WO1995027652A1 - Aeronef en forme de soucoupe volante - Google Patents

Aeronef en forme de soucoupe volante Download PDF

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Publication number
WO1995027652A1
WO1995027652A1 PCT/CN1995/000026 CN9500026W WO9527652A1 WO 1995027652 A1 WO1995027652 A1 WO 1995027652A1 CN 9500026 W CN9500026 W CN 9500026W WO 9527652 A1 WO9527652 A1 WO 9527652A1
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WO
WIPO (PCT)
Prior art keywords
cabin
flying
engine
nozzle
airbag
Prior art date
Application number
PCT/CN1995/000026
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English (en)
Chinese (zh)
Inventor
Gao Lu
Original Assignee
Gao Lu
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gao Lu filed Critical Gao Lu
Priority to AU21342/95A priority Critical patent/AU2134295A/en
Publication of WO1995027652A1 publication Critical patent/WO1995027652A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/001—Flying saucers

Definitions

  • the present invention relates to a new flight consisting of a side cabin, a middle cabin, a propulsion system, a fixture, a glare device, a driving wheel, and a passenger cabin.
  • Feiyu also known as UFO
  • UFO has been widely reported at home and abroad for its discovery. It may exist in aliens, and a large number of pictures have been taken of the shape of the flying saucer.
  • the object of the present invention is to provide a new aircraft, a flying raft, which is used for tourism, entertainment, short-distance passenger carrying, and long-distance transportation.
  • the flying saucer is composed of a side cabin, a middle cabin, a propulsion system, a fixing device, a glare device, a cockpit, and a passenger cabin;
  • the flying saloon has four side cabins, which are independent sealed bodies, and It is filled with helium, and the empty weight of the flying saucer is supported by the static lift of the helium in the side tank;
  • the flywheel side tank is composed of a skeleton, a longitudinal bulkhead, a transverse bulkhead, a reinforced longitudinal bulkhead, a strengthened transverse bulkhead, an outer shell, and a bulkhead Make up.
  • the side cabin skeleton is made of stringers, braces, and ring frames, and the fly cymbals side capsules are knotted .
  • a stringer upright in the center of the carcass is screwed with four "ten" -shaped braces and four pairs of braces.
  • the longitudinal partition frame is glued between the ring frame and the ring frame.
  • the horizontal partition pivot is glued between the vertical partition frame and the vertical partition frame.
  • a layer of shell is connected; the compartment is divided into four side tanks longitudinally according to the position of the support frame; each side tank has a self-sealing inflatable valve and a plastic pipe connecting the middle tank air vent; the UFO side tank can be
  • the inner bag structure is adopted, that is, an air bag is installed in each side cabin, and helium gas is contained in the air pocket.
  • the air bag is equipped with a self-sealing inflation valve and a plastic pipe communicating with the middle cabin air bag.
  • the UFO mid-cavity is composed of six-sided compartments with glued joints. There are two airbags in the mid-cabin, which are filled with helium gas to adjust the load of the flycatcher.
  • Each airbag is equipped with a self-sealing inflatable valve and a Electric control (switchable) valves
  • the bottom of the middle cabin is equipped with an electric blower and an exhaust port
  • the middle cabin is also equipped with a helium liquefaction ⁇
  • the two helium pumping pipes on the helium liquefaction ⁇ are connected to the two airbags respectively .
  • the flying propulsion system consists of a two-wing engine and a tail engine.
  • the engine diverting nozzle of the propulsion system consists of an upper turnable nozzle, a lower turnable nozzle, a rear turnable nozzle, a pipe, a nozzle, and a reversing valve.
  • the rotating nozzle is made of an outer tube, a worm wheel, a worm, a motor, a guide vane, and a blade regulator.
  • the rotating nozzle can be rotated from 0 to 360 °, and the guide vane can be adjusted from 0 to 8CTC, and can be adjusted up to 86. 5 °.
