CN201338727Y

CN201338727Y - Power aircraft with delta wing

Info

Publication number: CN201338727Y
Application number: CNU2008201573994U
Authority: CN
Inventors: 孙为红
Original assignee: Individual
Current assignee: Individual
Priority date: 2008-12-18
Filing date: 2008-12-18
Publication date: 2009-11-04
Anticipated expiration: 2018-12-18

Abstract

The utility model relates to a power aircraft with a delta wing, which comprises a cabin, a power driving device, a delta wing and a delta operation frame. The bottom of the cabin is provided with landing wheels, both sides are provided with hatches, and the inside is provided with seats; the power driving device is arranged on the rear side of the cabin; the delta wing is arranged above the cabin, and comprises a middle shaft and double wings which are unfolded symmetrically along the middle shaft; the middle shaft of the delta wing is connected with the cabin by a connecting support; the delta operation frame comprises two vertical posts and a horizontal post; the two vertical posts are crossed and fixedly connected with the middle shaft of the delta wing; the horizontal post goes through the cabin from the hatches on both sides of the cabin; and both ends of the horizontal post are connected with the front edge and the rear edge of the delta wing by control cables. The power aircraft of the delta wing can contain a plurality of people; and the design of the cabin prevents the passengers from being directly exposed outside, thereby improving the safety. When the aircraft needs to take off, a propeller on the rear end drives the aircraft to advance and adjusts the windward angle of the delta wing by the delta operation frame, so as to provide upward floating force for the aircraft, so that the aircraft takes off; and when the aircraft flies, the delta operation frame controls the flying direction and the rising and landing of the aircraft.

Description

The active flight device of tool delta wing

Technical field

The utility model relates to a kind of active flight device of tool delta wing, refer to especially a kind of have delta wing and can fly fast and on land, the water surface aircraft that all can land and take off.

Background technology

Aircraft has become the important vehicle, and existing aircraft generally comprises helicopter, and fixed wing aircraft etc. need the technical professional but handle this type of aircraft, and the expense costliness.

In order to satisfy people's requirement of familiarization flight in person, now developed some simple and easy aircraft of being convenient to operate, as: power angle blade, active flight umbrella and the unpowered umbrella etc. that slides.Such simple and easy aircraft mainly comprises a umbrella portion and the easy operating control of a cover, can allow the user hover aloft easily.

Only analyze as can be known,, just can't enjoy the enjoyment of circling in the air for the user of operation skill, also can't realize the transportation effect of this type of simple and easy aircraft for not having because its structure Design can only be carried a people by existing this type of simple and easy aircraft;

Other does not have this type of simple and easy aircraft of power to be subjected to the restriction of place and natural conditions bigger, takes off and land all to need specified conditions and match, and practical value is not high;

Moreover this type of simple and easy aircraft is outside awing the people is exposed to, and the both feet by the people during landing land, and is dangerous big, the safety deficiency;

Be exactly that this type of simple and easy aircraft can't land on the water surface or take off in addition, according to experience in the past, when it drop on the water surface, the people will fall into the water, and umbrella portion also can drop on the water surface, so promptly can not go again and take off.

Obviously existing this type of simple and easy aircraft still has its improved space.

Summary of the invention

Therefore the technical problems to be solved in the utility model is for providing a kind of active flight device of tool delta wing, and it can hold several people takes simultaneously, safe, and can travel by land, low to the site requirements that takes off and land, control comfort.

For solving the problems of the technologies described above, the utility model provides a kind of active flight device of tool delta wing, it is characterized in that comprising:

One cabin, its bottom is provided with a plurality of landing wheels, and the both sides, cabin are equipped with hatch, are provided with a seat in the cabin at least;

One Power Drive Unit is arranged at this cabin rear side;

One delta wing is located at top, described cabin, this delta wing comprise an axis and along in the double-vane that launches of rotational symmetry, be connected the support connection by one between described delta wing axis and the cabin;

One triangle control frame, described triangle control frame comprises two vertical rods, a cross bar and most root control wire, this two vertical rod is crossing to be fixedly connected on the axis of described delta wing, the cross bar of described triangle control frame passes described cabin from the hatch of both sides, described cabin, and the two ends of described cross bar are connected with the front and rear edges of described delta wing by control wire;

Described Power Drive Unit comprises the screw propeller of being located on the described cabin, is used to drive the driving engine of this screw propeller, and is located at the power management switch in the cabin.

