CN2290375Y - Control rack of wire-controlled airplane - Google Patents

Control rack of wire-controlled airplane Download PDF

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Publication number
CN2290375Y
CN2290375Y CN 96222530 CN96222530U CN2290375Y CN 2290375 Y CN2290375 Y CN 2290375Y CN 96222530 CN96222530 CN 96222530 CN 96222530 U CN96222530 U CN 96222530U CN 2290375 Y CN2290375 Y CN 2290375Y
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China
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control
metallic rod
pedestal
hollow axis
rod body
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Expired - Fee Related
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CN 96222530
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Chinese (zh)
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庄宗明
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Individual
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Individual
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Abstract

The utility model relates to a control rack of a wire-controlled airplane, which is arranged on an angle rack. The control rack of a wire-controlled airplane is connected with a model airplane by two first conducting wires, and is connected with a manually operated power control device by first control wires. The control rack of a wire-controlled airplane comprises a rotary control mechanism, a steering transmission mechanism and a traction mechanism which are pivoted mutually, a hollow shaft body, a metal rod body and a power supply transduction mechanism, wherein, the hollow shaft body is arranged on the angle rack; the metal rod body is pivoted in the hollow shaft body and is pivoted with the rotary control mechanism. The first control wires are driven by an operating power supply device and the force is driven to the power supply transduction mechanism; meanwhile, the steering transmission mechanism, the traction mechanism and the two first wires are driven to enable the airplane to move freely.

