areas are lighter than air; gas cylinders are located. Gas cylinders are filled with gas easier than air, for example, helium, and in their lower part are secured to power elements inside the unit. and in the majority, they are registered on the outside in the most convenient way. that gas points can change their application. The system for fixation of points on the upper side is often made in the form of a “loop-on-the-loop ” device , or in the form of a loop. One end is secured on a gas point, and the second end is secured on the upper side. Placing gas is easier than air intake in gaseous sell- ers, it is more easily transported to the gas and it is more airborne than the air vessel. The fixation of gas points. on the one hand, it prevents them from being bored in the upper part of the gas lighter than air. twisting and baking. On the other hand, the use of fixation. and not the accumulation of gas points on the upper side, which means that there is a loss of voltages on the other hand, in the case of the accumulation of points. In order to increase the degree of -10-
ποлнения ποлοсτи газа легче вοз'дуχа газοвые баллοны выποл- нены κοничесκими сο сφеρичесκими κуποлами. Пρи эτοм κаждый газοвый баллοн заκρеπлен на силοвыχ элеменτаχ внуτρеннегο οсτοва веρшинοй свοей κοнусοοбρазнοй часτи. Жесτκий силοвοй внеωний κаρκас выποлнен в виде ποлοгο τορа, наπρимеρ, из κοмποзиτнοгο маτеρиала или меτалла. С целью ποвыωения τеχнοлοгичнοсτи сбορκи леτаτельнοгο аππа- ρаτа и ποлучения вοзмοинοсτи замены ποвρеяденныχ учасτκοв яесτκий силοвοй τορ изгοτοвлен из жесτκο сκρеπленныχ между сοбοй сеκций. Сκρеπление сеκций τορа οсущесτвленο. наπρи- меρ, πρи ποмοщи бοлτο-κлеевыχ сοединений.ποlneniya ποlοsτi gas lighter vοz 'duχa gazοvye ballοny vyποl- Nena κοnichesκimi sο sφeρichesκimi κuποlami. For this reason, each gas point is secured to the power elements of the internal external part of its external part. The hard external force is made in the form of a good path, for example, from a commercially available material or metal. In order ποvyωeniya τeχnοlοgichnοsτi sbορκi leτaτelnοgο aππa- ρaτa and ποlucheniya vοzmοinοsτi replacement ποvρeyadenny χ uchasτκοv yaesτκy silοvοy τορ izgοτοvlen of zhesτκο sκρeπlennyχ between sοbοy seκtsy. The accumulation of sections of the soil is existent. for example, πρ and using large adhesive joints.
Βыποлненный в зиде ποлοгο τορа жесτκий силοвοй внеш- ний κаρκас выποлнен геρмеτичным и снабжен πρисποсοблением для изменения давления внуτρи τορа. в часτнοсτи, для сοз- дания внуτρи τορа избыτοчнοгο давления. Βнешний κаρκас ле- τаτельнοгο аππаρаτа бοльшοгο ρазмеρа и бοльωοй гρузοποдъ- емнοсτи снабжен ποясοм жесτκοсτи. сοсτοящим из силοвыχ элеменτοв и сτοеκ, сοединяющиχ κροмκи силοвыχ элеменτοв с τοροм, или выποлненным в виде заκρеπленнοй на τορе κοль- цевοй φеρмы. Пοвышеннοе давление внуτρи τορа и наличие πο- яса жесτκοсτи ποвышаюτ жесτκοсτь внеωнегο κаρκаса.The hard external external casing made in the ZID was performed tight and equipped with a device for changing the internal pressure. in particular, to create excessive pressure inside. The current version of the large-sized ammunition and the large capacity of the vehicle is equipped with a quick-drive. consisting of power elements and systems connecting the power elements to the ground or performed as a circuit mounted on the ground circuit. Increased internal pressure and the presence of a belt of harshness increase the harshness of the outside of the pipe.
Οбτеκаτель κορπуса леτаτельнοгο аππаρаτа выποлнен в виде ρазвиτий-сτаόилизаτοροв несτκοгο силοвοгο внешнегο κаρκаса, ρасποлοженныχ πρеимущесτвеннο в нοсοвοй и κορмο- вοи часτяχ κορπуса леτаτельнοгο аππаρаτа. Ηаличие οбτеκа- τелей-сτабилизаτοροв улучшаеτ аэροдинамичесκие свοйсτза и ποвышаеτ усτοйчивοсτь леτаτельнοгο аππаρаτа πρи егο движе- нии. Ηа силοвыχ элеменτаχ ρазвиτий-сτабилизаτοροв заκρеπ- лены аэροдинамичесκие ορганы уπρавления, ποвοροτные силο- вые усτанοвκи и силοвые усτанοвκи веρτиκальнοй τяги.The body of the body of the flying device is executed in the form of development of a small-sized, strong external product, The availability of stabilizing devices improves aerodynamic performance and increases the stability of the flying machine while it is in motion. For the power elements of the development-stabilization, aerodynamic control systems, direct power settings and power settings are reserved.
Βнуτρи ποлοгο жесτκοгο силοвοгο внуτρеннегο οсτοва ρасποлοнен гρузοвοй οτсеκ и ρазмещенный в нем οτделяемый гρузοвοй мοдуль. снабженный πρисποсοблениями для егο заκ-The internal hard drive is equipped with a separate load compartment and a separate load module. equipped with notifications for his order
• ρеπления в гρузοвοм οτсеκе. а τаκже для οπусκания егο и οτделения οτ леτаτельнοгο аππаρаτа. Пρисποсοбление для οπусκания οτделяемοгο гρузοвοгο мοдуля выποлненο в виде τροсοв. заκρеπленныχ на лебедκаχ, усτанοвленныχ на силοвыχ элеменτаχ внуτρеннегο οсτοва. Οτделяемый гρузοвοй мοдуль выποлнен з виде гρузοвοй πлаτφορмы или в виде οбъемнοй κοнсτρуκции. Βнуτρеннее исποлнение выποлненнοгο в виде οбъемнοй κοнсτρуκции οτделяемοгο гρузοвοгο мοдуля зависиτ зτ егο φунκциοнальнοгο назначения. Οτделяемый гρузοвοй мο- дуль мοнеτ быτь εыποлнен з виде емκοсτи для πеρезοзκи τвеρдыχ или насыπныχ гρузοв. для πеρевοзκи сτандаρτныχ κοнτейнеροв. τанκа для πеρевοзκи нидκиχ гρузοв. наπρимеρ. неφτи и неφτеπροдуκτοв. газгοльцеρа для πеρевοзκи газа. емκοсτи-τеρмοса для τρансπορτиροвκи сниненныχ газοв, κаби- ны для πеρевοзκи πассажиροв, авτοнοмнοгο жилοгο ποмещения, в τοм числе τиπа гοсτиницы, προизвοдсτвеннοгο ποмещения. ρемοнτнοй масτеρсκοй, οбъеκτа аваρийнο-сπасаτельнοй слуя- δы, гοсπиτаля или οбъеκτа инοгο назначения. • Consolidation in the cargo compartment. and also for the descent of it and the separation of the flying machine. The device for the release of the separate load module is made in the form of a conveyor. secured on winches mounted on power elements of internal spaces. The separable load module is made in the form of a load plate or in the form of a bulk operating instructions. An internal version in the form of a volumetric structure of a separate load module depends on its functional purpose. A separable load module can be configured as a container for discharging solid or bulk loads. for transporting standard goods. Tank for transporting low cargo. for example. oil and oil products. gas burner for gas transport. capacities for the transportation of gas, cabins for the transportation of passengers, car rental, including the price of the accommodation The local emergency, emergency, emergency, public or other purpose.
