CN204548497U

CN204548497U - A kind of many rotor flight devices

Info

Publication number: CN204548497U
Application number: CN201520240104.XU
Authority: CN
Inventors: 周道卿; 高硕颀
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-04-20
Filing date: 2015-04-20
Publication date: 2015-08-12
Anticipated expiration: 2025-04-20

Abstract

The utility model discloses a kind of many rotor flight devices, belong to cyclogyro, its body inside, cabin has a cabin, and cabin body establishes alighting gear and six groups of power spin oars, comprises a front propeller and an after screw and is located at the front and back of cabin body respectively and the first axle that all defines with cabin body of rotating shaft is coaxial; One left handed propeller and a right-hand screw oar are located at the left and right of cabin body and the second axis coaxle of all defining with cabin body of rotating shaft respectively; And on one screw propeller and once screw propeller be located at respectively cabin body up and down and the 3rd axis coaxle that all defines with cabin body of rotating shaft, each screw propeller comprises rotating shaft, blade and annulus; Phase the utility model is not owing to needing the manipulation of wing flap, aileron and empennage, simple with power spin oar for flying power, the necessary component of flight can be simplified, and take off and be not limited to runway and can perform in original place with landing, can easily change of flight attitude in the process of aloft flying, and can change of flight direction easily when flying, make handling to there is good degree of stability.

Description

A kind of many rotor flight devices

Technical field

The utility model belongs to autogiro.

Background technology

Existing flight instruments, is still with air transport based on fixed-wing aircraft.Though fixed-wing aircraft be with turbine spray or with screw propeller for power, the runway of certain length is needed when taking off, fixed-wing aircraft is allowed to slide on runway to certain speed, lift is provided to take off by the wing flap start on fixed-wing aircraft, and coordinating through aileron and empennage in flight course, reach the action of nosepiston, fuselage beat and upset.Relative wind when flying before also having now a kind of utilization blows autorotation to produce the rotary wing aircraft of lift, and its ahead power is directly provided by driven by engine screw propeller.

But, the flight instruments of existing fixed-wing aircraft, though through nosepiston, fuselage beat and upset action and can aloft fly, stand the impact of attitude change and limit to some extent in manipulation, cannot change of flight direction easily, and flight instruments arranges wing flap, aileron and empennage etc. cannot simplify for necessary component.

Utility model content

Large in order to overcome existing aircraft landing limitation, the deficiency that stability is not good, the utility model provides a kind of many rotor flight devices, and this kind of many rotor flight device not only landing is quick, and manipulation has good degree of stability.

The utility model solves the technical scheme that its technical matters adopts: a kind of many rotor flight devices, comprise cabin body, alighting gear, screw propeller, control unit, it is characterized in that: there is a cabin can taken for people body inside in described cabin having that a level runs through first axle before and after the body of described cabin, a level the second axis and run through about the body of described cabin vertically runs through the 3rd upper and lower axis of described cabin body, described first axle, the second axis are crossing in the center of gravity of described cabin body with the 3rd axis; Described alighting gear, is located at bottom the body of described cabin and parks in ground for described cabin body; Six groups of power spin oars, to comprise on a front propeller, after screw one left handed propeller, a right-hand screw oar, a screw propeller and once screw propeller, each described screw propeller comprises a rotating shaft, multiplely take rotating shaft as the blade that arranges in the form of a ring of axle center and a circular cross-section and be looped around the annulus of described blade tip; Described front propeller and after screw are located at the front and back of described cabin body respectively and rotating shaft is all coaxial with described first axle; Described left handed propeller and right-hand screw oar be located at the left and right of described cabin body respectively and rotating shaft all with described second axis coaxle; Described upper screw propeller and lower screw propeller be located at respectively described cabin body up and down and rotating shaft all with described 3rd axis coaxle; One control unit, is located at described cabin body and is electrically connected described six groups of power spin oars.

The many rotor flight devices of above-mentioned one, comprise a positioning navigation device further, and described positioning navigation device and described control unit are electrically connected.

The beneficial effects of the utility model are that the cabin body of many rotor flight devices flies with set six groups of power spin oars, cabin body taking off and landing before and after flight, and the flight attitude in flight course, can through the control of control unit, and make to comprise front propeller, after screw, left handed propeller, right-hand screw oar, upper screw propeller and the collocation of lower screw propeller manipulate and complete, for the structure of existing cyclogyro, owing to not needing wing flap, the manipulation of aileron and empennage, simple with power spin oar for flying power, the necessary component of flight can be simplified, and take off and be not limited to runway and can perform in original place with landing, can easily change of flight attitude in the process of aloft flying, and can change of flight direction easily when flying, make handling to there is good degree of stability.

