CN106621363A - Flight device with two power devices - Google Patents

Flight device with two power devices Download PDF

Info

Publication number
CN106621363A
CN106621363A CN201510740899.5A CN201510740899A CN106621363A CN 106621363 A CN106621363 A CN 106621363A CN 201510740899 A CN201510740899 A CN 201510740899A CN 106621363 A CN106621363 A CN 106621363A
Authority
CN
China
Prior art keywords
wheel
break
rotary shaft
power set
connecting rod
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.)
Withdrawn
Application number
CN201510740899.5A
Other languages
Chinese (zh)
Inventor
马铿杰
Original Assignee
马铿杰
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 马铿杰 filed Critical 马铿杰
Priority to CN201510740899.5A priority Critical patent/CN106621363A/en
Publication of CN106621363A publication Critical patent/CN106621363A/en
Withdrawn legal-status Critical Current

Links

Abstract

The invention provides a flying device with two power devices. The flying device includes a main power device, an auxiliary power device and a connecting rod; the main power device and the auxiliary power device are connected through the connecting rod, and the remote control flying toy greatly simplifies the overall structure of a model airplane, also reduces the weight of a plane body, effectively reduce the energy consumption and prolongs the flight time.

Description

Flight instruments with two power set
Technical field
The present invention relates to model plane field, espespecially a kind of flight instruments with two power set.
Background technology
General aeromodelling airplane by can belt transmission or gear drive drive the rotation of whole steering mechanism, the long-term friction in belt transmission due to belt is using causing larger abrasion so that steering mechanism's control is inaccurate;And gear-driven Power Component is made up of several gear reduction units, general airframe structure is complex, and increased the overall weight of fuselage, and weight increase will increase energy consumption.
In view of this, it is desirable to provide a kind of to simplify airframe structure, reduce aircraft weight itself, the Power Component of powerful.
The content of the invention
Based on the deficiencies in the prior art, present invention is primarily targeted at offer is a kind of and disclosure satisfy that flying for long time, turn to sensitive, powerful, the aircraft of simple structure.
In order to achieve the above object, the invention provides a kind of flight instruments with two power set, including main power plant, secondary power set and connecting rod, main power plant and secondary power set are connected by connecting rod, main power plant includes main rotary shaft, gear reduction and locating piece, gear reduction includes driving wheel and break-in wheel of the concentric locking collar on main rotary shaft, and driving wheel middle part offers deep-slotted chip breaker, and break-in wheel is built in the groove;The secondary power set include secondary rotary shaft and set secondary break-in wheel thereon and secondary locating piece;The both ends of the connecting rod are respectively provided with follower;The follower of the connection boom end is meshed respectively with the tail pair break-in wheel of the break-in wheel of main power plant and secondary power set.
Tailing axle fixture is further cased with secondary rotary shaft, is positioned on secondary break-in wheel by tailing axle fixture.Tail pipe is also cased with outside connecting rod.Main rotary shaft set is also cased with outside main rotary shaft, the unilateral bearing is closely set in main rotary shaft and puts.
Compared with prior art, the overall structure that enormously simplify aircraft of structure is closed in this gear reduction of the invention, the weight of fuselage is also mitigated, causes aircraft power more powerful while the present invention provides two power set, extend the flight time.
To make the present invention easier to understand, a kind of specific embodiment of the flight instruments with two power set of the present invention is expanded on further below in conjunction with accompanying drawing.
Description of the drawings
Fig. 1 is the structural representation of the flight instruments that the present invention has two power set.
Specific embodiment
Below in conjunction with the accompanying drawings, the present invention will be further described.
With reference to shown in Fig. 1, Power Component of the present invention 100 is installed on the middle part of model plane, and its one end connection steering unit, other end connection tail steering set drives steering unit and tail steering set synchronous axial system by the transmission of Power Component.
Should have the flight instruments of two power set includes main power plant 1, secondary power set 2 and connecting rod 3, and by connecting rod 3 main power plant 1 and secondary power set 2 are connected.Wherein, main power plant 1 includes main rotary shaft 10, gear reduction 11 and locating piece 12, main rotary shaft 10 is outer to be also cased with main rotary shaft set 101, gear reduction 11 includes driving wheel 110 and break-in wheel 112, several holes is symmetrically provided with the panel of driving wheel 110, to mitigate its weight, its middle part offers deep-slotted chip breaker 110a, break-in wheel 112 is built in the groove 110a of driving wheel 110, and the flank of tooth 112 ' of break-in wheel 112 is distributed upwards, and the flank of tooth 112 ' is substantially vertical with main rotary shaft 10.Locating piece 12 is included with one heart through the gear wheel axle sleeve 120 and unilateral bearing 122 of main rotary shaft 10, unilateral bearing 122 is embedded in gear wheel axle sleeve 120 and banding is at the middle part of main rotary shaft 10, by unilateral bearing 122 and gear wheel axle sleeve 120 by break-in wheel 112 and the locating piece of driving wheel 110 at the middle part of main rotary shaft 10.
Secondary power set 2 include secondary rotary shaft 20 and set tail pair break-in wheel 22, secondary locating piece 24, tailing axle fixture 26 thereon, are positioned on tail pair break-in wheel 22 by tailing axle fixture 26.
The both ends of connecting rod 3 are respectively provided with two followers 30.In one embodiment of the invention, connecting rod 3 is outer is also further cased with tail pipe 32.The follower 30 of the end of connecting rod 3 is meshed respectively with the tail pair break-in wheel 22 of break-in wheel 112 and secondary power set 2, so, connecting rod 3 itself can follow break-in wheel 112 to rotate together, and, the rotation of secondary power set 2 is driven by the transmission between gear, so as to drive the synchronous rotary of whole steering mechanism and tail steering set.
The embodiment is the present invention preferably embodiment; but do not represent and be only limited by the examples; other any Spirit Essences and any changes done in the case of principle without departing from the present invention, modification, replacement, combine, simplification; the substitute mode equivalent with the present invention is regarded as, is all contained within protection scope of the present invention.

