CN202113608U

CN202113608U - Toy armed aircraft

Info

Publication number: CN202113608U
Application number: CN201120241207XU
Authority: CN
Inventors: 王壮鹏
Original assignee: Individual
Current assignee: Individual
Priority date: 2011-07-09
Filing date: 2011-07-09
Publication date: 2012-01-18
Anticipated expiration: 2021-07-09

Abstract

The utility model relates to a toy armed aircraft, which comprises an aircraft body. The utility model is characterized in that the toy armed aircraft also comprises at least one missile launcher and at least one toy missile; the missile launcher(s) is/are arranged on the aircraft body and is positioned under the aircraft body; the toy missile(s) is/are arranged on the missile launcher(s); each the missile launcher comprises a base, a rotary missile mounting frame and a mounting frame driving mechanism; the mounting frame driving mechanism is fixed on the base; the rotary missile mounting frame can be rotatably fixed on the base; and the mounting frame driving mechanism is connected with the rotary missile mounting frame. The toy armed aircraft has the beneficial effects that as the missile launcher(s) and the toy missile(s) are arranged, the toy armed aircraft can launch the toy missile(s) to hit various targets or can confront with other toy aircrafts, the toy armed aircraft can launch the missile(s) at any time of flying and can launch a single missile or sequentially and continuously launch the missiles, and the launched missiles can be recycled, thereby greatly improving the enjoyment and the playability of the toy armed aircraft.

Description

Toy arms aircraft

Technical field

The utility model relates to a kind of toy airplane, more specifically to a kind of toy arms aircraft that can launch the toy guided missile.

Background technology

Existing toy airplane only possesses the flight function, does not have new meaning, lacks interest and playability.Therefore, these toy airplanes can't with the competition of the similar toy airplane of other function in show one's talent.

Because toy airplane can not go, carry out various antagonism matches on the ground as toy car; If carry out various antagonism matches as toy car on high, because the problem at people visual angle, visual effect is poor; And because each toy airplane is for fear of collision; Usually distance is far away, so these matches are difficult to occur excellent scene, and is interesting and playability is not high.

Summary of the invention

The utility model technical problem to be solved provides a kind of toy arms aircraft, and this toy arms aircraft can be launched the toy guided missile.The technical scheme that adopts is following:

A kind of toy arms aircraft; Comprise aircraft body, it is characterized in that: also comprise at least one missile launcher and at least one toy guided missile, said missile launcher is installed on the aircraft body; And missile launcher is positioned at the aircraft body below, and said toy guided missile is installed on the missile launcher; Said missile launcher comprises base, rotation guided missile installing rack, installing rack driving mechanism, and said installing rack driving mechanism is fixed on the base, rotating being fixed on the base of said rotation guided missile installing rack, and the installing rack driving mechanism connects rotation guided missile installing rack.

A kind of more excellent scheme; Said rotation guided missile installing rack comprises shell body, prelocalization frame, back locating rack and at least one toy guided missile detent mechanism; The leading flank of said base is provided with toy guided missile detent mechanism opening device; The front end of shell body has at least one guided missile inlet, and prelocalization frame, back locating rack are installed in respectively in the shell body, and said toy guided missile detent mechanism is arranged on the prelocalization frame; Said back locating rack comprises front rod, back joint pin and at least one spacer; The front rod rear end connects the front end of back joint pin; Said spacer is fixed on the joint pin outer circumference surface of back; The rear end of prelocalization frame has slot, rotating being fixed on the base of back joint pin of back locating rack, and the back joint pin is connected and installed the frame driving mechanism; The front rod of back locating rack inserts in the slot of prelocalization frame; And form at least one toy guided missile positioning chamber between prelocalization frame, back locating rack and the shell body, said toy guided missile detent mechanism is corresponding one by one with toy guided missile positioning chamber, and toy guided missile detent mechanism is located at the rear portion of toy guided missile positioning chamber.

More excellent scheme, the number of the number of the number of said spacer, toy guided missile detent mechanism, the number of toy guided missile positioning chamber, guided missile inlet, the number of toy guided missile detent mechanism are all identical.

The middle part of said toy guided missile periphery has locating slot; Said toy guided missile detent mechanism comprises small footprint, spring reference column, spring, supporting rod, and the spring reference column is fixed on the small footprint front end, and spring housing is on the spring reference column; The rear end of supporting rod is fixed on the small footprint; The rear portion of supporting rod is a curved surface, and the supporting rod middle part is provided with rotating shaft, and said rotating shaft is rotating to be fixed on the prelocalization frame that rotates the guided missile installing rack; The front end of supporting rod is provided with clamping and colludes, and the locating slot rear wall of toy guided missile is caught in clamping.

Said base is made up of preceding base panel and rear base panel; Form base intracavity between preceding base panel and the rear base panel; The installing rack driving mechanism comprises motor, train of reduction gears, and on the base panel leading flank, said train of reduction gears was installed in the base intracavity before motor was fixed on; And the input gear of train of reduction gears is installed on the output shaft of motor, and the output gear of train of reduction gears is coaxial fixing with the back joint pin of back locating rack.

