CS252549B1 - Self-propelled radio controlled trainer model - Google Patents
Self-propelled radio controlled trainer model Download PDFInfo
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- CS252549B1 CS252549B1 CS863025A CS302586A CS252549B1 CS 252549 B1 CS252549 B1 CS 252549B1 CS 863025 A CS863025 A CS 863025A CS 302586 A CS302586 A CS 302586A CS 252549 B1 CS252549 B1 CS 252549B1
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Abstract
Trenažér má naučit pilota-začiatočníka ovládať model lietadla v akejkolvek polohe v priestore, kde sú nebezpečia havárie. V trenažéri je uložený model v sebeotočných kruhoch umiestnených v rámu. Riešenie umožňuje sledovat reakcie lietadla na povely pilota alebo naopak nacvičit si reakcie na jednotlivé polohy lietadla.The simulator is intended to teach a novice pilot to control a model aircraft in any position in an area where there is a risk of an accident. The simulator stores the model in self-rotating rings located in the frame. The solution allows you to monitor the aircraft's reactions to the pilot's commands or, conversely, to practice reactions to individual aircraft positions.
Description
Vynález sa týká trenažéra pre modely lietadiel rádlom riadených s vlastným pohonom najma pre pilotov začiatočníkov.The present invention relates to a trainer for self-propelled self-propelled aircraft models, in particular for beginners.
V súčasnej době modely lietadiel rádioni riadených s vlastným pohonom pilot začiatočník začína ovládat model lietadla na štartovacej dráhe a potom vo votnom priestore.Currently, self-propelled self-propelled aircraft models pilot beginner control of the aircraft on the take-off runway and then in the flight area.
Takéto lietanie pilot začína sám připadne s inštruktorom, ale dochádza často k haváriam. K haváriam dochádza z důvodov zlých reakcií pilota na polohu lietadla v priestore. Na ovládanie modelu lietadla musí reagovat pilot velmi rýchle, a preto musí mať nacvičené reakcie na ovládanie modelu lietadla v jeho jednotlivých polohách.Such a flying pilot starts with himself or with an instructor, but accidents often occur. Accidents occur because of the pilot's bad reactions to the position of the aircraft in space. The pilot must respond very quickly to the aircraft model control, and therefore must have practiced responses to the aircraft model control in its individual positions.
V súčasnej době je známe závěsné zariadenie na cvičenie pilotov rádiom riadených modelov s vlastným pohonom, ktoré je náročné na zvětšený priestor a má omedzujúce kotvenie.At present, a self-propelled, self-propelled, pendulum-driveable pendulum training device is required, which is space-demanding and restricting anchoring.
Horeuvedené nedostatky odstraňuje trenažér pre modely lietadiel rádiom riadených s vlastným pohonom, ktorý pozostáva zo stojana a z troch kruhov, kde model lietadla je upevněný v príchytke spojenej s vnútorným kruhom otočné uloženého v proštrednom kruhu, ktorý je uložený v o vonkajšom kruhu a je uložený otočené na stojane a časť prúdu vzduchu je usměrněný na krídelká modelu lietadla osmerňovačom prúdu vzduchu.The above deficiencies are eliminated by the self-propelled radio-controlled trainer, which consists of a stand and three rings, where the aircraft model is mounted in a clip attached to an inner ring rotatably mounted in a center ring which is mounted in an outer ring and rotated on a stand. and a portion of the airflow is directed to the wings of the aircraft model by the airflow rectifier.
Zariadenie podl'a vynálezu má hlavnú výhodu v tom, že umožňuje lietadlo uviesť do akejkol'vek polohy ako pri pilotáži v priestore, bez nebezpečia havárie. Pilot riadi vysielačkou model lietadla s malej vzdialenosti a může sledovat reakcie lietadla na povely pilota, alebo naopak nacvičit si reakcie na jednotlivé polohy lietadla.The device according to the invention has the main advantage that it allows the aircraft to be brought to any position as in piloting in the area, without the risk of an accident. The pilot controls the model of a small-distance aircraft by radio and can observe the reactions of the aircraft to the pilot's commands or, conversely, practice the reactions to individual aircraft positions.
Na výkrese je znázorněné zariadenie v axonometrickom pohlade. Model 1 lietadla je upevněný v príchytke 2 spojenej s vnútorným kruhom 3 s otočným uložením 6. Vnútorný kruh 3 je otáčaný lietadlom vychýlením výškovky riadenej rádiovým vysielačom 9. Prostredný kruh 4 je upevněný v otočnom uložení B a je otáčaný lietadlom vychýlením směrovky riadenej vysielačom 9. Vonkajší kruh 5 je upevněný v otočnom uložení B na stojane 8. Časť prúdu vzduchu od vrtule je usměrněná na krídelká usmerňovačom 7 prúdu vzduchu. Vonkajší kruh 5 je otočný vychýlením krídelek modelu 1 lietadla riadených vysielačom 9.The drawing shows the device in axonometric view. The aircraft model 1 is mounted in a clip 2 connected to the inner ring 3 with a pivot bearing 6. The inner ring 3 is rotated by the aircraft by deflecting the radio-controlled elevation 9. The outer ring 5 is mounted in a pivot bearing B on the stand 8. A portion of the air stream from the propeller is directed to the wings by the air stream baffle 7. The outer ring 5 is rotatable by deflecting the wings of the aircraft model 1 controlled by the transmitter 9.
Zariadenie podl'a vynálezu pracuje takto: model 1 lietadla sa upevní příchytkami 2 spojených s otočným uložením B a vnútorným kruhom 3, nastaví sa usměrňovač 7 prúdu vzduchu tak, aby časť prúdu vzduchu směroval na krídelká. Uvedia sa do činnosti vysielač 9 a přijímač so servopohonmi umiestnenými v lietadle, ďalej uvedie sa do činnosti motor lietadla, ktorý naháňa vzduch na krídelká, výškovku a směrovku. Vychýlením směrovky, výškovky alebo krídeliek model 1 reaguje ako pri lete vo vol'nom priestore. Pilot s l'ubovol'nej vzdialenosti može začat ovládat lietadlo.The device according to the invention operates as follows: the aircraft model 1 is fixed by clips 2 connected to the pivot bearing B and the inner ring 3, the air flow baffle 7 is adjusted so that part of the air flow is directed towards the wings. The transceiver 9 and the actuator with actuators located in the aircraft are actuated, the aircraft engine is activated, which drives the air onto the wings, elevator and rudder. By deflecting the rudder, elevator or ailerons, the Model 1 reacts like in the open air. A pilot with any distance can start to operate the aircraft.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CS863025A CS252549B1 (en) | 1986-04-25 | 1986-04-25 | Self-propelled radio controlled trainer model |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CS863025A CS252549B1 (en) | 1986-04-25 | 1986-04-25 | Self-propelled radio controlled trainer model |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CS302586A1 CS302586A1 (en) | 1987-01-15 |
| CS252549B1 true CS252549B1 (en) | 1987-09-17 |
Family
ID=5369121
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CS863025A CS252549B1 (en) | 1986-04-25 | 1986-04-25 | Self-propelled radio controlled trainer model |
Country Status (1)
| Country | Link |
|---|---|
| CS (1) | CS252549B1 (en) |
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1986
- 1986-04-25 CS CS863025A patent/CS252549B1/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| CS302586A1 (en) | 1987-01-15 |
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