  • the structure of the engine reversing valve is that the reversing valve is an oval copper sheet.
  • the horizontal axis of the reversing valve passes through the nozzle.
  • the rocker outside the nozzle is fixed with the horizontal axis of the reversing valve.
  • One end is connected to a hydraulic actuator.
  • Propulsion system engines can use turbofan engines, or turbofan engines, or turbojet engines, or turbojet engines, or piston engines.
  • the stage fan generates thrust; the propulsion system controls the flight of the flycatcher by changing the direction of the valve and the rotation of the nozzles and guide vanes to change the direction of the ejected gas.
  • the flying saucer fixing device consists of a main fixed drill and a secondary fixed drill.
  • the fixed drill consists of a screw drill and a hydraulic actuator, a motor, a large cylindrical gear, a small cylindrical gear, and a thrust ball bearing.
  • the screw drill is the same as the large cylindrical gear.
  • the shaft rotates the small cylindrical gear by the motor, and drives the large cylindrical gear to rotate the auger bit.
  • the hydraulic actuating cylinder pressurizes the rotating auger bit so that It is drilled into the ground, and the motor is fixed on the piston rod of the hydraulic actuator.
  • Feiyu's strong light device consists of a short solitary xenon lamp with colored lenses on the chassis and a long arc xenon lamp with colored lenses under the butterfly wings.
  • the cockpit and passenger cabin are located under the load zone, the side and middle cabins are located, and the pilot gun is located at the front of the load zone.
  • the flying saucer is used for tourism, entertainment, short-distance passenger carrying, and long-distance transportation.
  • FIG. 1 Side view of UFO side cabin structure.
  • FIG. 1 Top view of UFO side cabin structure.
  • Figure 3 Side view of the internal knot of the fly.
  • Figure 4 Front view of the internal structure of the flying saucer.
  • Figure 5 Structure diagram of the two-wing engine of the UFO propulsion system.
  • FIG. 1 Structural diagram of the tail engine of the flying saucer propulsion system.
  • ⁇ 7. The installation positions of the "strengthening horizontal bulkhead”, “strengthening longitudinal bulkhead”, “strengthening support frame” and “strengthening ring frame” in the UFO side tank.
  • Fig. 8 Schematic diagram of flying flight (carcass rotation) control (bottom view).
  • Fig. 9 Schematic diagram of the flying cymbal rotation (disc rotation) (side view ⁇ ).
  • Figure 10 Side view of the rotatable nozzle of the Hida engine.
  • FIG. 11 Front view of the rotatable nozzle of the Hida engine.
  • the rotating nozzle of Hida engine has a "rotating device" structure which is sleepy from the top.
  • FIG. 14 Side view of the "rotating device" of the rotatable nozzle of the Hida engine.
  • FIG. 15 The first plan of the "blade adjustment ⁇ " of the rotatable nozzle of the Hida engine. ⁇ 16.
  • the second plan of the "blade regulator" of the rotating nozzle of the flying saucer engine is a side view.
  • Figure 17 Front view of the structure of the second scheme of the "blade regulator" of the rotary nozzle of the Hida engine.
  • FIG. 18 Enlarged view of the second solution structure of the "blade regulator" of the rotatable nozzle of the Hida engine (side view).
  • Fig. 20 Top view of the structure of the flyover engine reversing valve.
  • FIG. 21 Side view of the structure of the flyover engine reversing valve.
  • FIG. 23 structure diagram of Feiyu fixed drill (fixing device).
  • FIG. 24 Side view of Hida flight skills (engine control).
  • FIG. 25 Rear view of Hida flight skills (engine control).
  • FIG. 26 Installation position of piston engine in Hida propulsion system.
  • Fig. 27 Sectional view of the stringer of the flying salamander (first scheme).
  • Figure 29 Sectional view of the brace of the flying maggot skeleton.
  • Figure 30 Cross-section view of the ring frame of the flying pupa skeleton.
  • Figure 31 Sectional view of the longitudinal bulkhead of the Hida side tank (first option).