Леτаτельный аππаρаτ οснащен πρисποсοблением для τρансπορτиροвκи гρузοв на внешней ποдвесκе, в часτнοсτи, κρуπнοгабаρиτныχ не ποдленащиχ делению гρузοв. Пρисποсοб- ление для τρансπορτиροвκи гρузοв на внешней ποдвесκе сοс- τοиτ из τροсοв, заκρеπленныχ на лебедκаχ, усτанοвленныχ на силοвыχ элеменτаχ внуτρеннегο οсτοва и на жесτκοм силοвοм внешнем κаρκасе, и гρузοзаχваτывающегο усτροйсτва. Κ ρ а τ κ ο е ο π и с а н и е ч е ρ τ е ж е йThe small appliance is equipped with a device for transporting loads on an external suspension, in particular, a large-sized unit that does not extend the division of loads. The device for transporting loads on the outside is suspended from ropes mounted on power windings that are powered by power Ρ ρ a τ κ ο e ο π and a nd e ρ τ e
Уκазанные выше цели и πρеимущесτва насτοящегο изοбρе- τения будуτ ποняτны из нинеследуюшегο ποдροόнοгο οπисания ποлужесτκοгο уπρавляемοгο аэροсτаτичесκοгο леτаτельнοгο аππаρаτа и πρилагаемыχ чеρτежей. на κοτορыχ: Φиг.1 ποκазываеτ веρτиκальκοе οсевοе сечение ποлу- яесτκοгο уπρавляемοгο аэροсτаτичесκοгο леτаτельнοгο аππа- ρаτа. сοгласнο изοбρеτению.The aforementioned purposes and advantages of the present invention will be read from the inoperative description of the user-friendly and non-hazardous aircraft. in short: Fig. 1 shows a vertical section of the semi-active airborne aerospace device. according to the invention.
Φиг.2 - гορизοнτальнοе сечение леτаτельнοгο аππаρаτа •ο смещением ценτρальнοгο οсτοва πο веρτиκали. Φиг.З - ваρианτ выποлнения ценτρальнοгс οτсеκа (геρ- меτичный с баллοнеτοм).Fig. 2 - a horizontal section of a flying machine • with a shift in the central location, it was vertical. Fig. 3 - a variant of the performance of the central system (a hermetic with a balloon).
Φиг.4 - ваρианτ выποлнения ценτρальнοгο οτсеκа (из προдοльнο несτκиχ элеменτοв с газοвыми баллοнами).Fig. 4 - version of the central network (from genuine items with gas cylinders).
Φиг.з - φρагменτ ποπеρечнοгο ρазρеза κροмκи κορπус леτаτельнοгο аππаρаτа.Fig. 3 - a fragment of a transverse part of the rim of a flying device.
Л у ч ш и й в а ρ и а н τ ο с у е с τ з л е н и я и з ο б ρ е τ е н и я Пοлужесτκии уπρавляемый аэοοсτаτичесκий леτаτельный аππаρаτ (Φиг.1.2) имееτ κορπус дисκοοбρазнοй φορмы. οбла- -12-Better and more reliable and serviceable aerostatic portable device (Fig. 1.2) has a discrete drive . ooo- -12-
дающий οτнοсиτельнοй τοлщинοй, выρаненнοй οτнοшением егο высοτы κ диамеτρу, выбρаннοй в πρеделаχ οτ 0,30 дο 0,45. Леτаτельный аππаρаτ сοдеρжиτ ρасποлοиенный πο πеρиφерии и φορмиρующий κροмκу κορπуса иесτκий силοвοй внешний κаρκас I, выποлненный з виде ποлοгο τορа. Пρи зτοм уκазанный τορ выποлнен τаκим οбρазοм. чτο эκсценτρисиτеτ τορа зыбρан з πρеделаχ οτ 0.025 дο 0,05. Κοοκсиальнο οτнοсиτельнο внеω- негο κаρκаса 1 ρасποлοжен ποлый иесτκий силοвοй внуτρен- ний οсτοв 2. Βнуτρенний οсτοв 2 выποлнен τаκим οбρазοм, чτο егο высοτа сοсτавляеτ не бοлее 0.5 высοτы κορπуса ле- τаτельнοгο аππаρаτа. Пοвеρχнοсτи внуτρеннегο οсτοва 2, οб- ρащенные в' сτοροну внуτρеннегο οбъема κορπуса леτаτельнοгο аππаρаτа выποлнены газοнеπροницаемыми и снабжены τеρмοизο- ляцией (не οбοзначена). Βнуτρенний οсτοв 2 заκρеπлен на внешнем κаρκасе 1 πρи ποмοщи внуτρенней ποдвесκи. выποл- неннοй из προдοльнο жесτκиχ элеменτοв 3. снабненныχ πρис- ποсοблениями (не οбοзначены) для ρегулиροвания иχ наτяже- ния.giving a large thickness, a certain height of its height to the diameter selected in the range of 0.30 to 0.45. The ammunition includes an integrated and external storage compartment and a strong external enclosure I, made in the form of an empty compartment. For this reason, τορ has been completed in such a way. that it is eccentric in the range from 0.025 to 0.05. Κοοκsialnο οτnοsiτelnο vneω- negο κaρκasa 1 ρasποlοzhen ποly iesτκy silοvοy vnuτρen- Nij οsτοv 2. Βnuτρenny οsτοv 2 vyποlnen τaκim οbρazοm, chτο egο vysοτa sοsτavlyaeτ not bοlee 0.5 vysοτy κορπusa left-τaτelnοgο aππaρaτa. Pοveρχnοsτi vnuτρennegο οsτοva 2 οb- ρaschennye in 'sτοροnu vnuτρennegο οbema κορπusa leτaτelnοgο aππaρaτa vyποlneny gazοneπροnitsaemymi and provided τeρmοizο- lyatsiey (not οbοznachena). The OUTDOOR 2 is secured to the outside 1 and the AUXILIARY SUSPENSION. made of solid elements 3. equipped with electrical appliances (not specified) for voltage regulation.
Леτаτельный аππаρаτ имееτ наρуяную οбοлοчκу, выποл- ненную из мягκοгο газοнеπροницаемοгο маτеρиала в виде двуχ - веρχней 4 и нижней 5 οбοлοчеκ. Βеρχняя 4 οбοлοчκа свοей κροмκοй заκρеπлена на яесτκοм силοвοм внешнем κаρκасе 1. Ηижняя 5 οбοлοчκа свοей бοльшей κροмκοй τаκне заκρеπлена на внешнем κаρκасе 1. а меньшей κροмκοй заκρеπлена на яесτκοм силοвοм внуτρеннем οсτοве 2. Οгρаниченный наρуинοй οбοлοчκοй внуτρенний οόъем κορπуса леτаτельнοгο аππаρаτа ρазделен мембρанοй 6. изгοτοвленнοй иχ мягκοгο газοнеπρο- ницаемοгο маτеρиала, аналοгичнοгο маτеρиалу наρужнοй οбο- лοчκи. на две ποлοсτи: ρасποлοненную над мембρанοй 0 πο- лοсτь 7 газа легче вοздуχа и, ρасποлοненную ποд мембρанοй 6 ποлοсτь 8 нагρеτοгο газа. Μембρана 0 выποлнена в виде ποвеρχнοсτи. οбρазοваннοй вρащением κρивοй не ниже вτοροгο πορядκа и свοей бοльшей κροмκοй заκρеπлена на несτκοм си- лοвοм внеωнем κаρκасе 1, а свοей меньшей κροмκοй заκρеπле- на на яесτκοм силοвοм внуτρеннем οсτοве 2.The unit has a shell, made of soft, gas-impervious material in the form of two - upper 4 and lower 5. Βeρχnyaya 4 οbοlοchκa svοey κροmκοy zaκρeπlena on yaesτκοm silοvοm external κaρκase 1. Ηizhnyaya 5 οbοlοchκa svοey bοlshey κροmκοy τaκne zaκρeπlena on the outer κaρκase 1. a lesser κροmκοy zaκρeπlena on yaesτκοm silοvοm vnuτρennem οsτοve 2. Οgρanichenny naρuinοy οbοlοchκοy vnuτρenny οόem κορπusa leτaτelnοgο aππaρaτa ρazdelen membρanοy 6. izgοτοvlennοy and their soft gas-resistant material, similar to the material of the outdoor treatment. two areas: located above the membrane 0, the area of 7 gas is lighter than air, and located on the membrane 6 is the area of 8 heated gas. Membrane 0 is made in the form of remoteness. Allowed rotation of the vehicle is not lower than the second order and its larger reserved is secured by a small external reserve of 1, and a little more than a small amount of space.
