[go: up one dir, main page]

CN104548616B - A kind of telecontrolled aircraft - Google Patents

A kind of telecontrolled aircraft Download PDF

Info

Publication number
CN104548616B
CN104548616B CN201410683946.2A CN201410683946A CN104548616B CN 104548616 B CN104548616 B CN 104548616B CN 201410683946 A CN201410683946 A CN 201410683946A CN 104548616 B CN104548616 B CN 104548616B
Authority
CN
China
Prior art keywords
fuselage
propeller
fixed
protecting bin
rear portion
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.)
Active
Application number
CN201410683946.2A
Other languages
Chinese (zh)
Other versions
CN104548616A (en
Inventor
不公告发明人
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201410683946.2A priority Critical patent/CN104548616B/en
Publication of CN104548616A publication Critical patent/CN104548616A/en
Application granted granted Critical
Publication of CN104548616B publication Critical patent/CN104548616B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

A kind of telecontrolled aircraft, including fuselage, two wings and tail, two wings are respectively symmetrically fixed at two side of fuselage, tail is fixed at the rear portion of fuselage, protecting bin is fixedly installed in the lower-end rear portion of fuselage, receiver of remote-control sytem is fixed in protecting bin, fuselage afterbody is provided with propeller slot, motor is fixed at the front end of propeller slot, and it is located on fuselage, propeller on motor output shaft is arranged in propeller slot, it is fixedly installed multiple V-type landing chassis respectively in the front lower ends of fuselage and the lower end of protecting bin, the a line of multiple V-type landing chassis is respectively fixedly disposed in the front lower ends of fuselage and the lower end surface of protecting bin.The present invention has many advantages, such as that structure is simple, materials are convenient, safe and reliable, flight effect is good.

Description

A kind of telecontrolled aircraft
Technical field:
The present invention relates to aviation model field, in particular to a kind of improvement of telecontrolled aircraft structure.
Background technique:
Telecontrolled aircraft is a kind of self-powered, small aircraft to be flown by remote control control, and conventional remote control flies Machine is made into using the materials such as cork wood or foamed plastics, and take-off and landing device is all the steamboat of installation as sliding.It is existing not Foot is when landing on a land with a bumpy road, easily telecontrolled aircraft to be caused to turn over since telecontrolled aircraft wheel is smaller Damage model aircraft is rolled, that structure is complicated is at high cost for these model of an airplanes, and can only be formed and be produced by producer, and being broken will be by giving birth to Factory repair or replacement are produced, greatly improves the cost of telecontrolled aircraft in this way, is caused to model of an airplane fan economical negative Load.
Summary of the invention:
The purpose of the present invention, it is simple to be to provide a kind of structure, easy to use, when the model plane landed, does not easily cause winged A kind of telecontrolled aircraft of machine damage.
The technical solution adopted is that:
A kind of telecontrolled aircraft, including fuselage, two wings and tail, two wings are respectively symmetrically fixed at fuselage two Side, tail are fixed at the rear portion of fuselage, are fixedly installed protecting bin in the lower-end rear portion of fuselage, receiver of remote-control sytem fixation is set It sets in protecting bin, it is characterized in that being provided with propeller slot in fuselage afterbody, motor is fixed at the front end of propeller slot, and On fuselage, the propeller on motor output shaft is arranged in propeller slot, under the front lower ends of fuselage and protecting bin End is fixedly installed multiple V-type landing chassis respectively, and a line of multiple V-type landing chassis is respectively fixedly disposed under the front of fuselage On end and the lower end surface of protecting bin.
The beneficial effects of the present invention are: V-type landing chassis due to the adoption of the above technical scheme, can make telecontrolled aircraft fly When reduce resistance, and can make telecontrolled aircraft what ground environment in office all can safe landing, avoid the damage of the remote control plane, separately Outside, propeller is damaged when being placed in propeller slot by propeller and can avoid aircraft landing out of control.The present invention is simple with structure, takes The advantages that material is convenient, safe and reliable, flight effect is good.
Detailed description of the invention:
Fig. 1 is a kind of example structure schematic diagram of the invention;
Fig. 2 is the rearview of Fig. 1;
Fig. 3 is side view of the present invention.
Specific embodiment:
Embodiment one
A kind of telecontrolled aircraft, including 1, two wing 2 of fuselage and tail 3, two wings 2 are respectively symmetrically fixed at machine 1 two side of body, tail 3 are fixed at the rear portion of fuselage 1, are fixedly installed protecting bin 4 in the lower-end rear portion of fuselage 1, remote control connects It receives device to be fixed at 4 in protecting bin, 1 rear portion of fuselage is provided with propeller slot 6, motor 7 is fixed at propeller slot 6 Front end, and be located on fuselage 1, the propeller 8 on 7 output shaft of motor is arranged in propeller slot 6, can avoid aircraft landing out of control When propeller 8 damage.It is fixedly installed multiple V-type landing chassis 5 respectively in the front lower ends of fuselage 1 and the lower end of protecting bin 4, it is more The a line of a V-type landing chassis 5 is respectively fixedly disposed in the front lower ends of fuselage 1 and the lower end surface of protecting bin 4, uses V-type Landing chassis 5 can make telecontrolled aircraft what ground environment in office all can safe landing.

