FIELD: aircraft engineering.
SUBSTANCE: invention relates to the field of combined vehicles, in particular to the designs of aircraft based on cars. A feature of the construction of the aircraft is the absence of an open main rotor and its small dimensions, which allows it to fit into the dimensions of the car. The device provides a complete separation of air flows between the main rotor and the impeller with two blade crowns, which is achieved by means of a separation device fixed between them, located between the main rotor and the impeller and a small cup inside which a bearing is mounted connected to the upper edge of the engine shaft. The device is also equipped with a small cup with a bearing, which is connected to the upper edge of the motor shaft and mounted on centered spacers connected to the aircraft body, under a protective mesh. The separation device is made of an annular diaphragm, a cylindrical ring, thin-walled partitions of guide channels evenly spaced around the circumference, the outer edge of the annular diaphragm is connected to the end of the cylindrical ring, and the ring itself is connected to the body of the aircraft. The gearbox is connected to the main rotor and the motor shaft.
EFFECT: reliability and efficiency of the aircraft are improved.
1 cl, 10 dwg
Title |
Year |
Author |
Number |
AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING (SOLOUKHINA'S DEVICE) |
2019 |
- Soloukhin Nikolaj Dmitrievich
|
RU2713751C1 |
VTOL AIRCRAFT (E.N. SOLUKHINA'S CRAFT) |
2017 |
- Soloukhina Ekaterina Nikolaevna
- Soloukhin Nikolaj Dmitrievich
|
RU2652423C1 |
VTOL AIRCRAFT (E SOLOUKHINA'S CRAFT) |
2014 |
- Soloukhina Ekaterina Nikolaevna
- Soloukhin Nikolaj Dmitrievich
|
RU2560172C9 |
"MAXINIO" STANDARD TECHNOLOGY OF VEHICLE MANUFACTURING AND OPERATION, NO-RUN TAKE-OFF AND LANDING ELECTRIC AIRCRAFT (VERSIONS), LIFTING DEVICE, TURBO-ROTARY ENGINE (VERSIONS), MULTISTEP COMPRESSOR, FAN COWLING, TURBO-ROTARY ENGINE OPERATION METHOD AND METHOD OF ELECTRIC AIRCRAFT LIFTING FORCE CREATION METHOD |
2010 |
- Maksimov Nikolaj Ivanovich
|
RU2457153C2 |
AXISYMMETRIC AIRCRAFT |
2022 |
- Kotelkin Vyacheslav Dmitrievich
|
RU2789464C1 |
PISTON-TYPE ELECTROHYDRAULIC ENGINE AND ITS CONTROL PROCESS |
1996 |
- Soloukhina Ekaterina Nikolaevna
- Soloukhin Nikolaj Dmitrievich
|
RU2107835C1 |
GAS TURBINE ENGINE LOW-PRESSURE TURBINE (LPT) (VERSIONS), ROTOR SHAFT CONNECTION UNIT WITH LPT DISC, LPT ROTOR AIR COOLING PATH AND AIR FEEDING APPARATUS FOR COOLING LPT ROTOR BLADES |
2018 |
- Marchukov Evgenij Yuvenalevich
- Kuprik Viktor Viktorovich
- Andreev Viktor Andreevich
- Zolotukhin Andrej Aleksandrovich
- Komarov Mikhail Yurevich
- Kononov Nikolaj Aleksandrovich
- Krylov Nikolaj Vladimirovich
- Selivanov Nikolaj Pavlovich
|
RU2684355C1 |
ROTOR "AIR WHEEL", GYROSTABILISED AIRCRAFT AND WIND-DRIVEN ELECTRIC PLANT USING ROTOR "AIR WHEEL", SURFACE/DECK DEVICES FOR THEIR START-UP |
2013 |
|
RU2538737C9 |
INTEGRATED TECHNOLOGY OF OPERATION AND PRODUCTION "MAXINIO" TRANSPORT FACILITIES: VTOL ELECTRIC AIRCRAFT (VERSIONS), ELECTRIC AIRCRAFT UNITS AND METHODS OF EMPLOYMENT ELECTRIC AIRCRAFT AND ITS PARTS |
2010 |
- Maksimov Nikolaj Ivanovich
|
RU2466908C2 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE |
2016 |
- Marchukov Evgenij Yuvenalevich
- Erichev Dmitrij Yurevich
- Ilyasov Sergej Anatolevich
- Kuprik Viktor Viktorovich
- Savchenko Aleksandr Gavrilovich
- Shishkova Olga Vladimirovna
- Selivanov Nikolaj Pavlovich
|
RU2614709C1 |