  • Figure 32 Sectional view of the longitudinal bulkhead of the Hida side tank (second option).
  • Figure 33 Cross section of the UFO side tank.
  • Figure 34 Vertical section view of the UFO mid-cavity.
  • Figure 35 Horizontal section view of the flying saucer.
  • Fig. 36 Flying weight balance diagram (bottom view).
  • FIG. 1 Side view of Hida side cabin structure.
  • Figure 2 Top view of the structure of the flash tank.
  • the fringe side cabin is composed of a skeleton, a longitudinal bulkhead (5), a transverse bulkhead (6), a shell, and a bulkhead (7).
  • the side cabin skeleton is composed of a longitudinal beam (1), a support frame (2), and a ring frame (4).
  • the fly wing side cabin knots a stringer (1) standing upright in the center of the carcass is screwed with four "ten" -shaped braces (2), one outside each of the four braces (2)
  • a layer of shell is glued to the longitudinal bulkhead (5) and the transverse bulkhead (6); the compartment (7) divides the carcass into four side compartments (8) according to the position of the support (2). ).
  • Figure 3 Side view of the internal structure of the flying salamander.
  • Figure 4 Front view of the larvae in the fly.
  • the midship (9) of the Feihuo is composed of six-sided cabins through gluing.
  • the stringer (1) passes through the center of the midship (9), and the load-bearing area (92) is at the bottom of the Feihuo, that is, the side tank (8). And under the middle compartment (9).
  • Other internal parts of the flycatcher paper beam (1), ring frame (4), support frame (2), longitudinal bulkhead (5), compartment (7), and shell (3). See Fig. 36 for the installation position of the flying junk fixture.
  • the two-wing and tail engines in the Hida propulsion system can use five types of engines, such as turbofan engines (15), and also turbocharged turbofan engines, turbocharged turbojet engines, turbojet engines, piston engines, and turbofans.
  • the engine (15) is taken as an example: the engine split nozzle (16) of the propulsion system is composed of an upper rotatable nozzle (17), a lower rotatable nozzle (18), a rear rotatable nozzle (19), a pipe (20), and a spray nozzle.
  • the pipe (21), the reversing valve (22), and the guide vane (23) are composed.
  • the main function of the tail engine is to control the flight direction, because the gas emitted by the tail engine is easy to cause the yaw to generate yaw moment and head up and down head moment. Its second function is to generate flight thrust.
  • the structure of the tail engine is the same as that of the two-wing engine The difference is that the tail engine air inlet (24) is accessed by the flying saucer body.
  • the supporting frame (2) of the flying maggot can be equipped with two “reinforcing braces” (90), and “reinforcement” can be installed between the ring frame (4) and the ring frame (4).
  • the ring frame "(91) is screwed to the compartment (7); the structure of the" reinforced support frame “is the same as the support frame (2), and the structure of the" reinforced ring frame “is the same as the ring frame (4) (see figure 29, 30).
  • Fig. 8 Schematic diagram of flying maggot rotation flight (carcass rotation) (bottom view).
  • Fig. 9 Schematic diagram of flying maggot rotation flight (carcass rotation) (side view).
  • the two-wing engine and the tail engine's reversing valve (22) are operated to make the gas spray from the lower rotatable nozzle (18), and the lower rotatable nozzle and the guide vane (23) are rotated to make the airflow direction (52) and the vertical axis (OX) is 45 °, and the guide vane (23) is 80 ° to the vertical axis (OY).
  • Figure 10 Side view of the rotatable nozzle of the Hida engine.
  • FIG. 11 Front view of the rotatable jet nozzle of the Hida engine.
  • Rotary nozzle (25), guide vane (23), blade adjustment ⁇ (26).
  • FIG. 13 Top view of Feiyu's revolving spray nozzle 'rotating device'.
  • FIG. 14 Side view of the "rotating device" of the rotatable nozzle of Feiyu.
