CN203634824U

CN203634824U - Aircraft having kite function and being capable of being thrown or launching

Info

Publication number: CN203634824U
Application number: CN201320871073.9U
Authority: CN
Inventors: 蔡瑞标
Original assignee: Individual
Current assignee: Individual
Priority date: 2013-12-27
Filing date: 2013-12-27
Publication date: 2014-06-11
Anticipated expiration: 2023-12-27

Abstract

The utility model provides an aircraft having the kite function and being capable of being thrown or launching. The aircraft comprises an aircraft body, wherein the aircraft body is formed by cutting a foldable plastic membrane or a foaming piece or a paper board; the aircraft body comprises a longitudinal guide groove in the middle and horizontal wings on the two sides of the guide groove; a concave support is fixed to the front side of the guide groove; the tail of the guide groove protrudes out of the rear end of the wings on the two sides; the front ends of the wings on the two sides are provided with a transverse rigid pressing piece; the top of the front end of the concave support extends upwards and outwards to form a boss which can be fixed to the transverse pressing piece; the bottom of the front end of the concave support extends downwards to form a connection buckle which is used for connection of a rope. The aircraft is simple in structure and convenient and safe to operate, multiple playing methods of the aircraft are achieved, and the aircraft is a multifunctional toy suitable for children for playing.

Description

A kind of have kite function and can be used for the aircraft of throwing or launching

Technical field

the utility model relates to a kind of toy, relates in particular to a kind of flying toy, more specifically relates to a kind of aircraft that has kite function and can be used for throwing or launch.

Background technology

Kite is the toy that a kind of children like, it is papering or thin,tough silk on the skeleton of thin bamboo strips used for weaving etc., and hauling is superincumbent long line, utilizes the pulling force of long line, makes itself and air generation relative motion, thus acquisition lift upwards.Traditional kite is to carry out the control of height and the control of stability by cotton thread, and is subject to the impact of wind-force and wind direction larger, only, in the situation that wind-force is larger, just can play, and does not substantially possess the function that other are played; Throwing type aircraft, the most traditional, the most simply should belong to by the folding paper helicopter forming of the scraps of paper, this paper helicopter can only fly arbitrarily after throwing, at all uncontrollable; Ejection type aircraft, is to hook in toy fuselage with rubber band, launched to aerial toy by elastic force, and traditional ejection type aircraft, due to simple in structure, having a smooth flight property is poor, is detained the aerial time short; Electronic and the remotely-piloted vehicle of research and development in recent years, complex structure, and need the battery-operated rear flight control that just can carry out specific direction, and can not be used for throwing or launching, do not possess the function of kite yet.

Summary of the invention

For overcoming the problem of above existence, the purpose of this utility model is to provide a kind of multifunction aircraft that possesses kite function and can be used for throwing and launch, and this aircraft is easy to use, safe, and has multiple different playing method.

For realizing above object, the utlity model has kite function and can be used for the aircraft of throwing or launching, comprise Flight main body, it is characterized in that: described Flight main body is to adopt folding plastic film, foamed sheet or Paperboard cutting form, Flight main body comprises the longitudinal guiding gutter in the middle of being arranged at and is positioned at the wing that guiding gutter both sides are level, the front side of guiding gutter is fixed with a female bracket, afterbody protrudes from the rearward end of both sides wing, the leading section of both sides wing is provided with a lateral stiffness compressing tablet, the front top of female bracket is upwards outward extended with the boss that can be fixed on horizontal compressing tablet, bottom is extended with connecing of can linking for rope downwards and buckles.

For the ease of making, above-mentioned guiding gutter is by the Flight main body triangle guiding gutter that longitudinally center line is folded to form downwards, the cross section of female bracket is also corresponding triangular in shape, guiding gutter is fixed in female bracket by backstay, and the bottom of guiding gutter offers the installing hole that can pass for backstay latch.

Promotion and the easy operating that while playing in order to make to throw, can realize updraft, the rearward end of above-mentioned Flight main body guiding gutter both sides wing is respectively drawn in and is formed two empennages to centre, and empennage place is preset with the lateral fold that can manually upwards turn down.

For the ease of installing, the connection boss of leading section, compressing tablet and the female bracket of above-mentioned Flight main body is equipped with installing hole, and they are mutually permanently connected by negative and positive hasp.

For guiding gutter is better fixed in female bracket, the side of above-mentioned guiding gutter and the side of female bracket are equipped with installing hole, and both are interconnected and fixed by negative and positive hasp.

For different playing methods is provided, and be convenient to adjust in time according to the weight of compressing tablet the balance of aircraft, above-mentioned female bracket bottom comprises the position, closed hole that can supply rope or the collar to link and the hook that can be affiliated to for elastic threads to the button that connects of downward-extension, closed Kong Weiwei several and communicate with the bottom of support, hook is positioned at position, closed hole front end.

For the better resistance that reduces aircraft, the angle that the front end face of above-mentioned guiding gutter and rear end face and wing place plane form is acute angle.