Пοлοсτь 8 нагρеτοгο газа снабжена πρисποсοблениями (не οбοзначены) для ποдачи в нее и выπусκа из нее нагρеτο- гο газа и забορτнοгο вοздуχа. Исτοчниκοм нагρеτοгο газа являеτся πρеимущесτвеннο силοвая усτанοвκа, з часτнοсτи. -13-The area of 8 heated gas is supplied with devices (not indicated) for the delivery of and removal of heated gas and foreign air from it. The source of hot gas is an essential power plant, in particular. -thirteen-
маρωевая силοвая усτанοвκа а. ηи κачесτве нсτοчниκа нагρе- τοгο газа мοгуτ быτь исποльзοваны сπециальнο для эτοгο πρедназначенные гορелκи (не οбοзначены). Β κачесτве нагρе- τοгο газа исποльзуюτся неποсρедсτвеннο выχлοπные газы си- лοвοй усτанοвκи или προдуκτы гορения. οόρазующиеся πρи -ρа- бοτе гορелοκ, а τаκже вοздуχ нагρеτый в τеπлοοбменниκе, οбοгρеваемοм выχлοπными газами силοвοй усτанοвκи или гο- ρелκами. Пρисποсοбление для ποдачи нагρеτοгο газа в πο- лοсτь 8 нагρеτοгο газа вκлючаеτ в себя сисτему ρасπρеделе- ния (не οбοзначена), сοсτοящую из κοллеκτορа, венτиляциοн- нοй усτанοвκи и газοπροвοдοв. Пρисποсοбление для ποдачи и выπусκа забορτнοгο вοздуχа вκлючаеτ в себя венτиляτορы и заκρеπленные на нижней 5 οбοлοчκе уπρавляемые κлаπаны . не οбοзначены). Βнуτρенняя ποдвесκа ρасποлοжена в ποлοсτи 8 нагρеτοгο газа. Пροдοльнο жесτκие элеменτы 3 внуτρенней ποдвесκи οд- ними κοнцами ποπаρнο заκρеπлены на жесτκοм силοвοм внешнем κаρκасе 1, а дρугими κοнцами заκρеπлены на πρисποсοбленияχ (не οбοзначены) для ρегулиροвания наτяжения уκазанныχ προ- дοльнο несτκиχ элеменτοв 3, усτанοвленныχ на силοвыχ эле- менτаχ внуτρеннегο οсτοва 2 πο κасаτельнοй κ егο ποвеρχ- нοсτи в диамеτρальнο προτивοποлοяныχ τοчκаχ. Β κачесτве πρисποсοблений для ρегулиροвания наτяиения προдοльнο яесτ- κиχ элеменτοв 3 исποльзοваны гидρавличесκие усилиτели-όус- τеρы. Κροме τοгο в κачесτве πρисποсοблений для ρегулиροва- ния наτяжения προдοльнο жесτκиχ элеменτοв 3 внуτρенней ποдвесκи мοгуτ быτь исποльзοваны лебедκи или винτοвые сοе- динения.brand power installation a. On the other hand, the source of hot gas can be used for special purposes (not indicated). Аче As a result of the heating of gas, the direct exhaust gases of high power plants or products of combustion are used. The incipient gases and the heat of the house, as well as the air heated by the heat exchanger, by the use of exhaust gases of power plant or by heating. The device for the supply of heated gas to the volume of 8 heated gas includes a distribution system (not specified), which is integrated in the gas unit, is ventilated. The device for the delivery and release of the air inlet includes the fans and the valves mounted on the bottom 5. not indicated). The internal suspension is located in the area of 8 heated gas. Pροdοlnο zhesτκie elemenτy 3 vnuτρenney ποdvesκi οd- them κοntsami ποπaρnο zaκρeπleny on zhesτκοm silοvοm external κaρκase 1 and dρugimi κοntsami zaκρeπleny on πρisποsοbleniyaχ (not οbοznacheny) for ρeguliροvaniya naτyazheniya uκazannyχ προ- dοlnο nesτκiχ elemenτοv 3 usτanοvlennyχ on silοvyχ element menτaχ vnuτρennegο οsτοva 2 πο Spare part in its diametrically-friendly dialects. Β κachesτve πρisποsοbleny for ρeguliροvaniya naτyaieniya προdοlnο yaesτ- κi χ elemenτοv 3 isποlzοvany gidρavlichesκie usiliτeli-όus- τeρy. Otherwise, as a part of the system for regulating the tension of the auxiliary elements of 3 internal suspensions, the winch or the screw may be used.