The active flight device of above-mentioned tool delta wing can hold several people to be taken simultaneously, can avoid having strengthened safety outside the passenger directly is exposed to by the design in cabin.When needs take off, screw propeller driving aircraft by the rear end, cabin advances with certain speed, adjust the angle of facining the wind of delta wing simultaneously by the triangle control frame, for whole aircraft provides a buoyancy that makes progress, thereby make aircraft takeoff, in when flight, the operator can come the direction of controlling aircraft and rises and falls by the triangle control frame.

Further improvement of the utility model is, the active flight device of described tool delta wing is provided with a directional controller, this directional controller comprises the yaw rudder of being located at the aircraft rear end, is located at the rudder control device in the cabin and connects this yaw rudder and the direction of rudder control device operation rope.By the design of this directional controller, can this aircraft be turned on land freely by the orientation angle of change of direction rudder.

Further improvement of the present invention is that below, described cabin is provided with a keg float, and the bottom surface of this keg float is higher than the minimum touchdown point of described landing wheel.

By the design of described keg float, it is waterborne that this aircraft further is applied to.In water, this keg float provides buoyancy to aircraft, and sliding in the water is identical with the land, and the air-flow that produces by screw propeller promotes.

Description of drawings

Fig. 1 is the construction profile scheme drawing of active flight device first preferred embodiment of the utility model tool delta wing;

Fig. 2 is the Facad structure scheme drawing of active flight device first preferred embodiment of the utility model tool delta wing;

Fig. 3 is the second preferred embodiment construction profile scheme drawing of the active flight device of the utility model tool delta wing.

The specific embodiment

Consult Figure 1 and Figure 2, the active flight device of the utility model tool delta wing forms the cabin 1 of a stream line pattern, and this cabin 1 comprises a housing 10, is formed with passenger cabin 20 in housing 10.Housing 10 two side faces have a hatch 11 and a rear deck window 12, housing 10 front ends are provided with pibtot's tub 13, housing 10 bottoms are provided with a plurality of landing wheels 14, be provided with a screw propeller 15 simultaneously in the rear end of this housing 10 and be provided with a yaw rudder 16 in these screw propeller 15 rear ends, the rear end of aircraft is provided with a driving engine 17 mutually with screw propeller 15; Be provided with a keg float 30 below cabin 1, the bottom surface of this keg float 30 is higher than the minimum touchdown point of described landing wheel 14, therefore can not influence aircraft operation on land.Delta wing 40 is located at 1 top, described cabin, this delta wing 40 comprises the double-

vane

42,43 that rotational symmetry is launched in an axis 41 and the edge, being connected support 44 by one between described delta wing axis 41 and the cabin 1 connects, connecting support 44 is made up of two preceding bars 441 and a back bar 442, bar 441 is fixed in top, cabin respectively with an end of back bar 442 before two, and the other end of three bars intersects at described delta wing axis 41, keeps hanging connecting; This aircraft also comprises a triangle control frame 50, described triangle control frame 50 comprises two

vertical rods

51,52 and a cross bar 53, most root control wire 54, the intersection point of this two

vertical rod

51,52 is fixedly connected on the axis 41 of described delta wing, the cross bar 53 of described triangle control frame 50 passes described passenger cabin 20 from the hatch 11 of 1 both sides, described cabin, and the two ends of described cross bar 53 are connected with the front and rear edges of described delta wing 40 by control wire 54.

Be provided with an above seat 21 in the passenger cabin 20, when seat 21 is made as two when above, wherein a seat 21 is main driver seat 21, be provided with an one control lever 22 at close main driver seat 21 places and be used to control driving engine 17, also include a left side, right-hand tread plate 23,23 ', wherein left, right-hand tread plate 23,23 ' respectively direction of passage operation ropes 24,24 ' link to each other with rudder control arm 25 on the yaw rudder 16, pedal 23,23 ' be rudder control device of the present utility model, and pedal 23,23 ' simultaneously are connected with the landing wheel 14 of being located at cabin 1 front end, thus the direct of travel that turns to controlling aircraft of steer direction rudder 16 and front end landing wheel 14 thus.When aircraft need left-handed turning to the time, depress left-hand tread plate 23 and drive yaw rudder 16 deflections left, also make front end landing wheel 14 deflection left simultaneously, make thus whole aircraft left-handed turning to; When the aircraft right-hand turning to the time, by the operation of right-hand tread plate 23 ' in the same manner.