In order to reduce the resistance of Flight main body side, the side of above-mentioned wing is arc line type.

For the front end face of better protection Flight main body, the outer edge that above-mentioned compressing tablet and wing are affixed one side is provided with spacing raised line, and the inside edge of female bracket front end face is also provided with spacing raised line.

Above-mentioned backstay is by cross section the leg-of-mutton depression bar that stands upside down and forms to the latch corresponding with female bracket bottom through-hole of downward-extension with depression bar bottom.

Aircraft of the present utility model, Flight main body is provided with guiding gutter, this guiding gutter extends to afterbody from the front end of Flight main body, in the time of flight, can become the passage of aircraft airflow, balance to aircraft glide path plays conclusive effect, front side at guiding gutter is fixed with female bracket, can avoid the variation of guiding gutter shape, the flow through steady air current of guiding gutter of assurance, and the setting of wing front end compressing tablet, not only can protect the front end face of Flight main body, and can play the effect of adjusting center of gravity and the degree of balance, make whole aircraft in flight course, keep best balance state of flight.Aircraft of the present utility model, is being equipped with transmitter in the situation that, and while making both sides wing rearward end be level, can realize the function of general ejector straight line, curved flight or convolution flight; Be equipped with connecting line in the situation that, and when both sides wing rearward end is upwards turned down along default folding line, turning down angle by adjustment, adopting parallel throwing, realize different headings and gliding flight route to the mode of high-altitude throwing or reverse throwing; , also can increase after the film strip of balance in the afterbody laminating of aircraft enough large or large scale wing in the situation that at wind-force, make it possess the characteristic of kite by the length of control connection line.Aircraft of the present utility model, simple in structure, easy to operate, safety, and playing method is various, is the Multifunctional toy that a applicable children play.

Accompanying drawing explanation

Fig. 1 is the structural representation of the utility model aircraft.

Fig. 2 is the structural representation at the utility model aircraft back side.

Fig. 3 is the structural representation of Flight main body.

Fig. 4 is the structural representation of female bracket.

Fig. 5 is the structural representation of compressing tablet.

Fig. 6 is the structural representation of backstay.

Fig. 7 is the scheme of installation that Flight main body guiding gutter is fixedly connected with female bracket.

Fig. 8 is the scheme of installation that Flight main body leading section is fixedly connected with compressing tablet.

Fig. 9 is the location drawing of the link of throwing type playing method colored ribbon.

Figure 10 launches the location drawing that playing method rubber band is affiliated to.

The specific embodiment

As shown in Figure 1, 2, of the present utility model have kite function and can be used for the aircraft of throwing or launching, and comprises Flight main body 1, female bracket 2, compressing tablet 3 and backstay 4, and Flight main body is fixedly connected with by negative and positive hasp 5 with female bracket, compressing tablet;

As shown in Figure 3, Flight main body 1 is to adopt folding thin plastic film sheet, foamed sheet (for example PP, EVA or PS), the light materials such as cardboard cut and form, the utility model adopts PP diaphragm, it comprises the wing 12 that is level downwards by the Flight main body triangle guiding gutter 11 that longitudinally center line is folded to form and both sides, the angle that the front end face of triangle guiding gutter and rear end face and wing place plane form is acute angle, the bottom, front side of guiding gutter offers the installing hole 13 that can pass for backstay latch, side opening is provided with the locating hole 14 that can be fixed on female bracket, the afterbody of guiding gutter protrudes from the rearward end of both sides wing, the leading section of both sides wing offers the installing hole 15 that can be fixed on compressing tablet, the rearward end of both sides wing is respectively drawn in to centre and is formed two empennages 16, empennage place is preset with the lateral fold 17 that can manually upwards turn down, the side of wing is arc line type,

As shown in Figure 4, female bracket 2 is the triangular supports corresponding with guiding gutter shape, the front top of support is upwards outward extended with the boss 21 that can be fixed on horizontal compressing tablet, bottom is extended with three downwards can be for the position, closed hole 22 of rope or collar link and the hook 23 that can be affiliated to for elastic threads, the bottom of closed Kong Weiyu support communicates, hook is positioned at position, closed hole front end, support front end face and guiding gutter front end face maintain an equal level, and the inside edge of support front end face is provided with spacing raised line 24, with the front end face of protection guiding gutter, the side of support is also provided with and can supplies the fixing locating hole 25 of guiding gutter,

As shown in Figure 5, compressing tablet 3 adopts the plastic tab with certain rigidity to make, its surface offers the installing hole 31 corresponding with both sides wing leading section position of mounting hole and quantity, and the outer edge that compressing tablet and wing are affixed one side is provided with spacing raised line 32, to protect the front end face of wing;

As shown in Figure 6, backstay 4 is to be by cross section the leg-of-mutton depression bar 41 that stands upside down to form to the inserted block 42 corresponding with guiding gutter bottom installing hole of downward-extension with depression bar bottom;

When aircraft of the present utility model is installed, as shown in Figure 7,8, first adopt backstay 4 that the guiding gutter of Flight main body 1 is fixed in triangular supports 2, allow again the installing hole of the installing hole of Flight main body and compressing tablet 3, triangular supports boss align, utilize negative and positive hasp that compressing tablet, triangular supports are fixed on the leading section of Flight main body.