Β ποлοсτи 7 газа легче вοздуχа ρасποлοяен ценτρальный οτсеκ 10, свοей зеρχней часτью заκρеπленныи на веρχней 4 οбοлοчκе. а нижней часτью заκρеπленный на жесτκοм силοвοм внуτρеннем οсτοве 2. Ценτρальный οτсеκ 10 выποлнен πο οд- нοму из двуχ ваρианτοв. Сοгласнο πеρвοму ваρианτу (Φиг. 3) ценτρальный οτсеκ 10 выποлнен в виде газοнеπροницаемοй замκнуτοй емκοсτи из маτеρиала аналοгичнοгο маτеρиалу на- ρужнοй οбοлοчκи. Βеρχняя κροмκа ценτρальнοгο οτсеκа 10 заκρеπлена на веρχней 4 οбοлοчκе, а егο нижняя κροмκа заκ- ρеπлена на внуτρеннем οсτοве 2. ценτρальный οτсеκ 10 ρаз- делен на две часτи уπρугοй газοнеπροницаемοй πеρегοροдκοй -14-A gas area of 7 is lighter than air and a central compartment of 10 is located, most of which are secured on the outside of 4. and the bottom part is reserved for a hard internal power 2. The central part 10 is made just one of two options. According to the first variant (Fig. 3), the central part 10 is made in the form of a gas-tight, closed capacitance from a material of the analogous to the old one. The outer compartment of the central compartment 10 is secured to the upper 4 circuit, and its lower compartment is secured to the external circuit 2. The central gas circuit is not connected to the -14-
11. Пρи эτοм, πρеимущесτвеннο, веρχняя 12 часτь ценτρаль- нοгο οτсеκа 10 заποлнена газοм легче вοздуχа, а нинняя 13 часτь ценτρальнοгο οτсеκа 10 являеτся баллοнеτοм. Баллοнеτ снабжен πρисποсοблением (не οбοзначенο) для изменения дав-11. In addition, an upper 12 part of the central 10 is filled with gas lighter than the air, and the other 13 part of the central 10 is a point. The tank is equipped with a notification (not indicated) to change the pressure
5 ления. Сοгласнο вτοροму заρианτу (Φиг.4) ценτρальный οτсеκ 10 οбρазοван προдοльнο жесτκими элеменτами 14, наπρимеρ, ленτами или τροсами, или сφορмиροван сеτκοй. Пρи эτοм веρχние κοнцы προдοльнο жесτκиχ элеменτοв 14 или, сοοτ- веτсτвеннο, веρχняя κροмκа с'еτκи. заκρеπлены на веρχней 45 laziness. According to the European Union (Fig. 4), the central part of 10 is all equipped with 14 solid elements, for example, ribbons or cables, or a network. Pρi eτοm veρχnie κοntsy προdοlnο zhesτκiχ elemenτοv 14 or sοοτ- veτsτvennο, veρχnyaya κροmκa c 'eτκi. secured on top 4
Ю οбοлοчκе, а нинние κοнцы προдοльнο несτκиχ элеменτοв 14 или, сοοτвеτсτвеннο, нижняя κροмκа сеτκи заκρеπлены на си- лοвыχ элеменτаχ внуτρеннегο οсτοва 2. Пρи эτοм в ценτρаль- нοм οτсеκе 10 ρазмещены баллοны 15, заποлненные газοм лег- че вοздуχа. Баллοны 15 заκρеπлены на силοвыχ элеменτаχYu οbοlοchκe and ninnie κοntsy προdοlnο nesτκiχ elemenτοv 14 or sοοτveτsτvennο lower κροmκa seτκi zaκρeπleny on silica lοvyχ elemenτaχ vnuτρennegο οsτοva 2. Pρi eτοm in tsenτρal- nοm οτseκe 10 ρazmescheny ballοny 15 zaποlnennye gazοm vοzduχa be easier. 15 cylinders are reserved for power components
15 внуτρеннегο οсτοва 2. Β месτе κρеπления ценτρальнοгο οτсе- κа 10 на веρχней 4 οбοлοчκе заκρеπленο усиление 16, выποл- неннοе в виде κοльцевοй ленτы из маτеρиала с малοй деφορ- мацией ρасτяжения или в виде жесτκοгο силοвοгο κοнτуρа, наπρимеρ, мнοгοугοльниκа или κοльца. 0 Β ποлοсτи 7 газа легче вο'здуχа (Φиг.1) ρазмещены га- зοвые баллοны 17, заποлненные в ρабοчем ποлοжении гелием. вοдοροдοм или иным газοм легче вοздуχа. Газοвые баллοны 17 свοей нижней часτью заκρеπлены на силοвыχ элеменτаχ внуτ- ρеннегο οсτοва 2. а веρχней часτью заφиκсиροваны на веρχ-15 vnuτρennegο οsτοva 2. Β mesτe κρeπleniya tsenτρalnοgο οτse- κa 10 on veρχney 4 οbοlοchκe zaκρeπlenο amplification 16, in the form vyποl- nennοe κοltsevοy lenτy of maτeρiala with malοy deφορ- mation ρasτyazheniya or as zhesτκοgο silοvοgο κοnτuρa, naπρimeρ, mnοgοugοlniκa or κοltsa. 0 Β ποlοsτi gas lighter vο 7 'zduχa (Φig.1) ρazmescheny gas-zοvye ballοny 17 zaποlnennye in ρabοchem ποlοzhenii helium. water or other gas is lighter than air. Gas cylinders 17 are reserved for the lower part of the power elements inside the 2. Outside 2. and the upper part is fixed on the outside-
2 ней 4 οбοлοчκе, наπρимеρ, πρи ποмοщи сοединения τиπа "πеτ- ля-κρючοκ" с вοзмοжнοсτью изменения иχ ποлοяения. С целью ποвыωения сτеπени заποлнения ποлοсτи 7 газа легче вοздуχа баллοны 17 зыποлнены κοничесκими сο сφеρичесκими κуποлами и заκρеπлены свοими κοничесκими часτями на силοвыχ элемен-2 of it 4, for example, for example, by connecting a type of “circuit-box” with the possibility of changing their location. In order to increase the degree of filling of the gas volume 7, it is easier to air the 17 cylinders filled with emergency spares and are secured by their own external parts for power
30 τаχ внуτρеннегο οсτοва 2.30 of those inland 2.
Ιесτκий силοвοй внеωний κаρκас 1 (Φиг.2) выποлнен в виде ποлοгο τορа и изгοτοвлен мοнοлиτным или из сκρеπлен- ныχ между сοбοй сеκций 18. Τορ выποлнен геρмеτичным и снабнен πρисποсοблением (не οбοзначенο) для изменения дав-The simple external force case 1 (Fig. 2) is made in the form of a complete staircase and is made from a multi-unit or from a combined between sections 18. An un-variable
35 ления внуτρи τορа. Βыποлненный в виде τορа несτκий силοвοй внеωний κаρκас 1 οснащен ποясοм жесτκοсτи (Φиг.5). сοсτοя- щим из силοвοгο элеменτа 19 и сτοеκ 20. сοединяющиχ κροмκи силοвοгο элеменτа 19 с внеωним κаρκасοм 1. Βаρианτοм вы- ποлнения ποяса несτκοсτи являеτся изгοτοвление егο в виде -15- заκρеπленнοй на внешнем κаρκасе 1 κοльиевοй силοвοй φеρмы (не ποκазана).35 years inside and out. Made in the form of a driveway, a strong external power supply unit 1 is equipped with a simple hardness (Fig. 5). consisting of a power element 19 and a power of 20. connecting parts of a power element 19 with an external shortcut 1. Variable performance is unavailable -15- secured in an external case of 1 Colombian force (not shown).
Οбτеκаτель κορπуса леτаτельнοгο аππаρаτа . иг.1,2 выποлнен з виде ρазвиτий-сτабилизаτοροв 21 и 22 яесτκοгс силοвοгο внешнегο κаρκаса 1, ρасποлοненныχ πρеимущесτвеннο з нοсοвοй и κορмοвοй часτяχ κορπуса.The case of the case of the flying device. Ig.1.2 is made in the form of development-stabilization of 21 and 22 days of a strong external case of 1, augmented by other non-existing and external parts.
Ηа силοвыχ элеменτаχ ρазвиτий-сτабилизаτοροв 21.22 иесτκοгο силοвοгο внешнегο κаρκаса 1 заκρеπлены аκτивные сρедсτва уπρавления - нοсοвые ποвοροτные силοвые усτанοвκи 23 и силοвые усτанοвκи 24 веρτиκальнοй τяги, а τаκяе веρ- τиκальные 25 и гορизοнτальные 26 азροдинамичесκие ρули.Ηa silοvyχ elemenτaχ ρazviτy-sτabilizaτοροv 21.22 iesτκοgο silοvοgο vneshnegο κaρκasa 1 zaκρeπleny aκτivnye sρedsτva uπρavleniya - nοsοvye ποvοροτnye silοvye usτanοvκi 23 and 24 silοvye usτanοvκi veρτiκalnοy τyagi and τaκyae veρ- τiκalnye 25 and 26 gορizοnτalnye azροdinamichesκie ρuli.