  • the rotatable nozzle “rotating device” is composed of an outer pipe (50), a pipe (20), a worm gear (33), a worm (34), and a motor (35).
  • the outer pipe (50) is sleeved on the pipe (20), and the outer pipe
  • the worm (34) is driven by a motor (35); the rotatable nozzle can rotate from 0 to 360 °.
  • FIG. 15 is a structural diagram of the first scheme of the “blade regulator” of the rotatable nozzle.
  • the blade adjustment ⁇ is composed of a cylindrical gear (36), a rack (37), and a hydraulic actuator (38); at each guide vane (23 ) Has a cylindrical gear (36) at one end, and the cylindrical gear (36) is coaxial with the guide vane (23); above the cylindrical gear (36) is a rack (37), and the back of the rack (37) It has a fixed point (39) with the hydraulic actuator (38).
  • the blade adjustment ⁇ uses the expansion and contraction of the hydraulic actuator (38) to push the rack (37) to rotate the cylindrical gear (36), thereby controlling the guide vanes (23) Adjustment.
  • Each rotatable nozzle is equipped with a blade adjustment; the guide vanes can be adjusted from 0 to 80 °.
  • FIG. 1 Front view of the second solution of the rotatable nozzle "blade adjustment ⁇ ".
  • the blade adjuster pulls the guide vane (23) through the expansion and contraction of the hydraulic actuator (27), the piston rod (28) of the hydraulic actuator (27) and the exposed rocker (29) of the guide vane (23)
  • the rocker (29) is coaxial with the guide vane (23), and the rocker (29) on each guide vane is equipped with a hydraulic actuator (27).
  • the guide vane (23) is coaxial with the rocker (29), the shaft passes through the nozzle (53), (54) is the fulcrum of the rocker, and the end of the rocker (29) and the piston rod of the hydraulic actuator (27) (28) Connected.
  • Figure 20 Top view of the flyover engine reversing valve knot.
  • FIG. 21 Side view of the structure of the flyover engine reversing valve.
  • Figure 22 Enlarged view of the shuttle valve reversing valve structure (side view).
  • the flyover engine reversing valve (22) is an oval steel sheet.
  • the horizontal axis (56) of the reversing valve passes through the nozzle (57).
  • the rocker (58) outside the nozzle and the horizontal axis of the reversing valve. (56) fixed together.
  • the intersection of the horizontal axis (56) and the nozzle (57) is the fulcrum (59) of the reversing valve.
  • One end of the rocker (58) is connected to the hydraulic actuator (60).
  • the reversing valve (22) is operated by hydraulic pressure.
  • the extension of the moving cylinder (60) is performed.
  • the flying saucer fixed drill consists of a 1-2 meter long screw bit (43), a hydraulic actuator (44), a motor (45), a large cylindrical gear (46), a small cylindrical gear (47), and a thrust ball bearing; Auger The head (43) is coaxial with the large cylindrical gear (46), and the small cylindrical gear (47) is rotated by the motor (45) to drive the large cylindrical gear (46) to rotate the auger bit (43); 44) There is a thrust ball bearing between the screw bit (43) and the hydraulic screw (44) presses the rotating screw bit (43) into the ground; the motor (45) is fixed on the hydraulic tube (44) on the piston rod (48); when the flywheel takes off, the auger bit (43) turns and the hydraulic actuator (44) retracts. d indicates the large diameter of the auger and the small diameter of the auger.
  • Figure 24 Side view of flying saucer (engine control) skills.
  • FIG. 25 Rear view of Hida flight skills (engine operation level).
  • the Hida Due to the static buoyancy generated by the nitrogen in the side of the Hida, the Hida is close to zero gravity when suspended in the air, and the 200KN thrust generated by the Hida two-wing engine and the 100KN thrust generated by the tail engine make the Hida in the air. It has extremely strong maneuverability when flying; the UFO engine has special swivel nozzles. All nine swivel nozzles can rotate 0-360 °, and the guide vanes can be adjusted 0-80 °.