When aircraft of the present utility model is played, as shown in Figure 9, can adopt the metal clip 6 on colored ribbon accessory to be anchored to middle position, hole, reach optimum state by diagram target balance angle, then adjust the empennage of left and right wing rearward end, they are slightly upwards amounted to, up swing the rear relieving of colored ribbon 7 with hand, aircraft is slowly hovered after rising to peak, the angular dimension that empennage is upwards amounted to will determine head amplitude up when aircraft flight, and the angle of upwards amounting to is large, and aircraft upwards flies, angle is little, and the angle that aircraft upwards flies is just little or be tending towards level; As shown in figure 10, readjust the empennage of left and right wing rearward end, make they and wing keep coexisting a horizontal plane, can guarantee to fly like this time without wind resistance, and after being launched, aircraft can keep the route of rectilinear flight, adopt the transmitter 8 with rubber band, rubber band on transmitter 9 is anchored on the hook under fuselage, the center of aircraft afterbody press...withes one's finger, it is retracted to rear release and launch away, the angle before the strength of pullling and transmitting between aircraft wing and horizontal plane will determine distance and the path of aircraft.

More than just embodiment of the utility model aircraft illustrates; this embodiment is not in order to limit protection domain of the present utility model; all equivalences that does not depart from technical solutions of the utility model are implemented or change; as the change of Flight main body, guiding gutter, female bracket shape, also should be included in protection domain of the present utility model.The playing method of the utility model aircraft is also varied, more than just arbitrarily enumerates, and after playing skillfully, different skills links up while carrying out, will have various informative playing method constantly to occur.

Claims

1. one kind has kite function and can be used for the aircraft of throwing or launching, comprise Flight main body, it is characterized in that: described Flight main body is to adopt folding plastic film, foamed sheet or Paperboard cutting form, Flight main body comprises the longitudinal guiding gutter in the middle of being arranged at and is positioned at the wing that guiding gutter both sides are level, the front side of guiding gutter is fixed with a female bracket, afterbody protrudes from the rearward end of both sides wing, the leading section of both sides wing is provided with a lateral stiffness compressing tablet, the front top of female bracket is upwards outward extended with the boss that can be fixed on horizontal compressing tablet, bottom is extended with connecing of can linking for rope downwards and buckles.

2. the aircraft that has kite function and can be used for throwing or launching according to claim 1 is characterized in that: described guiding gutter is by the Flight main body triangle guiding gutter that longitudinally center line is folded to form downwards, the cross section of female bracket is also corresponding triangular in shape, guiding gutter is fixed in female bracket by backstay, and the bottom of guiding gutter offers the installing hole that can pass for backstay latch.

3. the aircraft that has kite function and can be used for throwing or launching according to claim 1 and 2 is characterized in that: the rearward end of described Flight main body guiding gutter both sides wing is respectively drawn in and formed two empennages to centre, and empennage place is preset with the lateral fold that can manually upwards turn down.

4. the aircraft that has kite function and can be used for throwing or launching according to claim 3 is characterized in that: the connection boss of leading section, compressing tablet and the female bracket of described Flight main body is equipped with installing hole, and they are mutually permanently connected by negative and positive hasp.

5. the aircraft that has kite function and can be used for throwing or launching according to claim 4 is characterized in that: the side of described guiding gutter and the side of female bracket are equipped with installing hole, and both are interconnected and fixed by negative and positive hasp.

6. the aircraft that has kite function and can be used for throwing or launching according to claim 5 is characterized in that: described female bracket bottom is buckled and comprised the position, closed hole that can supply rope or the collar to link and the hook that can be affiliated to for elastic threads to connecing of downward-extension, closed Kong Weiwei several and communicate with the bottom of support, hook is positioned at position, closed hole front end.

7. the aircraft that has kite function and can be used for throwing or launching according to claim 6 is characterized in that: the angle that the front end face of described guiding gutter and rear end face and wing place plane form is acute angle.

8. the aircraft that has kite function and can be used for throwing or launching according to claim 7 is characterized in that: the side of described wing is arc line type.

9. the aircraft that has kite function and can be used for throwing or launching according to claim 8 is characterized in that: the outer edge that described compressing tablet and wing are affixed one side is provided with spacing raised line, and the inside edge of female bracket front end face is also provided with spacing raised line.

10. the aircraft that has kite function and can be used for throwing or launching according to claim 9 is characterized in that: described backstay is by cross section the leg-of-mutton depression bar that stands upside down and forms to the latch corresponding with female bracket bottom through-hole of downward-extension with depression bar bottom.