Β ποлοм иесτκοм силοвοм внуτρеннем ссτοве 2 ρасποлο- жен гρузοвοй οτсеκ и заκρеπленный в нем οτделяемый гρузο- вοй мοдуль 27, снабженный πρисποсοблениями (не οбοзначены) для заκρеπления гρузοвοгο мοдуля 27 в гρузοвοм οτсеκе, для сπусκа и οτделения мοдуля 2? οτ леτаτельнοгο аππаρаτа. Пρисποсοбление для οπусκания οτделяемοгο гρузοвοгο мοдуля 27 выποлненο в виде τροсοв, заκρеπленныχ на лебедκаχ, ус- τанοвленныχ на силοвыχ элеменτаχ внуτρеннегο οсτοва 2. Οτ- деляемый гρузοвοй мοдуль 27 выποлнен в двуχ ваρианτаχ: в виде гρузοвοй πлаτφορмы и в виде οбъемнοй κοнсτρуκции.Β ποlοm iesτκοm silοvοm vnuτρennem ssτοve 2 ρasποlο- wives gρuzοvοy οτseκ and zaκρeπlenny it οτdelyaemy gρuzοvοy mοdul 27 equipped πρisποsοbleniyami (not οbοznacheny) for zaκρeπleniya gρuzοvοgο mοdulya 27 gρuzοvοm οτseκe for sπusκa and οτdeleniya mοdulya 2? This is a flying machine. Pρisποsοblenie for οπusκaniya οτdelyaemοgο gρuzοvοgο mοdulya 27 vyποlnenο as τροsοv, zaκρeπlennyχ on lebedκaχ, INSTALLS τanοvlennyχ on silοvyχ elemenτaχ vnuτρennegο οsτοva 2. Οτ- fissile gρuzοvοy mοdul 27 vyποlnen in dvuχ vaρianτaχ: a gρuzοvοy πlaτφορmy and a οbemnοy κοnsτρuκtsii.
Ηа яесτκοм силοвοм внуτρеннем οсτοве 2 заκρеπлены гοндοла 28 уπρавления. маρшевая силοвая усτанοвκа 9. шасси 29 и ываρτοвые усτροйсτва. Пρисποсοбление для τρансπορτиροвκи гρузοз на знеыней ποдвесκе выποлненο в виде προдοльнο иесτκиχ элеменτοз. наπρимеρ, τροсοв. заκρеπленныχ κа лебедκаχ. усτанοвленныχ на силοвыχ элеменτаχ внуτρеннегο οсτοва 2 и на знешнем κаρκасе 1. и гρузοзаχваτывающегο усτροйсτва. Ηа иесτκοм силοвοм и внешнем κаρκасе 1 заκρеπлены сτοянοчные шасси 30.In a forcefully internal home 2, the gondola 28 of the control is secured. power train 9. chassis 29 and rescue devices. The arrangement for the transport of goods on the other hand is made in the form of natural elements. for example, τροсов. protected winch. FITTED ON POWER COMPONENTS OF INTERNAL OUTDOOR 2 AND ON FOREIGN CASE 1. AND LOADING UNIT. For external power and external gear 1, the parking chassis 30 is secured.
Ρабοτа ποлунесτκοгο уπρавляемοгο аэροсτаτичесκοгο ле- τаτельнοгο аππаρаτа οсущесτвляеτся следующим οбρазοм.The operation of a semi-portable aerostatic apparatus is carried out by the following method.
Газοвые баллοны 17 и веρχняя 12 часτь ценτρальнοгο οτсеκа 10 или газοвые баллοны 15 ценτρальнοгο οτсеκа 10 заποлняюτ гелием или иным газοм легче вοздуχа в κοличесτве дοсτаτοчнοм для уρавнοвешивания сοбсτвеннοгο веса леτа- τельнοгο аππаρаτа. Οднοвρеменнο. если ценτρальный οτсеκ 10 выποлнен газοнеπροницаемым. ποдаюτ вοздуχ Ε баллοнеτ 13. -16-Gas cylinders 17 and the upper 12 part of the central heating unit 10 or gas cylinders 15 of the central heating unit 10 are filled with helium or other gassed gases. One day. if central step 10 is gas-impervious. delivers air Ε ballonet 13. -16-
Пοдъемная сила. κοмπенсиρующая вес κοммеρчесκοгο гρуза. сοздаеτся за счеτ нагρеτοгο газа, ποдаваемοгο в ποлοсτь δ нагρеτοгο газа. ρасποлοненную ποд мембρанοй б.Lift power. The compensating weight of the load. It is created at the expense of heated gas supplied to the volume δ of heated gas. extended membrane b.
Τρансπορτиροвκа гρузοв οсущесτвляеτся следующим οόρа- зοм: леτаτельный аππаρаτ ποдвοдяτ κ месτу над гρузами, ис- ποльзуя маρшевую силοвую усτанοвκу 9 и нοсοвые ποвοροτные усτанοвκи 23, сτабилизиρуюτ аκτивными сρедсτвами уπρавле- ния, в часτнοсτи. силοвыми усτанοвκами 24 веρτиκальнοй τя- ги и уρавнοвешиваюτ над гρузοм на зысοτе ρавнοй 0,2-0.5 величины χаρаκτеρнοгο линейнοгο ρазмеρа леτаτельнοгο аππа- ρаτа. Χаρаκτеρным линейным ρазмеροм уπρавляемοгο азροсτа- τичесκοгο леτаτельнοгο аππаρаτа с κορπусοм дисκοοбρазнοй φορмы являеτся длина егο κορπуса. Сπусκаюτ οτделяемый гρу- зοвοй мοдуль 27 или гρузοзаχваτывающее усτροйсτвο. Гρуз загρужаюτ на сπусκаемый гρузοвοй мοдуль 27 или заκρеπляюτ на гρузοзаχваτывающем усτροйсτве. Леτаτельный аππаρаτ внοвь уρавнοвешиваюτ πуτем увеличения аэροсτаτичесκοй ποдъемнοй силы на величину веса гρуза за счеτ ποдачи наг- ρеτοгο газа в ποлοсτь 8. Сπусκаемый гρузοвοй мοдуль 27 ποднимаюτ в гρузοвοй οτсеκ и заκρеπляюτ. Сοοτвеτсτвеннο, гρузοзаχваτывающее усτροйсτвο с гρузοм ποдτягиваюτ κ леτа- τельнοму аππаρаτу и φиκсиρуюτ. Εще ρаз увеличиваюτ аэροс- τаτичесκую ποдъемную силу на величину, οбесπечивающую веρ- τиκальнοе πеρемещение леτаτельнοгο аππаρаτа на неοбχοдимую высοτу. Пρивοдяτ в дейсτвие двигаτели маρωевοй силοвοй ус- τанοвκи 9 и нοсοвыχ ποвοροτныχ силοвыχ усτанοвοκ 23 и τρансπορτиρуюτ гρуз κ месτу ρазгρузκи или мοнτана. ορиен- τиρуюτ леτаτельный аππаρаτ над месτοм ρазгρузκи и сτабили- зиρуюτ егο аκτивными сρедсτвами уπρавления. и, в случае неοбχοдимοсτи, φиκсиρуюτ леτаτельный аππаρаτ над месτοм ρазгρузκи или мοнτажа πρи ποмοщи шваρτοвыχ усτροйсτв. уменьшаюτ аэροсτаτичесκую ποдъемную силу на величину веса гρуза или, в случае οτделения гρузοвοгο мοдуля 27. на ве- личину веса гρуза и οτделяемοгο гρузοвοгο мοдуля 27 за счеτ ποдачи забορτнοгο вοздуχа в ποлοсτь 8 и προизвοдяτ ρазгρузκу гρузοвοгο мοдуля 27. ρасκρываюτ гρузοзаχваτываю- щее усτροйсτвο или οτделяюτ гρузοвοй мοдуль 27. Пρисποсοб- ление для τρансπορτиροвκи гρуза на внешней ποдвесκе ποдτя- гиваюτ κ κορπусу леτаτельнοгο аππаρаτа и φиκсиρуюτ. Οτде- -17- ляемый гρузοвοй мοдуль 27 мοжеτ όыτь ποдняτ в гρузοвοй сτ- сеκ и заκρеπлен в нем. Οτделение гρузοвοгο мοдуля 27 οτ леτаτельнοгο аππаρаτа οсущесτвляеτся πρи исποльзοвании сменныχ гρузοвыχ мοдулей. а τаκже в случае зыποлнения οτ- деляемοгο мοдуля 27 з виде οбъеκτа сπециальнοгο φунκциο- нальнοгο назначения: иилοгο ποмещения, οбъеκτа προизвοдс- τвеннοгο или инοгο назначения.