Description

Line traffic control aircraft handling frame
The utility model relates to a kind of line traffic control aircraft, relates to the control frame structure of line traffic control aircraft or rather.
The line traffic control aircraft of traditional structure needs in the place of spaciousness nearly center to handle, because at present can be fewer and feweri for movable place in the city, therefore is subjected to the place restriction to cause controlling motion and can not promoting of line traffic control aircraft.
The purpose of this utility model is a kind of line traffic control aircraft handling frame of design, can can't handle its activity freely in the movable space at general line traffic control aircraft.
The utility model is to connect the manual power device and be the line traffic control aircraft handling shelf structure of activity centre with rotation control mechanism, steering gear, haulage gear and the formation of first lead with the corner bracket by power supply transduction mechanism by cable.
Line traffic control aircraft handling frame of the present utility model, be installed on the corner bracket, be connected with the model of an airplane and be connected with the power control of manual control by two first leads, comprise rotation control mechanism, steering gear and the haulage gear of mutual pivot joint, it is characterized in that by first control line:
Also include hollow axis body, metallic rod body and power supply transduction mechanism;
Described hollow axis body is installed on the corner bracket, and the hollow axis body is provided with at least one first conduction lamellar body away from the ora terminalis of corner bracket one end; Described metallic rod body is a cylinder, is articulated in the axis body of described hollow axis body, and the metallic rod body first conduction lamellar body surperficial and on the described hollow axis body contacts; Described power supply transduction mechanism is set on the metallic rod body, metallic rod body and described rotation control mechanism articulate, comprise a ring body, one pedestal, conducting element and at least one second conduction lamellar body, described ring body is provided with axial through hole, make ring body on the metallic rod body, move down, described pedestal is arranged on ring body near hollow axis body one side, pedestal is provided with axial through hole makes pedestal show to rotate at the bottom of ring body, described conducting element is arranged on the ring body surface place of pedestal top, the described second conduction lamellar body is arranged on the pedestal top, and the second conduction lamellar body contacts with conducting element; Described metallic rod body connects respectively with conducting element and establishes a lead and be connected described two first leads respectively.
Described hollow axis body is provided with at least one first conductive seat away from the ora terminalis of corner bracket one end, and the described first conduction lamellar body is arranged on first conductive seat.
Described pedestal top is provided with at least one second conductive seat, and the described second conduction lamellar body is arranged on second conductive seat.
Described metallic rod body and first conducts electricity and contacts with parallel mode between lamellar body.
Described conducting element and second conducts electricity and contacts with parallel mode between lamellar body.
Line traffic control aircraft handling frame of the present utility model, combining structure by hollow axis body, metallic rod body, power supply transduction mechanism, rotation control mechanism, steering gear and haulage gear, formation is the line traffic control aircraft of activity centre with the corner bracket, handle power control, drive first control line and strength is transferred to power supply transduction mechanism, rotation control mechanism, steering gear, haulage gear and two first leads, make aircraft movable freely.
Further specify technology of the present utility model below in conjunction with the embodiment accompanying drawing
Fig. 1 line traffic control aircraft handling frame perspective view;
Fig. 2 line traffic control aircraft handling frame operation state schematic diagram;
Fig. 3 line traffic control aircraft handling frame sectional perspective structural representation;
The three-dimensional decomposition texture schematic diagram of Fig. 4 line traffic control aircraft handling frame;
The model of an airplane perspective view that Fig. 5 cooperates with line traffic control aircraft handling frame;
Referring to Fig. 1, line traffic control aircraft handling frame 1 is installed on the corner bracket 2, be connected with the model of an airplane 3 by two first leads 10, control frame 1 is by first control line 11 (see figure 2) that is connected with manual power control, and first control line 11 is the cables with the control second lead effect.The model of an airplane 3, control frame 1 and corner bracket 2 etc. constitute with the control frame 1 installed on the corner bracket 2 operation, the action center as the model of an airplane 3.
Referring to Fig. 2, the operator handles power control 7 with manual mode near control frame 1, makes the model of an airplane 3 do to comprise that 360 degree are rotated in interior various grandstand plays.
Also combination is referring to Fig. 4 referring to Fig. 3, and this control frame 1 is provided with a hollow axis body 13, the metallic rod body 12 that in hollow axis body 13, is pivoted, and metallic rod body 12 can rotate in hollow axis body 13 for cylinder.Hollow axis body 13 is provided with first conductive seat 131 with the ora terminalis 130 that metallic rod body 12 articulates a side, be equipped with the first conduction lamellar body 132 on this first conductive seat 131 with metallic rod body 12 surperficial parallel contacts, no matter metallic rod body 12 relatively rotates in which way with hollow axis body 13, can guarantee that all the first conduction lamellar body 132 contacts with metallic rod body 12, the sheathed power supply transduction in the appropriate position of metallic rod body 12 above hollow axis body 13 mechanism 20.
Power supply transduction mechanism 20 is provided with a ring body 21, ring body 21 is provided with axial through hole, this through hole can make ring body 21 upper and lower moving in metallic rod body 12, ring body 21 is near the sheathed pedestal 22 of a side of hollow axis body 13, also be provided with axial through hole on this pedestal 22, pedestal 22 can rotate on the surface of ring body 21.The conducting element 23 that ring body 21 bottom surfaces of pedestal 22 tops are sticked and are made by metal material, this conducting element 23 is provided with ring slice 24, and be convexly equipped with a lamellar body 25 (lamellar body 25 is one-body molded with ring slice 24, makes by conductive material) in ring slice 24 upper limbs one end towards direction away from metallic rod body 12.Pedestal 22 1 sides outwards are convexly equipped with a fixed bar 26 with the radial direction of metallic rod body 12, are provided with the screw thread (not shown) in the ora terminalis of fixed bar 26, establish screw 27 for lock.
Pedestal 22 tops are provided with second conductive seat 28; this second conductive seat 28 is provided with and the conducting element 23 ring slices 24 parallel contacted second conduction lamellar bodies 29; no matter ring body 21 and pedestal 22 relative motion in which way; can guarantee that all the conduction of second on the pedestal 22 lamellar body 29 contacts with conducting element 23; in addition, ring body 21 tops radially are convexly equipped with a pin joint seat 220 along metallic rod body 12.Be arranged with rotation control mechanism 30 on the metallic rod body 12 of these power supply transduction mechanism 20 tops.
Rotation control mechanism 30 comprises: one slightly becomes the pedestal 31 of U type, establishes pivoted hole in U type pedestal 31 bottoms, and this pivoted hole is set in metallic rod body 12 tops, and can make U type pedestal 31 rotate on metallic rod body 12.Be respectively equipped with corresponding fixing hole on the lamellar body 310,311 of U type pedestal 31 both sides, metallic rod body 12 1 sides that articulate with these U type pedestal 31 bottoms connect in the radial direction at it and set out a metal lamellar body 121, and these U type pedestal 31 bottoms convex with holder 312.