Claims (1)

1. a kind of telecontrolled aircraft, including fuselage (1), two wings (2) and tail (3), respectively symmetrically fixation is set two wings (2) It sets in (1) two side of fuselage, tail (3) is fixed at the rear portion of fuselage (1), is fixedly installed in the lower-end rear portion of fuselage (1) Protecting bin (4), receiver of remote-control sytem are fixed in protecting bin (4), it is characterized in that being provided with propeller slot at fuselage (1) rear portion (6), motor (7) is fixed at the front end of propeller slot (6), and is located on fuselage (1), the spiral on motor (7) output shaft Paddle (8) setting is fixedly installed more respectively in propeller slot (6) in the front lower ends of fuselage (1) and the lower end of protecting bin (4) The a line of a V-type landing chassis (5), multiple V-type landing chassis (5) is respectively fixedly disposed at the front lower ends and protection of fuselage (1) On the lower end surface in storehouse (4).
CN201410683946.2A 2014-11-25 2014-11-25 A kind of telecontrolled aircraft Active CN104548616B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410683946.2A CN104548616B (en) 2014-11-25 2014-11-25 A kind of telecontrolled aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410683946.2A CN104548616B (en) 2014-11-25 2014-11-25 A kind of telecontrolled aircraft

Publications (2)

Publication Number Publication Date
CN104548616A CN104548616A (en) 2015-04-29
CN104548616B true CN104548616B (en) 2019-01-04

Family

ID=53066344

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410683946.2A Active CN104548616B (en) 2014-11-25 2014-11-25 A kind of telecontrolled aircraft

Country Status (1)

Country Link
CN (1) CN104548616B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105194882A (en) * 2015-09-21 2015-12-30 重庆燕蓝科技有限公司 Aeromodelling airplane seating frame
CN106823403B (en) * 2017-03-07 2024-06-14 王长民 Multi-oar remote control plane

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2201975Y (en) * 1993-01-05 1995-06-28 徐自毅 Toy plane with electric propeller
CN2598606Y (en) * 2003-03-06 2004-01-14 毛宗泽 Toy helicopter with seat
CN201091795Y (en) * 2007-09-14 2008-07-30 陈灿波 Single wing remote control toy airplane
CN101961974A (en) * 2010-09-15 2011-02-02 北京理工大学 Land, water and air multi-domain engine-driven carriage vehicle
CN203494164U (en) * 2013-09-30 2014-03-26 李欧 Telecontrolled aircraft with propulsion propeller
CN204319765U (en) * 2014-11-25 2015-05-13 王长民 A kind of telecontrolled aircraft

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2201975Y (en) * 1993-01-05 1995-06-28 徐自毅 Toy plane with electric propeller
CN2598606Y (en) * 2003-03-06 2004-01-14 毛宗泽 Toy helicopter with seat
CN201091795Y (en) * 2007-09-14 2008-07-30 陈灿波 Single wing remote control toy airplane
CN101961974A (en) * 2010-09-15 2011-02-02 北京理工大学 Land, water and air multi-domain engine-driven carriage vehicle
CN203494164U (en) * 2013-09-30 2014-03-26 李欧 Telecontrolled aircraft with propulsion propeller
CN204319765U (en) * 2014-11-25 2015-05-13 王长民 A kind of telecontrolled aircraft

Also Published As

Publication number Publication date
CN104548616A (en) 2015-04-29

Similar Documents

Publication Publication Date Title
CN204489181U (en) Variable motor angle four axle vertical takeoff and landing fixed-wing compound unmanned plane
WO2015143093A3 (en) Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
EP4417510A3 (en) Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
CN204355275U (en) There is the aircraft of safe propulsion system
CN202609086U (en) Downwards-throwing popup type parachute opening device of unmanned plane
WO2015143098A3 (en) Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
CN204210731U (en) Autogyro
CN105015770A (en) Vertical take-off and landing aircraft with wing body blended with single duct
CN104548616B (en) A kind of telecontrolled aircraft
CN104992586A (en) Airplane system capable of realizing flight experience
CN204021250U (en) A kind of have the round wing unmanned plane blowing wing mechanism
CN203842313U (en) Novel remote control model with combination of vertical take-off and landing and level fight characteristic of fixed wing
CN104548619A (en) Triphibian toy plane
CN204319765U (en) A kind of telecontrolled aircraft
CN203032936U (en) Passenger helicopter
CN106494604A (en) Hollow long endurance unmanned aircraft total arrangement
CN205044987U (en) Aircraft goes up and down to assist flying platform
CN103708029A (en) Light aircraft
CN206502016U (en) A kind of all-wing aircraft unmanned plane of vertical lift
CN204159032U (en) A kind of ejection model airplane
CN206404320U (en) A kind of remote-controlled unmanned vehicle
WO2011089458A3 (en) Airplane with aerodynamic stall-prevention layout and pertinent longitudinal stability arrangement
CN202379089U (en) Novel unmanned aerial vehicle
CN206518880U (en) Remote control amphibious aircraft
CN205730360U (en) A kind of four rotor flying model plane for detecting landform

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant