CN2309167Y - Air combat game computer - Google Patents

Air combat game computer Download PDF

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Publication number
CN2309167Y
CN2309167Y CN 97217989 CN97217989U CN2309167Y CN 2309167 Y CN2309167 Y CN 2309167Y CN 97217989 CN97217989 CN 97217989 CN 97217989 U CN97217989 U CN 97217989U CN 2309167 Y CN2309167 Y CN 2309167Y
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CN
China
Prior art keywords
seat
symmetry
rod
ejector
fuselage body
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Expired - Fee Related
Application number
CN 97217989
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Chinese (zh)
Inventor
林承达
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Individual
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Individual
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Publication date
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Priority to CN 97217989 priority Critical patent/CN2309167Y/en
Application granted granted Critical
Publication of CN2309167Y publication Critical patent/CN2309167Y/en
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Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to an air combat game machine, on which a machine table is arranged. Symmetrical machine bodies and defending barrier sheets are arranged inside the machine table; the machine bodies and the defending barrier sheets are respectively connected with handles on both sides of the machine table through rods, so that a player can control the machine bodies and the barrier sheets to shift forwards, backwards, to the left, and to the right; a conveying mechanism, an ejection mechanism, a standard target mechanism, etc. are arranged inside the machine body. A globular bullet can be led into an ejection seat by controlling the handle; the bullet can be ejected into a score hole of the other party from the ejection seat by pushing the handle; the ejection function of the other party can be stopped as hitting the standard target on the upper part of the machine body; the bullet can be supplied at any time through an elephant trunk and a funnel.