Rotation block 32, by 321 chimeric compositions of block 320, counterweight block, block 320 slightly in echelon among the figure, also can make other shapes during enforcement, counterweight block 321 slightly becomes oval tubbiness, the intermarginal groove of offering in oval tubbiness two ends, this counterweight block 321 can be by the trapezoidal bottom tabling of groove and block 320, and block 320 weight of rotation block 32 are lighter than counterweight block 321 far away.Counterweight block 321 and rotation block 320 combination backs are protruding to be exposed on the block 320 of counterweight block 321 1 side edge pivoted hole, and is provided with the through holes that bending 90 is spent between the ora terminalis of side edge and block 320 upper ends in addition at block 320.
Combination is referring to Fig. 1, Fig. 4 again, and steering gear 40 is provided with one group of trace 41, and this group trace 41 is provided with one first body of rod 42, and these first body of rod, 42 1 side vertical junction are established one second body of rod 43, and these first body of rod, 42 other sides then connect establishes second body of rod 44.
Referring to Fig. 4, the another side that second body of rod 43 and first body of rod 45 join is equipped with a steering component 45, this steering component 45 is provided with a body of rod 451, these body of rod 451 other ends are provided with hollow ring body 452, the body of rod 451 is established with the surperficial vertical junction of hollow ring body 452, be provided with ball 453 in the hollow ring body 452, ball 453 is provided with through hole.
Haulage gear 50 is provided with second control line 51; this second control line 51 penetrates the through hole of rotation control mechanism 30 blocks 320; and this second control line 51 passes through hole on the ball 453 of steering gear 40 steering components 45; second control line 51 is in outside the through hole away from steering gear 40 1 ends; and connect with a body of rod 510; sheathed body 52 outside the control line 51 that is equipped with the body of rod 510 1 ends; with this body 52 protections second control line 51; guarantee the stability of control action, can prevent that also second control line 51 and the body of rod 510 from being bent and rupture.Body 52 another terminations are established a control element 53, this control element 53 by control inlay 530 with Matrix body 531 constitutes by retaining element 550 is fixing, and control inlay 530 is provided with hollow tube 540, and the both sides corresponding with hollow tube 540 are respectively equipped with a lamellar body 541,542, are respectively equipped with corresponding through hole on the lamellar body 541,542. Matrix body 531 both sides are respectively equipped with a fixing hole 532,533, in Matrix body 531 centers locate to be provided with through hole 534 on the lower side.
During haulage gear 50 entire combination, the hollow tube 540 that will control inlay 530 earlier is linked in body 52 1 ends, makes the bending of the body of rod 510 1 ends pass The through hole 534 of below, matrix body 531 centers.
The relation that steering gear 40, power supply transduction mechanism 20, rotation control mechanism 30 and haulage gear are 50 is: second control line 51 of haulage gear 50 passes the spin 453 of steering gear 40, and by retaining element 46 second control line 51 is fixed on hollow ring body 452 outsides that are provided with ball 453 in these steering component 45 1 sides, second control line 51 be in steering component 45 with
Figure Y9622253000061
31 of type pedestals, the elasticity of second control line 51 should be moderate, and control line 51 is good with twisted wire.The holder 312 that first body of rod 42 of the trace 41 of steering gear 40 and second body of rod 43 connect the position of establishing and U type pedestal 31 articulates, and the 3rd body of rod 44 of steering gear 40 traces 41 connects with the pin joint seat 220 of power supply transduction mechanism 20.
Second lead 11 among Fig. 1 is connected with the power supply of power control, this second lead 11 is a cable, on the earth terminal of cable and first conductive seat 131 first conduction lamellar body 132 (see figure 3) of joining, the positive terminal of cable then is locked in the fixed bar 26 and screw 27 of power supply transduction mechanism 20, and the cable positive terminal also is connected with the second conduction lamellar body 29 of second conductive seat 28.10 in first lead connects the metal lamellar body 121 of U type pedestal 31 bottoms and the lamellar body 25 on power supply transduction mechanism 20 conducting elements 23 respectively, makes first wire connecting power.First lead 10 passes haulage gear 50 more respectively
Figure Y9622253000062
The fixing hole 532,533 of matrix body 531 both sides.
Combination is referring to Fig. 1 again, handle when using, the interactive relationship that power supply transduction mechanism 20, rotation control mechanism 30, steering gear 40, haulage gear 50 and first lead are 10 is: when the operating power control device, it drives first control line 11 that is connected, because first control line 11 is cables, so control device can drive to strength on the pin joint seat 220 of power supply transduction mechanism 20 1 sides, power supply transduction this moment mechanism 20 i.e. upper and lower moving on metallic rod body 12.This power supply transduction mechanism 20 drives steering gear 40 simultaneously, steering gear 40 is promptly because of on second body of rod 44, lower swing and make an end that is equipped with steering component 45 on second body of rod 43 on a left side, (end that joins because of second body of rod 43 and first body of rod 42 is with holder 312 pivot joints of U type pedestal 31 in swing on the right, with second control line, 51 meetings of ball 453 sockets thereby produce away from or near the perseveration of U type pedestal 31, and second control line 51 affects the body of rod 510, even the body of rod 510 shape lamellar bodies 531 are on vertical direction is done, therefore the action of lower swing is installed in Two first leads 10 on the shape lamellar body 531 two ends fixing holes 532,533 will produce tandem action).
Referring to Fig. 5, from
Figure Y9622253000064
Two first leads 10 that shape lamellar body 531 two ends are set out, two leads 301 of link model aircraft 3 inputs, the power supply that this lead 301 is provided by the structure of the model of an airplane 3 inside is connected with the power input of motor 302, utilize the empennage 303 of the lead 301 control model of an airplanes 3 to make upper and lower wobbling action, allow the model of an airplane 3 do various flight by manipulator's wish.After the model of an airplane takes off, because of rotation control mechanism 30 is provided with counterweight block 321, even therefore when the model of an airplane 3 when circling in the air with the direction of 31 one-tenth levels of U type pedestal, under the effect of reaction force, also can keep balance.Again because U type pedestal 31 and rotation block 32 structures that are articulated, and also mode of U type pedestal 31 and metallic rod body 12, spend and rotate and various grandstand plays so the model of an airplane 3 can do 360 on control frame 1 for articulating.
In the model of an airplane 3, be provided with go to action mechanism 60 in motor 302 rears, this go to action mechanism 60 is provided with T matrix body 61, and T matrix body 61 centers are provided with fixing hole 610, is respectively equipped with fixing hole 612,613 at transversal piece 611 two ends of this T matrix body 61; Go to action mechanism 60 also is provided with semicircle lamellar body 62, establishes with T matrix body 61 vertical junction.Two leads 301 pass the fixing hole 612,613 at transversal piece 611 two ends of T matrix body 61 respectively; 63 of the transmission bodies of rod and empennage 303 join.
When first lead 10 was done the action of front and rear direction, the lead 301 that drives the model of an airplane 3 was done the front and back action, and lead 301 orders connect the empennage of establishing with go to action mechanism 60 and make upper and lower wobbling action.
Line traffic control aircraft handling frame of the present utility model, be installed on the corner bracket, cable connects control frame and manual power control, by forming with the corner bracket with rotation control mechanism, steering gear, haulage gear and first lead is the line traffic control aircraft of activity centre, in general line traffic control aircraft can't movable space, have an easy control in the matter.