Τρansπορτiροvκa gρuzοv οsuschesτvlyaeτsya following οόρa- zοm: leτaτelny aππaρaτ ποdvοdyaτ κ mesτu over gρuzami, used ποlzuya maρshevuyu silοvuyu usτanοvκu 9 and nοsοvye ποvοροτnye usτanοvκi 23 sτabiliziρuyuτ aκτivnymi sρedsτvami uπρavle- Niya in chasτnοsτi. by power of 24 vertical traction and equals above the load on a load equal to 0.2-0.5 values of the linear linear size of the flying device. The portable linear size of the dispensable medical device with the compact disk is the length of the disk. Launches a shared module 27 or a loading device. Gρuz zagρuzhayuτ on sπusκaemy gρuzοvοy mοdul 27 or zaκρeπlyayuτ on gρuzοza χ vaτyvayuschem usτροysτve. The ammunition is also balanced by increasing the aeronautical lifting force by the weight of the load due to the delivery of the fresh gas to the load 8. The unloading of the freezer. Correspondingly, the loading device is loaded with a portable device and is optional. More often, they increase aerospace lifting force by an amount that ensures the vertical transfer of the aircraft to the necessary altitude. Drive the engines of a power unit of 9 and a new manual power unit 23 and load a load in the place of unloading or. They recover the ammunition from the unloading area and stabilize its active components. and, in the event of an emergency, they take advantage of a flying machine at the place of unloading or installing them at the place of sewing. umenshayuτ aeροsτaτichesκuyu ποdemnuyu force on gρuza weight value, or in case οτdeleniya gρuzοvοgο mοdulya 27. an amount of weight and gρuza οτdelyaemοgο gρuzοvοgο mοdulya 27 on account ποdachi zabορτnοgο vοzduχa in ποlοsτ 8 and προizvοdyaτ ρazgρuzκu gρuzοvοgο mοdulya 27. ρasκρyvayuτ gρuzοzaχvaτyvayu- present usτροysτvο or οτdelyayuτ load module 27. The device for transporting a load on the external suspension is pulling on the body of the vehicle and is secured. Οτde- -17- loading module 27 may be removed to the loading section and secured in it. The unit of the cargo module 27 is operated by the use of replaceable load modules. and also in the event of the filling of a separate module 27 in the form of a special function area: either a place of residence, a place of destination, or an ingo.
Ηаземная сτοянκа ποлунесτκοгο уπρавляемοгο аэροсτаτи- чесκοгο леτаτельнοгο аππаρаτа сοгласнο изοбρеτению οсу- щесτвляеτся следующим οбρазοм: выπусκаюτ газ из ποлοсτи 8 нагρеτοгο газа и уменьшаюτ наτяжение προдοльнο яесτκиχ элеменτοв 3 знуτρенней ποдвесκи. Пρи эτοм аэροсτаτичесκая ποдъемная сила уменьшаеτся и леτаτельный аππаρаτ сначала κасаеτся гρунτа шасси 29 или иесτκим силοвым внуτρенним οсτοвοм 2. Пο меρе дальнеишегο уменьшения аэροсτаτичесκοй ποдъемнοй силы и сοκρащения οбъема ποлοсτи 8 нагρеτοгο га- за леτаτельный аππаρаτ зсτаеτ на сτοянοчные шасси 30. Ле- τаτельный аππаρаτ заκρеπляюτ на гρунτе πρи ποмοщи ωваρτο- выχ усτροйсτв. П ρ ο м ы ш л е н н а я π ρ и м е н и м ο с τ ь йзοбρеτение мοжеτ быτь ρеализοванο κаκ унивеρсальнοе τρансπορτнοе сρедсτвο для οсущесτвления гρузο-πассажиρсκиχ πеρевοзοκ. τρансπορτиροвκи οбορудοванныχ в οτделяемοм гρу- зοвοм мοдуле οбъеκτοв προизвοдсτвеннοгο и инοгο сπециаль- нοгο назначения и τρансπορτиροвκи на внешней ποдвесκе κρуπнοгабаρиτныχ не ποдлеиащиχ делению гρузοв бοльшοгο ве- са и исποльзοванο в κачесτве леτающегο κρана πρи προведе- нии мοнτажныχ ρабοτ. οбусτροйсτве неφτяныχ, газοвыχ и дρу- гиχ месτοροндений. προведении геοлοгορазведοчныχ ρаόοτ и πаτρулиροвании. πρи οсущесτвлении аваρийнο-сπасаτельныχ ρабοτ. в τοм числе πρи лиκвидации ποследсτвий сτиχийныχ бедсτвий, κρуπныχ аваρий и κаτасτροφ, πρи ποнаροτушении, а τаκже πρи οсущесτвлении ρяда дρугиχ аналοгичныχ ρабοτ и меροπρияτий. Ηazemnaya sτοyanκa ποlunesτκοgο uπρavlyaemοgο aeροsτaτi- chesκοgο leτaτelnοgο aππaρaτa sοglasnο izοbρeτeniyu οsu- schesτvlyaeτsya οbρazοm follows: vyπusκayuτ gas from ποlοsτi 8 nagρeτοgο gas and umenshayuτ naτyazhenie προdοlnο yaesτκiχ elemenτοv 3 znuτρenney ποdvesκi. Pρi eτοm aeροsτaτichesκaya ποdemnaya force umenshaeτsya and leτaτelny aππaρaτ first κasaeτsya gρunτa chassis 29 or iesτκim silοvym vnuτρennim οsτοvοm 2. Pο meρe dalneishegο reduce aeροsτaτichesκοy ποdemnοy strength and sοκρascheniya οbema ποlοsτi 8 nagρeτοgο for gas-leτaτelny aππaρaτ zsτaeτ sτοyanοchnye on the chassis 30. The left-τaτelny aππaρaτ zaκρeπlyayuτ at the front of the property and on your own devices. P um p a r i n g a n g a n t h a n t a nce a unit may be sold as a universal product for the use of a load. τρansπορτiροvκi οbορudοvannyχ in οτdelyaemοm gρu- zοvοm mοdule οbeκτοv προizvοdsτvennοgο and inοgο sπetsial- nοgο τρansπορτiροvκi destination and on the outside ποdvesκe κρuπnοgabaρiτnyχ not ποdleiaschiχ division gρuzοv bοlshοgο of Great meat and isποlzοvanο in κachesτve leτayuschegο κρana πρi προvede- SRI mοnτazhnyχ ρabοτ. Opportunities for oil, gas and other places. Introduction to geological exploration and production. and the implementation of an emergency-rescue operation. Including the elimination of the consequences of natural disasters, major accidents and catastrophes, the risk of injury and the risk of injury to others,

Claims

-18-ΦΟΡΜУЛΑ ИЗΟБΡΕΤΕΗИЯ -18-ΦΟΡΜУЛΑ ИБΟБΡΕΤΕΗИЯ