Accompanying drawing explanation

Accompanying drawing 1 is three-dimensional appearance schematic diagram of the present utility model,

Fig. 2 is the organigram of side-looking plane of the present utility model and body inside, cabin,

In figure, 1. cabin body, 11. cabins, 2. alighting gear, 3. power spin oar, 31. front propellers, 311. rotating shafts, 312. blades, 313. annulus, 32. after screws, 321. rotating shafts, 322. blades, 323. annulus, 33. left handed propellers, 331. rotating shafts, 332. blades, 333. annulus, 34. right-hand screw oars, 341. rotating shafts, 342. blades, 343. annulus, screw propeller on 35., 351. rotating shafts, 352. blades, 353. annulus, 36. times screw propellers, 361. rotating shafts, 362. blades, 363. annulus, 4. control unit, 41. positioning navigation devices.

Detailed description of the invention

Detailed description of the invention of the present utility model is, as shown in the figure:

Embodiment 1, a kind of many rotor flight devices, as shown in Figure 1, comprise cabin body 1, alighting gear 2, six groups of power spin oars 3 and a control unit 4, wherein:

As shown in Fig. 1 to 2, the inside of described cabin body 1 has a cabin 11 can taken for people, described cabin body 1 has a first axle R, one second axis P and the 3rd axis Y, wherein said first axle R level runs through before and after described cabin body 1, described second axis P level runs through described cabin body about 1, described 3rd axis Y vertically runs through described cabin body about 1, and described first axle R, the second axis P are crossing in the center of gravity of described cabin body 1 with the 3rd axis Y.

As shown in Fig. 1 to 2, there are in the present embodiment two alighting gears 2, in the present embodiment, be symmetrically set in the two bottom sides of described cabin body 1, by alighting gear 2, parking in ground when taking off or land for described cabin body 1.

As shown in Fig. 1 to 2, six groups of power spin oars 3 comprise a front propeller 31, one after screw 32, one left handed propeller 33, one right-hand screw oar 34, screw propeller 35 and once screw propeller 36 on one, each described screw propeller 31, 32, 33, 34, 35, 36 comprise a rotating shaft 311, 321, 331, 341, 351, 361, multiple with affiliated rotating shaft 311, 321, 331, 341, 351, 361 blades 312 arranged in the form of a ring for axle center, 322, 332, 342, 352, 362, and a circular cross-section and be looped around described blade 312, 322, 332, 342, 352, the annulus 313 of the end of 362, 323, 333, 343, 353, 363.

Front propeller 31 and after screw 32 are located at the front and back of described cabin body 1 respectively and rotating shaft 311,321 is all coaxial with described first axle R; Left handed propeller 33 and right-hand screw oar 34 are located at the left and right of described cabin body 1 respectively and rotating shaft 331,341 is coaxial with described second axis P; Upper screw propeller 35 and lower screw propeller 36 are located at the upper and lower of described cabin body 1 respectively and rotating shaft 351,361 is coaxial with described 3rd axis Y.

As shown in Figure 2, control unit 4 is located at described cabin body 1, and is electrically connected described six groups of power spin oars 3, and controls described six groups of power spin oars 3 and fly to make described cabin body 1.In the present embodiment, comprise a positioning navigation device 41 further, this positioning navigation device 41 is electrically connected with described control unit 4, can auto-flare system device flight extremely location.

Claims

1. rotor flight device more than a kind, comprise cabin body, alighting gear, screw propeller, control unit, it is characterized in that: there is a cabin can taken for people body inside in described cabin having that a level runs through first axle before and after the body of described cabin, a level the second axis and run through about the body of described cabin vertically runs through the 3rd upper and lower axis of described cabin body, described first axle, the second axis are crossing at the center of gravity place of described cabin body with the 3rd axis; Described alighting gear, is located at bottom the body of described cabin and parks in ground for described cabin body; Six groups of power spin oars, to comprise on a front propeller, an after screw, a left handed propeller, a right-hand screw oar, a screw propeller and once screw propeller, each described screw propeller comprises a rotating shaft, multiplely take rotating shaft as the blade that arranges in the form of a ring of axle center and a circular cross-section and be looped around the annulus of described blade tip; Described front propeller and after screw are located at the front and back of described cabin body respectively and rotating shaft is all coaxial with described first axle; Described left handed propeller and right-hand screw oar be located at the left and right of described cabin body respectively and rotating shaft all with described second axis coaxle; Described upper screw propeller and lower screw propeller be located at respectively described cabin body up and down and rotating shaft all with described 3rd axis coaxle.