Claims (3)

1. a kind of flight instruments with two power set, it is characterised in that:Including main power plant, secondary power set and connecting rod, main power plant and secondary power set are connected by connecting rod, main power plant includes main rotary shaft, gear reduction and locating piece, gear reduction includes driving wheel and break-in wheel of the concentric locking collar on main rotary shaft, driving wheel middle part offers deep-slotted chip breaker, and break-in wheel is built in the groove;The secondary power set include secondary rotary shaft and set tail pair break-in wheel thereon and secondary locating piece;The both ends of the connecting rod are respectively provided with follower;The follower of the connection boom end is meshed respectively with the secondary break-in wheel of the break-in wheel of main power plant and secondary power set.
2. there is as claimed in claim 1 the flight instruments of two power set, it is characterised in that:The flank of tooth of the break-in wheel is vertical with main rotary shaft.
3. there is as claimed in claim 2 the flight instruments of two power set, it is characterised in that:Tailing axle fixture is further cased with the secondary rotary shaft, is positioned on secondary break-in wheel by tailing axle fixture.
CN201510740899.5A 2015-10-31 2015-10-31 Flight device with two power devices Withdrawn CN106621363A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510740899.5A CN106621363A (en) 2015-10-31 2015-10-31 Flight device with two power devices

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510740899.5A CN106621363A (en) 2015-10-31 2015-10-31 Flight device with two power devices

Publications (1)

Publication Number Publication Date
CN106621363A true CN106621363A (en) 2017-05-10

Family

ID=58851178

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510740899.5A Withdrawn CN106621363A (en) 2015-10-31 2015-10-31 Flight device with two power devices

Country Status (1)

Country Link
CN (1) CN106621363A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106669176A (en) * 2015-11-05 2017-05-17 郑华耀 Multi-propeller comprehensive flight system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080265088A1 (en) * 2005-02-04 2008-10-30 Silverlit Toys Manufactory, Ltd. Propulsion System for Model Airplane
CN201249035Y (en) * 2008-07-31 2009-06-03 何健仁 Stimulation solar rocking toy with a plurality of doll heads in simultaneous motion
CN105597335A (en) * 2014-11-24 2016-05-25 马铿贵 Flight device with two power devices

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080265088A1 (en) * 2005-02-04 2008-10-30 Silverlit Toys Manufactory, Ltd. Propulsion System for Model Airplane
CN201249035Y (en) * 2008-07-31 2009-06-03 何健仁 Stimulation solar rocking toy with a plurality of doll heads in simultaneous motion
CN105597335A (en) * 2014-11-24 2016-05-25 马铿贵 Flight device with two power devices

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106669176A (en) * 2015-11-05 2017-05-17 郑华耀 Multi-propeller comprehensive flight system

Similar Documents

Publication Publication Date Title
CN204050974U (en) There is the remote control distributor toy of multiple power set
WO2013012456A3 (en) Long endurance vertical takeoff and landing aircraft
CN203767064U (en) Wing-folded type unmanned aerial vehicle
CN204337751U (en) Powerful aircraft
CN106621363A (en) Flight device with two power devices
CN105597335A (en) Flight device with two power devices
CN201419025Y (en) Model helicopter
CN204233766U (en) There is the flying toy of multiple power set
CN106669176A (en) Multi-propeller comprehensive flight system
CN106178529A (en) Multiple propeller integrated flying systems
EP3061988A3 (en) Shock absorber assembly for power drive unit of a vehicle
CN203652108U (en) Transmission mechanism for extension and retraction of ceiling propeller of vertical takeoff and landing low-altitude civil rotorcraft
CN106466528A (en) Rotor blade, rotor, aircraft and method
CN105688420A (en) Flight vehicle with two power devices
CN107224725A (en) Remote control distributor toy with multiple power set
CN204473141U (en) Bionic mechanical bird
CN107054640B (en) A kind of lift unit with the disk wing and the aircraft using the device
CN100441258C (en) Power assembly of model airplane
CN105561605A (en) Flight toy with plurality of power devices
CN105197239A (en) Flapping aircraft scheme
CN106669167A (en) Aero-model power assembly
CN106031830A (en) Aircraft capable of effectively improving endurance
CN109107183A (en) Remote control distributor toy with multiple power devices
CN203921186U (en) Band rotating shaft function wing
CN109381868A (en) The aircraft of cruising ability can be effectively improved

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WW01 Invention patent application withdrawn after publication
WW01 Invention patent application withdrawn after publication

Application publication date: 20170510