Description

The air battle game machine
The utility model relates to a kind of air battle game machine, refers to that especially a kind of player of supplying controls fuselage mutually to reach the craps game machine of attacking score.
Because the differentiation of lifestyle, make the modern lack very much the adjustment of amusement and recreation, and based on the result that all can develop, some indoor recreation grounds quite are subjected to liking of people, but these sports grounds mostly are provided with TV type Game device or fruit machine, and be not suitable for the whole family's participation, and this TV type Game device also influences people's eyesight in long-time direct-view.
The utility model main purpose is to provide a kind of air battle game machine, and it is a kind of mechanical device, but practical operation is carried out in simulated air combat, increases the interest of recreation.
The purpose of this utility model is to realize like this, a kind of air battle game machine promptly is provided, it comprises: a board, its left and right sides wall is respectively equipped with groove and microscler groove, wears two sliding bars in it, is respectively equipped with fuselage body and defence catch on the described sliding bar, described fuselage body and defence catch are arranged in the translot of described board front and back side with the body of rod, the described body of rod is connected with handle, and the inner edge of side then is respectively equipped with Yi Biyuan before and after the described board, and described wall wall is provided with several circular holes; One ejector-seat, be located on the set slide rail in described fuselage body the place ahead, its below is an oblique shape groove, the top is the sheet that colludes of symmetry, the side wall is provided with a tooth bar, and described tooth bar meshes a gear, and center, described gear top is provided with check grid, described ejector-seat bottom vertical is extended a lamellar body, and the front and back end of described lamellar body is connected in the head of described fuselage body and the ejector block at rear with spring and trace respectively; One colludes and holds seat, is located at top, described ejector-seat rear end, and it is one anti-L shaped, and its horizontal part front end is provided with a hook part, and the upper end of vertical component effect then is provided with a circular cover, describedly colludes the fixed bar that the pedestal backplate both sides of holding seat are provided with symmetry, wears spring on it; One target is located at described fuselage body top, and its bottom is provided with the clip-connecting rod of symmetry, and described clip-connecting rod bottom is provided with tab, and described tab both sides are provided with the fixed leg of symmetry; One shooting handle, it comprises a hollow tube of being located at described body of rod end, described body top articulates the depression bar of symmetry, two depression bars articulate mutually with a brace that is arranged in the chute of the described body of rod, described depression bar surface coating one lever, the bottom of described lever holds with a spring and described body, the bottom of described depression bar then articulates the lead-in wire that trace connected by described ejector-seat, the internal sleeve of described body is equipped with a button, described button articulates the drive link of symmetry and is connected in a holding sheet, and the described lead-in wire that drive link connected of holding seat that colludes is articulated in described holding sheet.
The advantage of the utility model device is, reaches the purpose of simulated air combat with mechanical device, and is easy to operate, interesting strong.
Below in conjunction with accompanying drawing, embodiment of the present utility model is described, wherein:
Fig. 1 is a schematic perspective view of the present utility model;
Fig. 2 is the three-dimensional exploded view of fuselage body of the present utility model;
Fig. 3 is the transmission mechanism allocation plan of fuselage of the present utility model;
Fig. 4 A, 4B are the action schematic diagram of body of rod drive-connecting shaft of the present utility model;
Fig. 5 is a lead-in wire connected structure schematic diagram of the present utility model;
Fig. 6 is the handle structural scheme of mechanism of controlling of the present utility model;
Fig. 7 is the action embodiment schematic diagram that shoots of the present utility model;
Fig. 8 is the action embodiment schematic diagram that launches of the present utility model;
Fig. 9 is a target action schematic diagram of the present utility model;
Please consult shown in Figure 1 earlier, the utility model mainly is provided with a board 1, left side in board 1, right two side walls 11, be respectively equipped with groove 111 on 12,121 and microscler groove 112,122 for sliding bar 13,14 wear, and in this sliding bar 13, be respectively equipped with fuselage body 2 and defence catch 3 on 14, and be provided with a funnelform bullet receiver 27 in fuselage body 2, and with this fuselage body 2 and catch 3 with the body of rod 20,30 be arranged in board 1 before, the translot 15 of rear side, after 16, be connected in handle 22,32, and this wall 11,12 microscler groove 112,122 the place aheads then are respectively equipped with circular hole 113,123, for the player fuselage body 2 is controlled to this circular hole 113,123 limits, make the opening of the body of rod 20 be resisted against circular hole 113,123, thereby can be by circular hole 113,123 drop into spherical projectiles to fuselage body 2 inside, the inner edge of this board 1 front and back side then respectively is provided with a wall wall 17,18, and in this wall wall 17, several circular holes 171 are set on 18,181, to detect score, combination via above-mentioned member, the hand-holdable handle 22 of player, 32, to control fuselage body 2 and catch 3 along groove 111,121 and microscler groove 112,122 and translot 15, before 16 works, after, a left side, right displacement, and by the control of handle 22, spherical projectiles in the fuselage body 2 is injected the other side's circular hole 171, in 181, or control the bullet that catch 3 stops that the other side penetrates by handle 32, to constitute the recreation of simulated air combat, the bullet of being injected then falls within a microscler box body 1711 (figure does not show) respectively, in 1811, extract this box body 1711 out for the player, 1811, the built-in bullet of taking is thrown to circular hole 113,123 is interior via trunk formula pipe 114,124 import funnelform bullet receivers 27 and arrive and put in the magazine.