In order to make missile launcher more true to nature, said missile launcher also is provided with the back decorative box, and said back decorative box is fixed on the trailing flank of base.

The toy guided missile is made up of two parts, i.e. body and bullet.Body is processed by the ABS material, and bullet is processed by environmental protection soft PVC, and is not only safe but also reliable.People can the remote control missile launcher come out the toy MISSILE LAUNCHING, impact all types of target, perhaps resist with other toy airplane.

The utility model beneficial effect against existing technologies is; Owing to be provided with missile launcher and toy guided missile, so toy airplane can launch the toy guided missile and impact all types of target, perhaps resists with other toy airplane; But toy airplane is at any time of flight operation issue toy guided missile all; Both can singlely launch, also can launch continuously successively, significantly improved the interest and the playability of toy airplane.

Description of drawings

Fig. 1 is the structural representation of the utility model preferred embodiment;

Fig. 2 is the structural representation of preferred embodiment missile launcher shown in Figure 1 and toy guided missile;

Fig. 3 is the parts explosion of preferred embodiment missile launcher shown in Figure 1 and toy guided missile;

Fig. 4 is the structural representation of preferred embodiment toy guided missile detent mechanism shown in Figure 1;

Fig. 5 is the structural representation that rotation guided missile installing rack is removed shell body.

The specific embodiment

Shown in Fig. 1-5; Toy arms aircraft in this preferred embodiment; Comprise 1,2 missile launchers 2 of aircraft body and a plurality of toy guided missile 3; Said missile launcher 2 is installed on the aircraft body 1, and missile launcher 2 is positioned at aircraft body 1 below, and said toy guided missile 3 is installed on the missile launcher 2; Said missile launcher 2 comprises base 202, rotation guided missile installing rack 204, installing rack driving mechanism 203; Said installing rack driving mechanism 203 is fixed on the base 202; Said rotation guided missile installing rack 204 rotating being fixed on the base 202, installing rack driving mechanism 203 connect rotation guided missile installing rack 204.Aircraft body 1 is a toy helicopter in the present embodiment.

Said rotation guided missile installing rack 204 comprises shell body 20404, prelocalization frame 20403, back locating rack 20401 and 5 toy guided missile detent mechanisms 20402.The leading flank of said base 202 is provided with toy guided missile detent mechanism opening device 202021; The front end of said shell body 20404 has 5 guided missile inlets 204041; Prelocalization frame 20403, back locating rack 20401 are installed in respectively in the shell body 20404, and said toy guided missile detent mechanism 20402 is arranged on the prelocalization frame 20403; Said back locating rack 20401 comprises that cross section is pentagonal front rod 204012, back joint pin 204011 and 5 spacers 204013; Front rod 204012 rear ends connect the front end of back joint pin 204011; Said spacer 204013 is fixed on joint pin 204011 outer circumference surfaces of back; The rear end of prelocalization frame 20403 has the slot 204031 identical with front rod 204012 cross sections; Back joint pin 204011 rotating being fixed on the base 202 of back locating rack 20401; And back joint pin 204011 is connected and installed frame driving mechanism 203, and the front rod 204012 of back locating rack 20401 inserts in the slot 204031 of prelocalization frame 20403, and forms 5 toy guided missile positioning chambers between prelocalization frame 20403, back locating rack 20401 and the shell body 20404; Said toy guided missile detent mechanism 20402 is corresponding one by one with toy guided missile positioning chamber, and toy guided missile detent mechanism 20402 is located at the rear portion of toy guided missile positioning chamber.

Toy guided missile 3 is made up of two parts, i.e. body 302 and bullet 303.Body 302 is processed by the ABS material, and bullet 303 is processed by environmental protection soft PVC, and is not only safe but also reliable.The middle part of said body 302 peripheries has locating slot 301.

Said toy guided missile detent mechanism 20402 comprises small footprint 204021, spring reference column 204022, spring 204024, supporting rod 204023; Spring reference column 204022 is fixed on small footprint 204021 front ends; Spring 204024 is enclosed within on the spring reference column 204022, and the rear end of supporting rod 204023 is fixed on the small footprint 204021, and the rear portion of supporting rod 204023 is a curved surface 2040231; Supporting rod 204023 middle parts are provided with rotating shaft 2040233; Said rotating shaft 2040233 rotating being fixed on the prelocalization frame 20403, the front end of supporting rod 204023 is provided with clamping and colludes 2040232, clamping collude 2040232 catch on toy guided missile 3 locating slot 301 rear walls.

Said base 202 is made up of with rear base panel 2021 preceding base panel 2022; Form base intracavity between preceding base panel 2022 and the rear base panel 2021; Installing rack driving mechanism 203 comprises motor 20302, train of reduction gears 20301; Motor 20302 is fixed on preceding base panel 2022 leading flanks; Said train of reduction gears 20301 is installed in the base intracavity, and the input gear of train of reduction gears 20301 is installed on the output shaft of motor 20302, and the output gear of train of reduction gears 20301 is coaxial fixing with the back joint pin 204011 of back locating rack 20401.