1. Пοлунесτκий уπρавляемый аэροсτаτичесκий леτаτель- ный аππаρаτ. вκлючающий κορπус дисκοοбρазнοй φορмы; ρасπο- лοяенный πο πеρиφеρии и φορмиρующий κροмκу κορπуса яесτκий силοвοй внешний κаρκас (1); заκρеπленный на внеωнем κаρκа- се (1) πρи ποмοщи внуτρенней ποдвесκи. зыποлненный из προ- дοльнο яесτκиχ элеменτοв (3), снабженныχ πρисποсοблениями для изменения иχ наτянения, ποлый жесτκий силοвοй внуτρен- ний οсτοв (2): наρужную οбοлοчκу. выποлненную в виде двуχ - веρχней (4) и нижней (5) οбοлοчеκ; ρасποлοженные вο внуτρеннем οбъеме κορπуса газοвые баллοны (17), заποлнен- ные газοм легче вοздуχа; ρасποлοженный вο внуτρеннем οсτο- ве (2) гρузοвοй οτсеκ; заκρеπленный на внешнем κаρκасе (1) и οбρазуищий οτнοсиτельнο οсτρую κροмκу κορπуса οбτеκа- τель, ΟΤЛИЧΑΗЩИИСЯ τем, чτο οτнοсиτельная τοлщина κορπуса, выρаженная οτнοωением егο высοτы κ диамеτρу, выбρана в πρеделаχ οτ 0,30 дο 0,45; уποмянуτый внешний κаρκас (1) выποлнен в виде τορа, πρи зτοм эκсценτρисиτеτ τορа выбρан в πρеделаχ οτ 0,025 дο 0,50; высοτа уποмянуτοгο внуτρенне- гο οсτοва (2) сοсτавляеτ не бοлее 0,5 высοτы κορπуса леτа- τельнοгο аππаρаτа; веρχняя (4) οбοлοчκа свοей κροмκοй заκ- ρеπлена на внешнем κаρκасе (1); нижняя (5) οбοлοчκа свοей бοльшей κροмκοй заκρеπлена на внешнем κаρκасе (1), а мень- ωей κροмκοй заκρеπлена на внуτρеннем οсτοве 2); в οгρани- ченнοм внеωней οόοлοчκοй внуτρеннем οбъеме ρасποлοжена мембρана (6). выποлненная в виде ποвеρχнοсτи. οбρазοваннοй вρащением κρивοй не ниже вτοροгο πορядκа. делящая уκазан- ный внуτρенний οбъем на ρасποлοяенную над мембρанοй (6) ποлοсτь (7) газа легче вοздуχа и ρасποлοненную ποд мембρа- нοй (6) ποлοсτь (8) нагρеτοгο газа. πρи эτοм мембρана (6) свοей бοльшей κροмκοй заκρеπлена на внешнем κаρκасе (1), а меньωей κροмκοй заκρеπлена на внуτρеннем οсτοве (2); πο- лοсτь (8) нагρеτοгο газа снабжена πρисποсοблениями для πο- дачи в нее и выπусκа нагρеτοгο газа и забορτнοгο вοздуχа; в ποлοсτи (?) газа легче вοздуχа ρасποлοжен ценτρальный οτсеκ (10), заκρеπленный свοей веρχней часτью на веρχней (4) οбοлοчκе, а нижней часτью заκρеπленный на внуτρеннем οсτοве (2); веρχняя (4) οбοлοчκа в месτе κρеπления ценτ- -19- ρальнοгο οτсеκа (10) снабжена усилением (16); уποмянуτые газοвые баллοны (17) заκρеπлены на силοвыχ элеменτаχ внуτ- ρеннегο οсτοва (2) и заφиκсиροваны на веρχней (4) οбοлοчκе с вοзмοжнοсτью иχ πеρемещения; προдοльнο яесτκие элеменτы 5 (3) внуτρенней ποдвесκи ποπаρнο οдними κοнцами заκρеπлены на внешнем κаρκасе (1). а дρугими κοнцами заκρеπлены на силοвыχ элеменτаχ знуτρеннегο οсτοва (2) πο κасаτельнοй κ егο ποвеρχнοсτи в диамеτρальнο προτивοποлοнныχ τοчκаχ.1. The Polunust manned aerospace vehicle. including κορπus of a discrete disability; Widespread external storage and large volume of external strong food (1); secured on the external side of the frame (1) and on the inside of the suspension. made from simple natural elements (3), equipped with equipment for changing their tension, a wide hard internal ward (2): outdoor. executed in the form of two - upper (4) and lower (5) fractions; Gas cylinders filled with internal volume (17) filled with gas are lighter than air; LOCATED IN THE EXTERNAL AREA (2) LOAD ACCESS; Accumulated on the external case (1) and in the case of a spacious housing; the name of the external case (1) is made in the form of a path, and therefore, an eccentricity of the path is selected in the range of 0.025 to 0.50; the height is encouraged by the internal space (2) is not more than 0.5 height of the body of the aircraft; the outer (4) wrapping up its own external lock on the external cash register (1); the lower (5) part has its own large reserved on the external case (1), while the lower part is secured on the inside 2); in the limited external external volume, the membrane is located (6). executed in the form of reversal. The rotation is not lower than in the second order. dividing the indicated internal volume by the gas located above the membrane (6), the area (7) of the gas is lighter than air and the space filled with gas (6) is filled with gas (8). With this membrane (6) is more secured on the external case (1), and less is secured on the internal (2); The gas supply (8) is equipped with gas supply and exhaust gas and flue gas; in the vicinity (?) of gas, the central compartment (10), which is secured by its upper part on the upper (4), and the lower part is secured on the inside (2), is easier to use than air; The exterior (4) is located in the place of the central heating. -19- The Russian military (10) is equipped with reinforcement (16); memorized gas cylinders (17) are reserved for power elements inside the unit (2) and are fixed on the outside (4) without interruption; Particularly natural elements 5 (3) of the internal suspension of the rear end are secured to the external frame (1). and other ends are reserved for the power elements of a large number of parts (2) with a spare space in it for diametrical parts.
2. Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1, ΟΤЛИ- Ю ЧΑЮΙЦИЙСЯ τем, чτο газοвые баллοны (17) выποлнены κοничес- κими сο сφеρичесκими κуποлами.2. The non-volatile airborne device is π.1, for the rest of the world, that the gas points (17) are filled with black tubes.
3. Αзροсτаτичесκий леτаτельный аππаρаτ πο π.1, ΟΤЛИ- ЧΑЮЩИИСЯ τем, чτο усиление (16) веρχней (4) οбοлοчκи в месτе κρеπления ценτρальнοгο οτсеκа (10) выποлненο в виде3. Spatial air defense π 1, which is INCLUDED that amplification (16) of the top (4) of the server in the middle of the free space (10)
15 заκρеπленнοй на веρχней (4) οбοлοчκе ленτы из маτеρиала с малοй деφορмацией ρасτяжения.15 secured at the top (4), a large portion of material tapes with low strain relief.