Claims (5)

1, a kind of line traffic control aircraft handling frame, be installed on the corner bracket, be connected with the model of an airplane and be connected with the power control of manual control by two first leads, comprise rotation control mechanism, steering gear and the haulage gear of mutual pivot joint, it is characterized in that by first control line:
Also include hollow axis body, metallic rod body and power supply transduction mechanism;
Described hollow axis body is installed on the corner bracket, and the hollow axis body is provided with at least one first conduction lamellar body away from the ora terminalis of corner bracket one end; Described metallic rod body is a cylinder, is articulated in the axis body of described hollow axis body, and the metallic rod body first conduction lamellar body surperficial and on the described hollow axis body contacts; Described power supply transduction mechanism is set on the metallic rod body, metallic rod body and described rotation control mechanism articulate, comprise a ring body, one pedestal, conducting element and at least one second conduction lamellar body, described ring body is provided with axial through hole, make ring body on the metallic rod body, move down, described pedestal is arranged on ring body near hollow axis body one side, pedestal is provided with axial through hole makes pedestal show to rotate at the bottom of ring body, described conducting element is arranged on the ring body surface place of pedestal top, the described second conduction lamellar body is arranged on the pedestal top, and the second conduction lamellar body contacts with conducting element; Described metallic rod body connects respectively with conducting element and establishes a lead and be connected described two first leads respectively.
2, line traffic control aircraft handling frame according to claim 1 is characterized in that: described hollow axis body is provided with at least one first conductive seat away from the ora terminalis of corner bracket one end, and the described first conduction lamellar body is arranged on first conductive seat.
3, line traffic control aircraft handling frame according to claim 1 is characterized in that: described pedestal top is provided with at least one second conductive seat, and the described second conduction lamellar body is arranged on second conductive seat.
4, line traffic control aircraft handling frame according to claim 1 is characterized in that: described metallic rod body and first conducts electricity and contacts with parallel mode between lamellar body.
5, line traffic control aircraft handling frame according to claim 1 is characterized in that: described conducting element and second conducts electricity and contacts with parallel mode between lamellar body.
CN 96222530 1996-09-05 1996-09-05 Control rack of wire-controlled airplane Expired - Fee Related CN2290375Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 96222530 CN2290375Y (en) 1996-09-05 1996-09-05 Control rack of wire-controlled airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 96222530 CN2290375Y (en) 1996-09-05 1996-09-05 Control rack of wire-controlled airplane

Publications (1)

Publication Number Publication Date
CN2290375Y true CN2290375Y (en) 1998-09-09

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Application Number Title Priority Date Filing Date
CN 96222530 Expired - Fee Related CN2290375Y (en) 1996-09-05 1996-09-05 Control rack of wire-controlled airplane

Country Status (1)

Country Link
CN (1) CN2290375Y (en)

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C19 Lapse of patent right due to non-payment of the annual fee
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