CN2350097Y - Propelled electric remote-controlled toy aircraft - Google Patents

Propelled electric remote-controlled toy aircraft Download PDF

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Publication number
CN2350097Y
CN2350097Y CN 98225600 CN98225600U CN2350097Y CN 2350097 Y CN2350097 Y CN 2350097Y CN 98225600 CN98225600 CN 98225600 CN 98225600 U CN98225600 U CN 98225600U CN 2350097 Y CN2350097 Y CN 2350097Y
Authority
CN
China
Prior art keywords
remote control
fuselage
model
utility
propeller
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
CN 98225600
Other languages
Chinese (zh)
Inventor
田瑜
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHANGHAI PI'ENSI TELECOMMUNICATION ELECTRONICS CO Ltd
Original Assignee
SHANGHAI PI'ENSI TELECOMMUNICATION ELECTRONICS CO Ltd
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 SHANGHAI PI'ENSI TELECOMMUNICATION ELECTRONICS CO Ltd filed Critical SHANGHAI PI'ENSI TELECOMMUNICATION ELECTRONICS CO Ltd
Priority to CN 98225600 priority Critical patent/CN2350097Y/en
Application granted granted Critical
Publication of CN2350097Y publication Critical patent/CN2350097Y/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model discloses a propelled electric remote-controlled toy airplane, which comprises a fuselage, wings, a horizontal tail wing, a vertical tail wing, a motor provided with a propeller, a dynamic speed-regulating controller, a direction steering engine, and a power supply, a remote control transmission device, and a remote control receiving device. The utility model is characterized in that the motor which is provided with the propeller and produces push force is arranged on the rear part of an airplane head and the middle part of trailing edge the middle wing along the axial direction of the fuselage; the combination of the horizontal tail wing and the fuselage can be a fixed structure and a moveable structure. The utility model has the advantages of simple structure, low cost, high safety, convenient operation and remote control, etc.

Description

A kind of pusher electric remote control aircraft
The utility model relates to a kind of model airplane aircraft, is a kind of pusher electric remote control aircraft specifically.
The propeller of traditional remote control electric aircraft provides pulling force advances aircraft, thereby propeller is arranged at the head front portion usually, and such design breaks propeller when landing aircraft easily.The general four-channel remote control device that adopts on handling, the vertical aileron of one number service road control aircraft, No. two passage control aircraft power speed regulators, No. three passage control aircraft vertical tails, No. four passage control aircraft tailplanes.
The purpose of this utility model be to provide a kind of simple in structure, production cost is low, security is good, the pusher electric remote control aircraft of handiness.
To achieve these goals, the utility model adopts following technology, a kind of pusher electric remote control aircraft, comprise that fuselage, wing, tailplane, vertical tail, the motor that propeller is housed, power speed setting controller, the mechanical, electrical source of rudder, remote control emission and remote control receive, and is characterized in that: be equipped with motor that propeller produces thrust along fuselage be axially set in head the rear, in look the trailing edge middle part of the wing.
Good effect of the present utility model is: owing to drive the trailing edge middle part that the motor of propeller generation thrust is arranged at the rear of head, middle wing, thereby security is relatively good, is difficult for breaking propeller and motor after clashing into; Again, tailplane and fuselage combination can be fixed structures, saved control to tailplane, thereby make the utility model simple in structure, production cost is low, by traditional employing four-channel remote control device, uses the binary channels remote controller instead and can control left and right sides flight attitude under the worker of aircraft, about realizing, one number service road control aircraft vertical tail turns the speed and the pitching cover attitude of No. two passage control aircraft stepless speed adjusting gear control aircrafts.
Fig. 1 is the structural representation of a preferred embodiment of the utility model;
Fig. 2 is a preferred embodiment outward appearance of a utility model schematic top plan view.
See also illustrated in figures 1 and 2, the utility model by fuselage 2, wing, tailplane 6, vertical tail 9, the motor 1 that propeller 5 is housed, power speed setting controller 10, direction steering wheel 12, power supply 13, remote control receive 14 and remote control emission (not shown) etc. form.Wing of the present utility model is made up of port wing 8, middle wing 4 and starboard wing 7.The utility model tailplane 6 and the fuselage 2 employing fixed structure of organizing a performance, thereby saved tailplane 6 controls, the lifting of aircraft realizes by the speed of regulating aircraft.The utility model dynamical system is made up of propeller 5, motor 1, motor switch 11, power speed setting controller 10 and power supply 13, power supply adopt seven nickel-cadmium cell.Motor 1 axially is installed on the rear of head 3, the trailing edge middle part of middle wing 4 along fuselage 2.The propeller 5 that produces thrust is installed on the motor drive shaft.
Manipulation of the present utility model uses the binary channels remote controller to control the attitude up and down of aircraft, one number service road controlling party realizes that to steering wheel 12, vertical tail 9 there is turning on a left side, the speed and the lifting of No. two passage control power speed setting controller 10 control aircrafts.
Tailplane 6 of the present utility model as required also can be a bascule with fuselage 2 combinations.