As mentioned above, described joystick 22, screw propeller 15, driving engine 17 has constituted the Power Drive Unit of this aircraft.Certainly, this Power Drive Unit also can change the substitute of equivalence into, as injecting type; This screw propeller 15 can adopt ducted fan pattern as shown in FIG. in addition, it can provide comparatively actv. thrust on the one hand, on the other hand also because its screw propeller 15 is to be a coated state, and can significantly improve the safety of its use, can in use not injure personnel or clash into peripheral object.

Described yaw rudder 16, pedal 23,23 ', direction of passage operation rope 24,24 ' linking to each other has constituted the directional controller of this aircraft.Certainly, this directional controller also can change the substitute of equivalence into.

In addition, the nearly landing wheel in 1 bottom 14 places are provided with a stop motion mechanism 18 in the cabin, and its similar is stopped in the butterfly of bicycle, does not do detailed description at this.

When aircraft of the present invention moved on land, the driver can be seated on the main driver seat 21, holds joystick 22, control throttle size; By pedal 23,23 ' come steering rudder 16 and be located at the direction of the landing wheel 14 of front end, thus the direct of travel of controlling aircraft; During stop, can realize by the stop motion mechanism 18 of bottom, cabin.

Design by described keg float 30, this aircraft can directly sail in the water, in water, support the balance of aircraft by keg float 30, sliding in the water handled identical with the land, at this moment, pedal 22 steering rudders 16 and preceding landing wheel 14 are controlled the direction of advancing, and this preceding landing wheel 14 can provide the effect of similar boats and ships yaw rudder.

When needing to take off on land, the screw propeller 15 by 1 rear end, cabin drives aircraft and advances with certain speed, adjusts the angle of facining the wind of delta wings 40 simultaneously by triangle control frame 50, for whole aircraft provides a buoyancy that makes progress, thereby makes aircraft takeoff.When flying, handle the direction that the both sides angles control of delta wing 40 is advanced thereby can adjust triangle control frame 50 equally by control wire 54, thereby the angle of facining the wind that perhaps changes delta wing 40 is regulated flying speed aloft.

As preferred embodiment of the present utility model, below cabin 1, be provided with a keg float 30, aircraft is taken off in water and land.

Again as shown in Figure 3, another embodiment of the present utility model.It has removed described keg float 30 on the basis of the foregoing description, make structure more simple, and has kept above-mentioned aircraft and travel on land, takes off and function such as landing.

Claims

1. the active flight device of a tool delta wing is characterized in that comprising:

One Power Drive Unit is arranged at this cabin rear side;

One triangle control frame, described triangle control frame comprises two vertical rods, a cross bar and complex root control wire, this two vertical rod is crossing to be fixedly connected on the axis of described delta wing, the cross bar of described triangle control frame passes described cabin from the hatch of both sides, described cabin, and the two ends of described cross bar are connected with the front and rear edges of described delta wing by control wire.

2. the active flight device of tool delta wing as claimed in claim 1 is characterized in that: described Power Drive Unit comprises the driving engine of being located at the screw propeller on the described cabin and being used to drive this screw propeller.

3. the active flight device of tool delta wing as claimed in claim 2 is characterized in that: described screw propeller is a ducted fan.

4. as the active flight device of claim 1,2 or 3 described tool delta wings, it is characterized in that: the active flight device of described tool delta wing is provided with a directional controller, this directional controller comprises the yaw rudder of being located at the Power Drive Unit rear end, is located at the rudder control device in the cabin and connects this yaw rudder and the direction of rudder control device operation rope.

5. the active flight device of tool delta wing as claimed in claim 1 is characterized in that: described cabin is provided with pibtot's tub.

6. the active flight device of tool delta wing as claimed in claim 1 is characterized in that: below, described cabin is provided with a keg float, and the bottom surface of this keg float is higher than the minimum touchdown point of described landing wheel.

7. the fast aircraft of tool delta wing as claimed in claim 4 is characterized in that: described cabin is provided with pibtot's tub.

8. the fast aircraft of tool delta wing as claimed in claim 7 is characterized in that: below, described cabin is provided with a keg float, and the bottom surface of this keg float is higher than the minimum touchdown point of described landing wheel.