Power and control module for model airplanes
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0339077
(1989-04-14)
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발명자
/ 주소 |
- Molina Joseph (6931 Glenview La. Lino Lakes MN 55014)
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인용정보 |
피인용 횟수 :
10 인용 특허 :
0 |
초록
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One feature of the present invention is a removable power and control module for a model airplane wherein the module mounts a great majority of the model airplane components such as the propeller, engine, gas tank, battery, radio receiver and servo motors. Accordingly, since the module is removable,
One feature of the present invention is a removable power and control module for a model airplane wherein the module mounts a great majority of the model airplane components such as the propeller, engine, gas tank, battery, radio receiver and servo motors. Accordingly, since the module is removable, repair and replacement of parts is facilitated. Another feature of the present invention is a number of levels of vibration isolators. One set of vibration suppressing soft mounts isolates the engine from the rest of the module; another set of soft mounts isolates the module from the model airplane. The soft mounts suppress engine produced vibrations which would otherwise be transmitted to the fuselage and skin-like covering of the model airplane and the airplane components. Since such vibrations contribute to the noise of a model airplane and to wear and tear on the airplane components, a quieter and more durable model airplane is an end result.
대표청구항
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A power and control module for a model airplane with a nose portion and maneuvering components including a rudder, elevators, stabilizer, wings and ailerons, comprising: a frame including front and rear sections and a firewall separating the sections, the frame being mountable within the model airpl
A power and control module for a model airplane with a nose portion and maneuvering components including a rudder, elevators, stabilizer, wings and ailerons, comprising: a frame including front and rear sections and a firewall separating the sections, the frame being mountable within the model airplane, power means including a propeller and motor for propelling the model airplane and being mounted on the front section of the frame, control means on the frame including a radio receiver and servomotor for receiving radio signals and connectable to such maneuvering components, the control means implementing the power means and such maneuvering components, energy source containing means on the frame for containing an energy source to be supplied to the motor, radio receiver and servomotor, means for connecting the frame to the model airplane, the connecting means including centering means on the frame cooperating with the model airplane to orient the module in the model airplane whereby the module is operable in or out of the model airplane and readily connectable to the model airplane to facilitate installation, maintenance, repair and reconstruction of the frame, the power means, the control means, the energy source containing means, the connecting means and other components of the model airplane.
이 특허를 인용한 특허 (10)
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Lai Aling,TWX, Assembling structure for landing gear of a model airplane.
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Nance, C. Kirk, Automated inspection of aircraft landing gear internal fluid levels.
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Nance, C. Kirk, Automated inspection of aircraft landing gear internal fluid levels.
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Stoughton, Philip Howard; Dietsch, Benjamin Allen; Durchholz, Anthony John; Eckert, Michael Charles, Dampers for fan spinners of aircraft engines.
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Delorio ; Jr. Ralph, Flexible shaft driven rotary control valve.
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Frontera Castaner, Miguel A., Model landing gear assembly.
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Amireh, Nicholas; Kang, Paulo; Strom, David; Chui, Chi Keung, Modular toy aircraft.
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Amireh, Nicholas; Kang, Paulo; Strom, David; Chui, Chi Keung, Modular toy aircraft with capacitor power sources.
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Zhao, Jie, Modularized airplane structures and methods.
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Newton, Jean Marie; Amireh, Nicholas, Toy flying aircraft.
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