  • the turning nozzle (19) sprays downward, and the airflow direction (72), the flying bird flies forward and upward 62 °; on the way, the flying bird flies toward the upper rear 34 °, and the flight direction ( ⁇ ), this second procedure, in the first
  • the lower rotatable nozzle (18) is turned to the front, and the guide vane (63) is adjusted to the vertical axis ( (X) to 34 °, and then the reversing valve [the dotted line (61) in Figure (24) refers to the position after the reversing valve is moved], so that the gas is ejected from the lower rotatable nozzle (18), and the airflow direction ( 62) is 34 with the vertical axis.
  • Flight direction (66) this third procedure, at this time, the upper turnable nozzle (17) has turned to the left (see Figure 25), and the guide vane (65) has been adjusted to a position of 18 ° with the horizontal axis Then, the reversing valve is mobilized, so that the gas is ejected from the upper turnable nozzle (17), and the gas ejection direction (73) is at 18 ° with the horizontal axis (0Z), so that the flywheel turns to fly to the lower right 18 °: Feiyu turns to other angles, and can be analogized by this method. 5 ° ⁇ The flying vane guide blades can be adjusted up to 86.5 ° when needed.
  • the Hida can take off vertically quickly: When the UFO is parked on the ground, two fixed drills ⁇ two auger drills are drilled into the ground, and when the Hida is taking off vertically, the two afterburning turbofans of the two-wing engine start
  • the material of the mid-airbag of the Hida Polyurethane 66 load-bearing parts combined with anti-cracking weaving method; single-sided polyurethane S coating.
  • Hida diameter 93m Hida side cabin, middle cabin
  • Flight chart airspeed indicator, altimeter, horizon, heading indicator ⁇ , speedometer, turning inclinometer, wind direction and wind speed indicator ⁇ , atmospheric temperature indicator, remote reading magnetic compass.
  • Engine instrumentation tachometer, pressure ratio gauge, temperature gauge, fuel gauge, fuel pressure gauge, oil pressure gauge, intake pressure gauge, torque gauge, vibration gauge.
  • Auxiliary instruments ammeter, hydraulic meter, power meter, frequency meter.
  • Xenon lamps are installed at the bottom and under the wings of the flying scorpion.
  • the bottom is a short-arc xenon lamp combined into various shapes, such as circular, oval, triangular, and cross.
  • the xenon lamps are covered with colored lenses, which can produce colored intense light: this is the "strong light device" of Feiyu.
  • the left and right cabins are equipped with a large area of high-strength glass, the material is polymethyl methacrylate. S purpose; the square glass on the sides and bottom of the cabin is made of carbon / ring.
  • the cockpit and part of the cabin are made of Kevlar 49 / ring-mold resin molded parts.
  • the cabin is equipped with a seat and a seat belt.
  • the exterior glass is brown, and the bottom glass is protected. Change when entering the cabin. Put on clean rubber-soled shoes.
  • a helium liquefier is installed in the midge of the Hida.
  • the two helium pumping pipes on the helium liquefier are connected to the two airbags respectively. During the flight, the helium equivalent to the fuel consumption of the engine is liquefied. Suspension.
  • the flying safety number of this flying maggot is very high; in case of helium leakage or a piece of skin (shell) of the flying saucer side case, the four side compartments of this flying maggot are independent sealed bodies, and the middle airbag There are also two seals.
  • the UFO loses only the nitrogen of one side tank, and the result is that the UFO slowly descends; if the engine catches fire or even the fuel tank explodes, only the helium of the two side tanks is lost. The other two The side and middle cabins were still working, and the flying saucer landed without any surprise.
  • FIG. 26 Installation position of piston engine.
  • Piston engine (74) can be used in the flying stern engine. It is driven by the piston engine to generate thrust by the three stern fan (75). UFOs with this type of engine have low noise and are suitable for low-altitude sightseeing flights, and their fuel consumption is very low, making them suitable for long-distance transportation.
