WO2019074393A1 - Летательный аппарат - Google Patents
Летательный аппарат Download PDFInfo
- Publication number
- WO2019074393A1 WO2019074393A1 PCT/RU2018/000281 RU2018000281W WO2019074393A1 WO 2019074393 A1 WO2019074393 A1 WO 2019074393A1 RU 2018000281 W RU2018000281 W RU 2018000281W WO 2019074393 A1 WO2019074393 A1 WO 2019074393A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- hull
- annular
- plane
- ring
- Prior art date
Links
- 230000007246 mechanism Effects 0.000 claims description 2
- 238000005096 rolling process Methods 0.000 abstract description 3
- 240000002836 Ipomoea tricolor Species 0.000 abstract description 2
- 230000001413 cellular effect Effects 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
Definitions
- the present invention relates to the field of aircraft (LA), can serve as an alternative to the helicopter fleet, has a range of applications from children's toys, unmanned lifting devices to mainline L A.
- the present invention is a further development of the LA, presented in the specified patent.
- the claimed invention can serve as a pilot of a new class of aircraft with the conventional name “Zan” (ZAN), where, in contrast to the class “helicopters”, instead of the rotor of the helicopter, a closed multi-blade annular fan wheel (CVC) is used with a rotary drive on therefore, there is no central shaft, which causes the rotation of the HB.
- ZAN conventional name “Zan”
- CVC closed multi-blade annular fan wheel
- a fan wheel with controlled direct blades is considered as a propeller.
- the aim of the present invention is to provide an aircraft in which the thrust and the possibility of wide maneuvering are provided by an annular yoke (QD) located around the hull and consisting of two propellants in the form of annular fan wheels.
- QD annular yoke
- This goal is achieved by the fact that the aircraft contains a body made in the form of a lenticular body of rotation, while part of the body of which has the form of a spherical layer, on the side surface of which for transmitting thrust and for maneuvering the aircraft, rolling motion KO. At the same time, there is a gap between the surface of the convex ball layer and the concave QO surface, so that these structural elements do not touch each other.
- the propellers are protected by a casing fairing and guide and rectifying devices, which excludes the possibility of damage to the fan wheels with blades when the aircraft contacts the trees, houses, power lines, etc. Also, in the event of an emergency for the flight personnel of the aircraft, it became possible to safely evacuate up or down (along the Z axis), eject or install parachute systems.
- the present invention includes various options for manned and for unmanned use of aircraft.
- the ball layer in the context of the present invention means the part of the ball bounded by two parallel planes intersecting the ball (https: // m. Wikipedia.org/wiki/%D0%A8%D0%B0%D1%80%D0BE%D0% B2% D0% BE% D0% B9% D 1% 81% D0% BB% D0% BE% D0% B9 (viewed September 20, 2017).
- the lenticular shape of the aircraft body provides good streamlining by the oncoming air flow during flight.
- the convex part of the lenticular shape of the aircraft falls on the cockpit, which ensures good visibility during flight.
- An annular cage (KO) is used as a propulsor located around the body of an aircraft, while it consists of two annular fan wheels (ICC) located one below the other and rotating in opposite directions with.
- the thrust vectoring is controlled by running KO around the spherical layer of the LA body by force action through 4 vertical slots (2 along the X axis and 2 along the Y axis) in its lateral surface.
- FIG. 1 shows a general view of the aircraft
- FIG. 2 shows an annular cage of a small LA
- FIG. 3 shows an annular holder of a large aircraft.
- the proposed LA has the appearance of a “flying saucer” and resembles the astronomical fact of the location of the rings of the planet Saturn, while in LA there is the possibility of inclining the plane of the rings relative to the subject.
- annular holder KO 2 details Fig. 2 and Fig. 3
- annular fan wheels 5 and 7 rotating in opposite directions (coaxial scheme) and representing each of the inner and outer rims located between them controlled blades, which are rotated by mechanical drive systems (gear), electromagnetic, gas-dynamic or other methods.