See also Fig. 2,3, these fuselage body 2 inside are provided with an ejector-seat 21, these ejector-seat 21 belows are an oblique shape groove 211, the top is then for colluding sheet 212, and a microscler tooth bar 213 is set at the side wall surface of this ejector-seat 21, make this tooth bar 213 engagements one gear 2131, and establish check grid 2132 in gear 2131 tops, the bottom vertical of this ejector-seat 21 is extended a lamellar body 214, the front and back end of this lamellar body 214 is connected in the head of fuselage body 2 and the ejector block 217 at rear with spring 215 and trace 216 respectively, this ejector-seat 21 is placed on a slide rail 23, with the pulling by trace 216 and spring 215, moves along this slide rail 23; And when behind this ejector-seat 21, moving,, make check grid 2132 backstops in oblique shape groove 211 the place aheads because of 2131 rotations of tooth bar 213 driven gears.
The top of these ejector-seat 21 rear ends is provided with one and is anti-L shaped colluding and holds seat 24, this colludes the horizontal part front end of holding seat 24 and is provided with a hook part 241, the upper end of vertical component effect then is provided with a circular cover 240, and be provided with the fixed bar 242 of symmetry in the both sides of pedestal backplate, for wearing spring 243, this colludes holds seat 24 suitable hypsokinesis, makes ejector-seat 21 when post-tensioning, collude to close and hold seat 24 hook part 241 to collude sheet 212, with action to be launched in colluding;
The back upper place of this slide rail 23 is provided with one and puts magazine 25, this puts magazine 25 front ends is a bending body 251, the outlet of this body 251 is suspended on the plane of ejector-seat 21, the rear end then is connected mutually with the outlet of funnel-form bullet receiver 27, after spherical projectiles 26 is dropped into by this receiver 27, concentrate on this and put magazine 25, and owing to put the inside of magazine 25 is the inclined-plane, bullet is concentrated to body 251 landings, so can be when trace 216 post-tensionings, spherical projectiles 26 can be fallen within the oblique shape groove 211 of ejector-seat 21 by the outlet of body 251, and nationality prevents that by the backstop of check grid 2132 it from outwards dropping.
The top of this fuselage body 2 is provided with a target 28, the bottom of this target 28 respectively is articulated with a tab 281 with the clip-connecting rod 280 of symmetry, this tab 281 is provided with fixed leg 2811, make to collude and hold seat 24 vertical component effect and stretch between two clip-connecting rods 280, when target 28 is gone down, hold holding of seat 24 circular cover 240 because of 281 pairs of tabs collude, make to collude and hold seat 24 and lean forward and can't collude and hold ejector-seat 21, to end to launch function.
See also shown in Fig. 1,4A, the 4B, this body of rod 20 is placed on the drive-connecting shaft 201 of clamping on the translot 16 of board 1, this drive-connecting shaft 201 is a hollow tube, its both ends open edge is provided with prominent ring 202, for the translot 16 that is clamped on board 1, its inner rim then is nested with another pipe 203, and the surface central authorities of this pipe 203 are sticked in the internal face of drive-connecting shaft 201 with a card post 2031, so, the body of rod 20 can move forward and backward along pipe 203, as Fig. 4 A, and because of the card post 2031 formed fulcrums of pipe 203, and constitute upper and lower swing, as Fig. 4 B; See also shown in Fig. 5,8, trace 216 in this fuselage body 2 and collude and hold seat 24 and be connected with lead-in wire 2161 and 2441 respectively, and stretch in fuselage body 2 outsides, wherein, lead-in wire 2161 is connected in a guiding mechanism that is made of bolt 2162, for the elasticity of adjusting lead-in wire 2161, going between 2441 then is connected in the guiding mechanism that another is made of bolt 2442, and it is interior and be connected in handle that this lead-in wire 2161 and 2441 is arranged in the body of rod 20 respectively.
See also Fig. 1, shown in 6, this handle 22 is positioned at the end of the body of rod 20, it is provided with a vertical hollow tube 221, articulate the depression bar 222 of symmetry in the top of this body 221, make this depression bar 222 be arranged in the chute 204 of the body of rod 20 with a connecting piece 2221, to constitute mobile location, and in depression bar 222 surperficial coating one levers 223, the bottom of this lever 223 is held with body 221 with a spring 224, the bottom of depression bar 222 then articulates the lead-in wire 2161 that is connected by the trace 216 in the fuselage body 2, make depression bar 222 when pushing, ejector-seat 21 is pulled back, hold seat 24 to collude to close in colluding, then be equipped with a button 225 in the body 221, this button 225 is articulated in the drive link 226 of symmetry, holds the lead-in wire 2441 that seat 24 drive link 244 connected and is articulated in this holding sheet 227 to be connected in a holding sheet 227, to make to collude, when button 225 presses down, hold seat 24 and break away from because of moving behind the holding sheet 227, make to collude with ejector-seat 21, with ejector-seat 21 ccontaining spherical projectiles 26 outwards launch.
See also Fig. 7, and cooperation Fig. 1,2, the utility model is when operation, except that the displacement of control fuselage body 2, when handle 22 pressings, ejector-seat 21 can be pulled back, make its be sticked in collude hold the seat 24, and make spherical projectiles 26 fall within the oblique shape groove 211 of ejector-seat 21, nationality with spherical projectiles 26 backstops that fall into and prevent its outside landing, forms state to be penetrated, as shown in Figure 8 by check grid 2132, when the button 225 of handle 22 presses down, ejector-seat 21 will be broken away from, and check grid 2132 are opened because of backward rotation, and because of the pulling force of spring 215, spherical projectiles 26 is launched score hole to the other side, constituted the craps game effect of simulated air combat.
As shown in Figure 9, when target 28 is hit and when falling, the tab 281 of its bottom will collude the circular cover 240 of holding seat 24 tops because of rotation and hold, make relatively to collude and hold seat 24 and be the shape that leans forward, ejector-seat 21 promptly can't collude and close, and makes to launch action and end.