In order to make missile launcher 2 more true to nature, said missile launcher 2 also is provided with back decorative box 201, and said back decorative box 201 is fixed on the trailing flank of base 202.

People can remote control missile launcher 2 emit toy guided missile 3, impact all types of target, perhaps resist with other toy airplane.At first, toy guided missile 3 is filled in the toy guided missile positioning chamber from guided missile inlet 204041, toy guided missile 3 overcomes the power of spring 201022 to the motion of toy guided missile positioning chamber bottom, up to clamping collude 2040232 catch on locating slot 301 rear walls of toy guided missile 3 till.Then, people can take off by telecontrolled aircraft body 1, in aircraft body 1 flight course; People can work by remote-control motor 20302; The output shaft of motor 20302 drives train of reduction gears 20301 and rotates, and makes rotation guided missile installing rack 204 and then rotate, when the curved surface 2040231 at supporting rod 204023 rear portions by 202021 crimps of toy guided missile detent mechanism opening device; The clamping of these supporting rod 204023 front ends collude 2040232 just break away from toy guided missile 3 locating slot 301; Said spring 201022 just ejects toy guided missile 3, makes toy guided missile 3 penetrate from guided missile inlet 204041, strikes target.

The preferred embodiment that the above is merely the utility model is not the practical range that is used for limiting the utility model; Be all equivalents of being done according to the claim scope of the utility model, be the utility model claim scope and cover.

Claims

1. a toy is equiped with arms aircraft; Comprise aircraft body; It is characterized in that: also comprise at least one missile launcher and at least one toy guided missile; Said missile launcher is installed on the aircraft body, and missile launcher is positioned at aircraft body below, and said toy guided missile is installed on the missile launcher; Said missile launcher comprises base, rotation guided missile installing rack, installing rack driving mechanism, and said installing rack driving mechanism is fixed on the base, rotating being fixed on the base of said rotation guided missile installing rack, and the installing rack driving mechanism connects rotation guided missile installing rack.

2. toy arms aircraft as claimed in claim 1; It is characterized in that: said rotation guided missile installing rack comprises shell body, prelocalization frame, back locating rack and at least one toy guided missile detent mechanism; The leading flank of said base is provided with toy guided missile detent mechanism opening device; The front end of shell body has at least one guided missile inlet, and prelocalization frame, back locating rack are installed in respectively in the shell body, and said toy guided missile detent mechanism is arranged on the prelocalization frame; Said back locating rack comprises front rod, back joint pin and at least one spacer; The front rod rear end connects the front end of back joint pin; Said spacer is fixed on the joint pin outer circumference surface of back; The rear end of prelocalization frame has slot, rotating being fixed on the base of back joint pin of back locating rack, and the back joint pin is connected and installed the frame driving mechanism; The front rod of back locating rack inserts in the slot of prelocalization frame; And form at least one toy guided missile positioning chamber between prelocalization frame, back locating rack and the shell body, said toy guided missile detent mechanism is corresponding one by one with toy guided missile positioning chamber, and toy guided missile detent mechanism is located at the rear portion of toy guided missile positioning chamber.

3. toy as claimed in claim 2 arms aircraft is characterized in that: the number of the number of the number of said spacer, toy guided missile detent mechanism, the number of toy guided missile positioning chamber, guided missile inlet, the number of toy guided missile detent mechanism are all identical.

4. toy arms aircraft as claimed in claim 3, it is characterized in that: the middle part of said toy guided missile periphery has locating slot, and said toy guided missile detent mechanism comprises small footprint, spring reference column, spring, supporting rod; The spring reference column is fixed on the small footprint front end; Spring housing is on the spring reference column, and the rear end of supporting rod is fixed on the small footprint, and the rear portion of supporting rod is a curved surface; The supporting rod middle part is provided with rotating shaft; Said rotating shaft is rotating to be fixed on the prelocalization frame that rotates the guided missile installing rack, and the front end of supporting rod is provided with clamping and colludes, and the locating slot rear wall of toy guided missile is caught in clamping.

5. toy arms aircraft as claimed in claim 4; It is characterized in that: said base is made up of preceding base panel and rear base panel; Form base intracavity between preceding base panel and the rear base panel; The installing rack driving mechanism comprises motor, train of reduction gears, and on the base panel leading flank, said train of reduction gears was installed in the base intracavity before motor was fixed on; And the input gear of train of reduction gears is installed on the output shaft of motor, and the output gear of train of reduction gears is coaxial fixing with the back joint pin of back locating rack.

6. toy arms aircraft as claimed in claim 5, it is characterized in that: said missile launcher also is provided with the back decorative box, and said back decorative box is fixed on the trailing flank of base.