  • Figure 27 Sectional view of the stringer (1) of the flying pupa skeleton (first scheme).
  • Figure 28 Sectional view (2) of the longitudinal beam (1) of the Hida skeleton.
  • Fig. 29 is a sectional view of the support frame (2) of the flying maggot skeleton.
  • Fig. 30 is a sectional view of the ring frame (4) of the flying maggot skeleton.
  • Figure 31 Sectional view of the longitudinal bulkhead (5) of the flywheel side wheel (first scheme).
  • Figure 32 Sectional view of the longitudinal bulkhead (5) of the fringe side tank (second option).
  • connection and fixation between the longitudinal beam (1) and the support frame (2), the support frame (2) and the ring frame (4) of the flying skeletal frame adopts screwing and riveting (see Figures 1 and 2); the longitudinal partition frame ( 5).
  • the horizontal bulkhead (6) and the ring frame (4) are connected and fixed with high-performance adhesives: the shell and the ring frame (4), the horizontal bulkhead (5), and the horizontal bulkhead.
  • the anastomosis between the frame (S), the shell and the shell is also glued.
  • the Hida housing (skin) is made of glued Kevlar 49 / ring panel and Nomex honeycomb sandwich material, and the outside of the housing is sprayed with hafnium titanium coating.
  • the longitudinal beams (1), braces (2), ring frames (4), compartments (7), longitudinal bulkheads (5), and transverse bulkheads (6) of the flying salamander frame are unidirectional Kevlar 49 / rings Air skin and Nomex honeycomb sandwich materials are made by copying; the cockpit and passenger cabin can also be made by this method and then assembled.
  • the static lift of the helium in the UFO side tank supports the empty weight of the flywheel.
  • Each side tank is equipped with a self-sealing inflatable valve.
  • Feiyu side capsules can use internal knots, that is, an airbag is installed in each side capsule, and ⁇ is installed in the airbag; the shape and size of the airbag are similar to the side capsule.
  • Split weaving method single-sided PVC coating. (This airbag material weighs only 160 grams per square meter)
  • Figure 34 Vertical section view of the midge of the Hida.
  • Figure 35 Horizontal section of the midge of Hida.
  • Each airbag (76) is equipped with a self-sealing inflation valve (77) for filling and recovering helium; an electrically controlled (switchable) valve (78) for safely deflating the outside of the thorium; There are connections (89) for plastic pipes (88) from the two side tanks (8) (the Hida has four side tanks, and each airbag connects two side tanks).
  • the exhaust port (81) is essentially an electric control (switchable) valve; the functions of the various parts in the middle cabin are The following example illustrates: when the airbag (76) is inflated, helium gas is charged from the self-sealing inflation valve (77), the exhaust port (81) is opened at this time, and the air in the middle cabin is discharged from the exhaust port (81); the airbag (76) ) When the air is safely deflated, the exhaust port (81) is closed, the electric control (switchable) valve (78) of the airbag (76) is opened at this time, and the electric air blower (80) is filled with air into the middle compartment (9) The airbag (76), under the pressure of the air filled in the middle compartment (9), began to discharge helium from the electric control valve (78) to the outside of the thorium.
  • the flying saucer uses the static lift force of helium to balance the gravity of flying, so that the unique propulsion system of the flying hoop can exert its maximum functions.
  • the flying hoop can take off quickly and vertically, the carcass can fly in the air, hover in the air, and it can turn without any direction Fly forward and backward, land vertically, and shoot from any point in the air to any angle in the air.
  • the Hida can land on grass, mountains, and flat ground, and can hover on the water to work.
  • the side compartment itself is a seal: this sandwich panel forms a fire-resistant shell structure.
  • the engine is installed in this fire-resistant shell, and the Graviner flame control is also installed in the fire-resistant shell. Testing and fire extinguishing systems, each engine uses two fire extinguishing bottles.