Claims (3)

1. pusher electric remote control aircraft, comprise that fuselage, wing, tailplane, vertical tail, the motor that propeller is housed, power speed setting controller, the mechanical, electrical source of rudder, remote control emission and remote control receive, and is characterized in that: the motor (1) that propeller (5) generation thrust is housed is axially set in the trailing edge middle part of the rear of head (3), middle wing (4) along fuselage (2).
2. a kind of pusher electric remote control aircraft according to claim 1 is characterized in that: described tailplane (6) can be a fixed structure with fuselage (2) combination.
3. a kind of pusher electric remote control aircraft according to claim 1 is characterized in that: described tailplane (6) can be a bascule with fuselage (2) combination.
CN 98225600 1998-11-11 1998-11-11 Propelled electric remote-controlled toy aircraft Expired - Lifetime CN2350097Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 98225600 CN2350097Y (en) 1998-11-11 1998-11-11 Propelled electric remote-controlled toy aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 98225600 CN2350097Y (en) 1998-11-11 1998-11-11 Propelled electric remote-controlled toy aircraft

Publications (1)

Publication Number Publication Date
CN2350097Y true CN2350097Y (en) 1999-11-24

Family

ID=33976261

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 98225600 Expired - Lifetime CN2350097Y (en) 1998-11-11 1998-11-11 Propelled electric remote-controlled toy aircraft

Country Status (1)

Country Link
CN (1) CN2350097Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002007844A1 (en) * 2000-07-14 2002-01-31 Shanghai Helang Electronics Co., Ltd. The electric remote-controlled airplane
WO2003035203A1 (en) * 2001-10-26 2003-05-01 Yu Tian Remote-controlled ultrasonic transmitting firing aircraft

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002007844A1 (en) * 2000-07-14 2002-01-31 Shanghai Helang Electronics Co., Ltd. The electric remote-controlled airplane
GB2380690A (en) * 2000-07-14 2003-04-16 Shanghai Helang Electronic Co The electronic remote-controlled airplane
GB2380690B (en) * 2000-07-14 2004-07-21 Shanghai Helang Electronic Co Remote electro-aeroplane
WO2003035203A1 (en) * 2001-10-26 2003-05-01 Yu Tian Remote-controlled ultrasonic transmitting firing aircraft
GB2398026A (en) * 2001-10-26 2004-08-11 Yu Tian Remote-controlled ultrasonic transmitting firing aircraft
GB2398026B (en) * 2001-10-26 2006-05-10 Yu Tian Remote-controlled ultrasonic transmitting firing aircraft

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C53 Correction of patent for invention or patent application
COR Change of bibliographic data

Free format text: CORRECT: PATENTEE ADDRESS; FROM: 19F, NO. 1, LANE 99, JIANGCAO ROAD(SOUTH), SHANGHAI CITY, 200233 TO: NO. 1935-1, CAOAN ROAD, SHANGHAI CITY, 201803

CP02 Change in the address of a patent holder

Address after: 201803 Shanghai City Caoan Road No. 1935-1 Zheng Dongcheng

Patentee after: Shanghai Piens Telecommunications Electronics Co., Ltd.

Address before: 200233, 19F, Tian Tian Yu, No. 99, Lane 1, rainbow South Road, Shanghai

Patentee before: Shanghai Piens Telecommunications Electronics Co., Ltd.

C53 Correction of patent for invention or patent application
COR Change of bibliographic data

Free format text: CORRECT: PATENTEE ADDRESS; FROM: (P.S. TO: NO. 1991-1, CAOAN ROAD, SHANGHAI CITY, 201803

CP03 Change of name, title or address

Address after: 201803 Shanghai City Caoan Road No. 1991-1 Yang Wenfang Zheng Dongcheng

Patentee after: Shanghai Piens Telecommunications Electronics Co., Ltd.

Address before: (Note: the original address is incorrect)

Patentee before: Shanghai Piens Telecommunications Electronics Co., Ltd.

AV01 Patent right actively abandoned
C20 Patent right or utility model deemed to be abandoned or is abandoned