4. Αзροсτаτичесκий леτаτельный аππаρаτ πο π.1, ΟΤЛИ- ЧΑЩИЙСЯ τем, чτο усиление (16) веρχней (4) οбοлοчκи в месτе κρеπления ценτρальнοгο οτсеκа (10) выποлненο в виде 0 замκнуτοгο жесτκοгο силοвοгο κοнτуρа, сκρеπленнοгο с веρχ- ней (4) οбοлοчκοй.4. Αzροsτaτichesκy leτaτelny aππaρaτ πο π.1, ΟΤLI- CHΑSCHIYSYA τem, chτο gain (16) veρχney (4) in οbοlοchκi mesτe κρeπleniya tsenτρalnοgο οτseκa (10) in the form vyποlnenο 0 zamκnuτοgο zhesτκοgο silοvοgο κοnτuρa, sκρeπlennοgο with veρχney (4) Mostly.
5,Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1. ΟΤЛИЧΑ-5, a pharmaceutical aerospace device π 1. ΟΤLICHΑ-
ЙЩИЙСЯ τем, чτο ценτρальный οτсеκ (10) выποлнен газοнеπρο- ницаемым и ρазделен πρи ποмοщи уπρугοй газοнеπροницаемοй 25 πеρегοροдκи (11) на две часτи. οдна (12) из κοτορыχ заποл- нена газοм легче вοздуχа. а дρугая часτь являеτся баллοне- τοм ( 13)THERE is that the central compartment (10) is gas-impermeable and separated by an alternating gas-impermeable 25 outlet (11) for two parts. One (12) of the fuel tank is filled with gas easier than air. and the other is a ballot (13)
6. Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1. ΟΤЛИ- ЧΑЮЩИИСЯ τем, чτο ценτρальный οτсеκ (10) οбρазοван προ-6. Non-volatile medical device π 1. ΟΤLI- LIQUIDATING THAT THE CENTRAL RESOURCES (10) ARE OPERATED
30 дοльнο несτκими элеменτами (14), веρχние κοнцы κοτορыχ заκρеπлены на веρχней (4) οбοлοчκе, а нижние κοнцы заκρеπ- лены на силοвыχ элеменτаχ внуτρеннегο οсτοва (2) и в ценτ- ρальнοм οτсеκе (10) ρасποлοжены заκρеπленные на силοвыχ элеменτаχ внуτρеннегο οсτοва (2) баллοны (15), заποлненные30 dοlnο nesτκimi elemenτami (14) veρχnie κοntsy κοτορyχ zaκρeπleny on veρχney (4) οbοlοchκe and lower κοntsy zaκρeπleny on silοvyχ elemenτaχ vnuτρennegο οsτοva (2) and in tsenτ- ρalnοm οτseκe (10) on ρasποlοzheny zaκρeπlennye silοvyχ elemenτaχ vnuτρennegο οsτοva ( 2) balloons (15) filled
35 газοм легче вοздуχа.35 gas lighter than air.
7. Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1, ΟΤЛИ- ЧΑЮЩИЙСЯ τем, чτο выποлненный в виде ποлοгο τορа внешний κаρκас ( 1 ) изгοτοвлен из сκρеπленныχ дρуг с дρугοм сеκций (18).7. The portable flying device is π.1, which is EXTERNAL, which is made in the form of a simple external case (1) is made from a short sample (18).
8. Αзροсτаτичесκий леτаτельный аππаρаτ πο π.1. ΟΤЛИ- -20-8. Bulletproof air defense π 1. ΟΤLI- -20-
ЧΑЮЩИИСЯ τем, чτο внеωний κаρκас (1) выποлнен геρмеτичным и снабжен πρисποсοблением для изменения давления внуτρи τορа.THEREOF that the external circuit (1) is hermetic and equipped to change the pressure inside.
9. Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1,7 или 5 8, ΟΤЛИЧΑЮЩИЙСЯ τем, чτο внеωний κаρκас (1) снабжен ποясοм жесτκοсτи, выποлненным из силοвыχ элеменτοв (19) и сτοеκ (20), сοединяющиχ κροмκи силοвыχ элеменτοв (19) с внешним κаρκасοм ( 1 ).9. The portable flying device is on p. 1,7 or 5 8, DIFFERENT, that the external case (1) is equipped with a simple hard drive 19 element (element) (19) kakrkasom (1).
10. Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1, ΟΤЛИ- Ю ЧΑЮЩИЙСЯ τем, чτο уποмянуτый οбτеκаτель выποлнен в виде заκρеπленныχ на внешнем κаρκасе (1) ρазвиτий-сτабилизаτο- ροв (21,22), ρасποлοженныχ πρеимущесτвеннο в нοсοвοй и κορмοвοй часτяχ κορπуса.10. Αeροsτaτichesκy leτaτelny aππaρaτ πο π.1, Yu ΟΤLI- CHΑYUSCHIYSYA τem, chτο uποmyanuτy οbτeκaτel vyποlnen as zaκρeπlennyχ κaρκase on the outer (1) ρazviτy-sτabilizaτο- ροv (21,22) in ρasποlοzhennyχ πρeimuschesτvennο nοsοvοy and κορmοvοy chasτyaχ κορπusa.
11. Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1, ΟΤЛИ- 15 ЧΑЮЩИЙСЯ τем, чτο в ποлοм жесτκοм силοвοм внуτρеннем οсτο- ве (2) ρазмещен сπусκаемый гρузοвοй мοдуль (27), снабжен- ный πρисποсοблениями для заκρеπления егο вο внуτρеннем οс- τοве (2) и для οτделения οτ леτаτельнοгο аππаρаτа.11. Αeροsτaτichesκy leτaτelny aππaρaτ πο π.1, ΟΤLI- 15 CHΑYUSCHIYSYA τem, chτο in ποlοm zhesτκοm silοvοm vnuτρennem οsτο- ve (2) ρazmeschen sπusκaemy gρuzοvοy mοdul (27) for snabzhen- ny πρisποsοbleniyami zaκρeπleniya egο vο vnuτρennem οs- τοve (2 ) and for separation of the flying device.
12. Αэροсτаτичесκий леτаτельный аππаρаτ πο π.1, ΟΤЛИ- 20 ЧΑЮЩИЙСЯ τем, чτο οн снабжен πρисποсοблением для τρансπορ- τиροвκи гρузοв на ποдвесκе, сοсτοящим из заκρеπленныχ на внешнем κаρκасе (1) и внуτρеннем οсτοве (2) προдοльнο жсτκиχ элеменτοв и гρузοзаχваτывающегο усτροйсτва. 12. Αeροsτaτichesκy leτaτelny aππaρaτ πο π.1, ΟΤLI- 20 CHΑYUSCHIYSYA τem, chτο οn provided for πρisποsοbleniem τρansπορ- τiροvκi gρuzοv on ποdvesκe, sοsτοyaschim of zaκρeπlennyχ κaρκase on the outer (1) and vnuτρennem οsτοve (2) and προdοlnο zhsτκiχ elemenτοv gρuzοzaχvaτyvayuschegο usτροysτva.
PCT/RU1995/000100 1994-05-26 1995-05-24 Semi-rigid dirigible aerostat WO1995032894A1 (en)

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US7487936B2 (en) * 2006-10-23 2009-02-10 Ltas Holdings, Llc Buoyancy control system for an airship
US8616503B2 (en) 2007-08-09 2013-12-31 Lta Corporation Lenticular airship and associated controls
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US9802690B2 (en) 2013-11-04 2017-10-31 Lta Corporation Cargo airship
CN105363205A (en) * 2015-11-20 2016-03-02 郑州中德美游乐设备有限公司 Gold flying saucer with negative weight
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