- KVK separated stationary intermediate guide air flow apparatus 6 in the cavities of which can accommodate drive systems.
- the first KVK 5 there is a fixed guide vane of a lattice or cellular type 4, forming an air flow at its entrance, and after the second KVK 7 there is a stationary rectifying device also of a lattice or cellular type 8, organizing the air flow at its exit.
- a stationary rectifying device also of a lattice or cellular type 8, organizing the air flow at its exit.
- KO 2 is inclined in the case of small LA forms (FIG. 2) by controlling the crosspiece 10 attached to the CO through 4 vertical slots in the side walls of the LA ball layer (one of them is indicated at 11 in Fig.
- Manipulating the KO 2 causes the maneuvering of the aircraft, which may cause the pilot and crew to differ from the direction of the thrust vector of the aircraft, therefore the combination of directions is provided by the on-board computer controlled misalignment of the rotational speeds of the KVK 5, 7 using controlled blades or the driving system of one or the other KVK.
- the design of the aircraft body to increase its capacity allows for the addition of another lenticular module with the placement of fuel tanks, passenger seats, combat or cargo equipment, retractable landing gear, etc.
- the shape of the aircraft in this case will look like a flattened figure "8" with a ring clip on the upper half. Placing an additional main engine in the module will allow to obtain high subsonic flight speeds.
- the claimed invention also differs increased speed characteristics, increased carrying capacity, reducing vertical dimensions, increasing the safety of the aircraft.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2017136177A RU2668541C1 (ru) | 2017-10-12 | 2017-10-12 | Летательный аппарат |
RU2017136177 | 2017-10-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2019074393A1 true WO2019074393A1 (ru) | 2019-04-18 |
Family
ID=63798102
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/RU2018/000281 WO2019074393A1 (ru) | 2017-10-12 | 2018-04-28 | Летательный аппарат |
Country Status (2)
Country | Link |
---|---|
RU (1) | RU2668541C1 (ru) |
WO (1) | WO2019074393A1 (ru) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2336199C1 (ru) * | 2007-02-16 | 2008-10-20 | Эдуард Дмитриевич Житников | Стратегический вертолет |
RU82674U1 (ru) * | 2008-11-11 | 2009-05-10 | Жак Андрэ Морис Жонио | Беспилотный летательный аппарат вертолетного типа |
US20100264256A1 (en) * | 2009-04-16 | 2010-10-21 | The Trustees Of The University Of Pennsylvania | Counter-rotational inertial control of rotorcraft |
RU2617014C1 (ru) * | 2016-04-11 | 2017-04-19 | Светослав Владимирович Занегин | Летательный аппарат |
WO2017125923A1 (en) * | 2016-01-20 | 2017-07-27 | N.M.B. Medical Applications Ltd | System, assemblies and methods for mechanical-thrust power conversion multifans |
-
2017
- 2017-10-12 RU RU2017136177A patent/RU2668541C1/ru active
-
2018
- 2018-04-28 WO PCT/RU2018/000281 patent/WO2019074393A1/ru active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2336199C1 (ru) * | 2007-02-16 | 2008-10-20 | Эдуард Дмитриевич Житников | Стратегический вертолет |
RU82674U1 (ru) * | 2008-11-11 | 2009-05-10 | Жак Андрэ Морис Жонио | Беспилотный летательный аппарат вертолетного типа |
US20100264256A1 (en) * | 2009-04-16 | 2010-10-21 | The Trustees Of The University Of Pennsylvania | Counter-rotational inertial control of rotorcraft |
WO2017125923A1 (en) * | 2016-01-20 | 2017-07-27 | N.M.B. Medical Applications Ltd | System, assemblies and methods for mechanical-thrust power conversion multifans |
RU2617014C1 (ru) * | 2016-04-11 | 2017-04-19 | Светослав Владимирович Занегин | Летательный аппарат |
Also Published As
Publication number | Publication date |
---|---|
RU2668541C1 (ru) | 2018-10-01 |
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