  • Some parts of Hida engine can be made of silicon carbide fiber or silicon nitride fiber reinforced ceramics.
  • UFO longitudinal control and direction control the gas from the two-wing engine of the flying saucer is directly ejected from the rear reversible nozzle (the guide vanes are parallel to the nozzle at this time, and the gas is ejected in a straight line), generating forward thrust: at this time the tail engine gas Spraying upwards from the rear rotatable nozzle will generate a head-up torque (rotation of the rear rotatable nozzle and movement of the guide vanes), and the gas will be sprayed downward to generate a low head torque; the tail engine gas will be sprayed to the left or right. Will produce a yaw moment to the left or right.
  • UFO flying electronics also include: Very High Frequency ommidirectional Rang / Instrument Landing System (VHF omnidirectional beacon / instrument landing system); Distance Measuring Equipment (Measuring System) (made in the UK).
  • VHF omnidirectional beacon / instrument landing system Very High Frequency ommidirectional Rang / Instrument Landing System
  • Distance Measuring Equipment Measureasuring System
  • Figure 36 Schematic diagram of Feiyu weight balancing (bottom view)
  • the main fixed drill (82) is installed in the center of the UFO chassis (83) (vertical axis position), and the fixed hook (84) is installed on the left side; the auxiliary fixed drill (85) is installed on the right side of the cockpit (11), and the two-wing engine (13) ) On the horizontal axis (OZ).
  • the invention can be used for tourism, entertainment, short-distance passenger carrying, and long-distance transportation.

Abstract

Aérostat en forme de soucoupe volante comportant un compartiment latéral, un compartiment central, un système de propulsion, des éléments auxiliaires, des lampes à lumière intense, un poste de pilotage et une cabine de passagers. Le poids de l'aérostat est porté par la force de sustentation de l'hélium présent dans le compartiment latéral. Deux ballons d'hélium sont prévus dans le compartiment central et permettent de réguler l'altitude. Le système de propulsion est composé de deux réacteurs d'aile et d'un réacteur en queue. Les neuf tuyères de ces trois réacteurs peuvent tourner sur 360°. Les aubes directrices des tuyères peuvent se déplacer sur 80°. On détermine la direction des gaz expulsés par le système de propulsion en régulant des vannes et en faisant tourner les tuyères rotatives et les aubes directrices, afin de commander la tenue en vol de l'aérostat. Le poste de pilotage et la cabine de passagers se situent en dessous de la zone de chargement, du compartiment latéral et du compartiment central. Cet aérostat peut être utilisé pour les vols de plaisance ou les vols commerciaux sur de courtes distances et pour le transport de marchandises sur de longues distances.
PCT/CN1995/000026 1994-04-09 1995-04-04 Aeronef en forme de soucoupe volante WO1995027652A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU21342/95A AU2134295A (en) 1994-04-09 1995-04-04 Saucer-shaped aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN94207726U CN2188544Y (zh) 1994-04-09 1994-04-09 飞碟
CN94207726.1 1994-04-09

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Publication Number Publication Date
WO1995027652A1 true WO1995027652A1 (fr) 1995-10-19

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PCT/CN1995/000026 WO1995027652A1 (fr) 1994-04-09 1995-04-04 Aeronef en forme de soucoupe volante

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CN (1) CN2188544Y (fr)
AU (1) AU2134295A (fr)
WO (1) WO1995027652A1 (fr)

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CN108945484A (zh) * 2018-07-02 2018-12-07 山东理工大学 一种双向喷气飞行器
CN109866908B (zh) * 2019-03-06 2021-06-22 重庆理工大学 一种高压气体为动力的碟状飞行器
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US8616503B2 (en) 2007-08-09 2013-12-31 Lta Corporation Lenticular airship and associated controls
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USD670638S1 (en) 2010-07-20 2012-11-13 Lta Corporation Airship
US8894002B2 (en) 2010-07-20 2014-11-25 Lta Corporation System and method for solar-powered airship
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