Claims (3)

1. air battle game machine is characterized in that it comprises:
One board, its left and right sides wall is respectively equipped with groove and microscler groove, wear two sliding bars in it, be respectively equipped with fuselage body and defence catch on the described sliding bar, described fuselage body and defence catch are arranged in the translot of described board front and back side with the body of rod, the described body of rod is connected with handle, and the inner edge of side then is respectively equipped with Yi Biyuan before and after the described board, and described wall wall is provided with several circular holes;
One ejector-seat, be located on the set slide rail in described fuselage body the place ahead, its below is an oblique shape groove, the top is the sheet that colludes of symmetry, the side wall is provided with a tooth bar, and described tooth bar meshes a gear, and center, described gear top is provided with check grid, described ejector-seat bottom vertical is extended a lamellar body, and the front and back end of described lamellar body is connected in the head of described fuselage body and the ejector block at rear with spring and trace respectively;
One colludes and holds seat, is located at top, described ejector-seat rear end, and it is one anti-L shaped, and its horizontal part front end is provided with a hook part, and the upper end of vertical component effect then is provided with a circular cover, describedly colludes the fixed bar that the pedestal backplate both sides of holding seat are provided with symmetry, wears spring on it;
One target is located at described fuselage body top, and its bottom is provided with the clip-connecting rod of symmetry, and described clip-connecting rod bottom is provided with tab, and described tab both sides are provided with the fixed leg of symmetry;
One shooting handle, it comprises a hollow tube of being located at described body of rod end, described body top articulates the depression bar of symmetry, two depression bars articulate mutually with a brace that is arranged in the chute of the described body of rod, described depression bar surface coating one lever, the bottom of described lever holds with a spring and described body, the bottom of described depression bar then articulates the lead-in wire that trace connected by described ejector-seat, the internal sleeve of described body is equipped with a button, described button articulates the drive link of symmetry and is connected in a holding sheet, and the described lead-in wire that drive link connected of holding seat that colludes is articulated in described holding sheet.
2. air battle game machine as claimed in claim 1, it is characterized in that, the body of rod that described fuselage body connected is provided with a drive-connecting shaft, described drive-connecting shaft is a hollow tube, and its both ends open edge is provided with prominent ring, and inner edge then is nested with another pipe, described pipe surface central authorities are provided with a card post, described card post is sticked in the internal face of described drive-connecting shaft, and the described body of rod is set in the described pipe and moves forward and backward along described pipe, and is the upper and lower swing of fulcrum with described card post.
3. air battle game machine as claimed in claim 1, it is characterized in that, circular hole and trunk shape that described board both sides are respectively equipped with symmetry are dropped into pipe, described fuselage body top is provided with funnelform receiver, described receiver and the described magazine of putting connect, and are fallen within via the funnel-form receiver by the spherical projectiles of described circular hole input and put magazine and replenish bullet in recreation.
CN 97217989 1997-09-01 1997-09-01 Air combat game computer Expired - Fee Related CN2309167Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 97217989 CN2309167Y (en) 1997-09-01 1997-09-01 Air combat game computer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 97217989 CN2309167Y (en) 1997-09-01 1997-09-01 Air combat game computer

Publications (1)

Publication Number Publication Date
CN2309167Y true CN2309167Y (en) 1999-03-03

Family

ID=33934379

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 97217989 Expired - Fee Related CN2309167Y (en) 1997-09-01 1997-09-01 Air combat game computer

Country Status (1)

Country Link
CN (1) CN2309167Y (en)

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GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee