CN2882742Y - Pilot ejection parachuting device of toy aircraft - Google Patents
Pilot ejection parachuting device of toy aircraft Download PDFInfo
- Publication number
- CN2882742Y CN2882742Y CN 200620057467 CN200620057467U CN2882742Y CN 2882742 Y CN2882742 Y CN 2882742Y CN 200620057467 CN200620057467 CN 200620057467 CN 200620057467 U CN200620057467 U CN 200620057467U CN 2882742 Y CN2882742 Y CN 2882742Y
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- cylinder
- seat
- pilot
- toy aircraft
- slide block
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Abstract
The utility model provides an ejection bailout device for the pilot of toy aircraft, which comprises a toy aircraft. A pilot, a chair seat, an ejection mechanism and a braking mechanism are arranged in the flight deck of the toy aircraft. Under the condition of ready to launch, a guide column is positioned inside a cylinder of the stand and the chair seat; the lower end surface of the chair seat cylinder press a washer and a spring to shrink into the cylinder of stand for energy storage; the cylinder of chair seat is buckled reversely to the chair seat cylinder; an extruding brim on the lower end surface of the chair seat cylinder is clamped by a sliding block of the braking mechanism. Under the condition of launch, the braking mechanism control the sliding block to shrink back and separate from the extruding brim of the chair seat cylinder. At the time, the spring releases energy and the washer propel the chair seat and the pilot connected to the chair seat to eject out of the aircraft in the upward direction. The utility model, with simple and compact structure, small volume, light weight and excellent performance in safety and reliability, can realize stunt ejection action and facilitate the manufacturing, assembly and application.
Description
Technical field
The utility model relates to toy, is specifically related to a kind of pilot ejection parachute device that is provided with the toy aircraft of spring catapult-launching gear.
Background technology
In the prior art, what some toy aircraft were arranged possesses simulation paraoperation function, and the operator can drop from the air the simulation paratrooper on some toy airplane by straighforward operation.But do not find to be provided with the toy aircraft that the pilot simulates the parachute jumping escape device at present as yet.
The utility model content
The purpose of this utility model is, provides under a kind of operator's of can be implemented in the control, and the pilot can carry out the pilot ejection parachute device of the toy aircraft of emulation parachute jumping escape action.
The utility model for achieving the above object, and the technical scheme that provides is as follows: a kind of pilot ejection parachute device of toy aircraft, comprise toy aircraft, it is characterized in that: described toy aircraft driving cabin in, also be provided with a pilot and seat thereof, an ejection mechanism and an arrestment mechanism; Described ejection mechanism and arrestment mechanism are fixed on the base, described base be the cylinder that an opening makes progress, its top also is provided with a side stand that is used for fixing described arrestment mechanism; Be equipped with one guide pillar in the cylinder of described base, the upper surface of this guide pillar also is provided with a circle flange, on the bottom is fixed at the bottom of the described base cylinder; Also be arranged with a spring on the described guide pillar, the upper end of spring is blocked by described guide pillar flange, and the lower end is blocked by the bottom of base cylinder; Described pilot is fixing, and this seat is a cylinder that Open Side Down on the seat, and described guide pillar can insert in this seat cylinder, and the barrel dliameter of this seat cylinder is less than the barrel dliameter of base cylinder; Also be provided with a circle flange on its lower surface; On the described guide pillar, spring top also is arranged with a packing ring, the diameter of this packing ring is greater than the barrel dliameter of described seat cylinder; The slide block that described arrestment mechanism is provided with an expanding-contracting action mechanism and is connected with this mechanism, this slide block is under battery, and it stretches out and can block described seat cylinder flange under the state, and can leave described seat cylinder flange under the contraction state;
Under the battery, described guide pillar is built in described base cylinder and the seat cylinder, described packing ring and pressuring spring are oppressed in seat cylinder lower surface, also accumulation of energy in the described base cylinder of indentation, the seat cylinder tips upside down on the described base cylinder, and the flange on its lower surface is blocked by the slide block that described arrestment mechanism stretches out;
During emission, described arrestment mechanism is controlled its slide block retraction, away from described seat cylinder lower surface flange, this moment, spring released energy, packing ring promotes the lower surface of seat cylinder and then promotes seat together with the pilot who is arranged on this seat, upwards launches, and leaves aircraft.
The housing top of described aircraft also is installed with a preceding skylight, and this rear portion, preceding skylight is hinged with one back skylight by a jointed shaft; Skylight, described back can be around the folding up and down of the axle center of its jointed shaft.In the flight course, after back skylight was flicked by external force, its power of closing came from air drag and earth attraction.
Described arrestment mechanism is an electromagnetism actuating mechanism, and it comprises a magnetic coil, and is arranged on the iron core push rod at this coil middle part, on the outside end face of this push rod, is fixed with described slide block; Also be arranged with a slide block back-moving spring on this push rod.
Described arrestment mechanism can also be a motor tooth punch-out equipment structure, and it comprises a motor, and a tooth case that is connected with this motor, and it is elastic that described tooth case can drive a connected push rod; On the outside end face of this push rod, be fixed with described slide block; Also be arranged with a slide block back-moving spring on this push rod.
On the described seat, also be provided with a parachute and open mechanism.
Described guide pillar bottom, be fixed on described base tube by screw at the bottom of.
Described arrestment mechanism is by screw, and its bottom is fixed on the described side stand.
The course of work of the present utility model is such: under the battery, described guide pillar is built in described base cylinder and the seat cylinder, described packing ring and pressuring spring are oppressed in seat cylinder lower surface, also accumulation of energy in the described base cylinder of indentation, the seat cylinder tips upside down on the described base cylinder, and the flange on its lower surface is blocked by the slide block that described arrestment mechanism stretches out; During emission, described arrestment mechanism is controlled its slide block retraction, away from described seat cylinder lower surface flange, this moment, spring released energy, packing ring promotes the lower surface of seat cylinder and then promotes seat together with the pilot who is arranged on this seat, upwards launch, push skylight, described back open, leave aircraft; Afterwards, back skylight automatically resets under air drag and terrestrial gravitation effect.
Described seat and pilot open parachute in dropping process, be retracted until landing; After the withdrawal, can by hand it be reset on the base in the cabin, and the slide block that is braked mechanism blocks, wait for the new operation of launching.So can use repeatedly.
Advantage of the present utility model is: because the utility model is by being set together seat and pilot, provide through the spring ejection mechanism and to launch power, the remote-controlled driving arrestment mechanism action of operator, realize pilot's parachute jumping action, the pilot is ejected from aircraft top, consistent with pilot in the reality escape design of parachuting, strengthened the interest of toy aircraft; The utility model also aircraft driving cabin on happy former and later two skylights are set, preceding skylight is fixed on the aircraft; Back skylight connects by the preceding skylight of hinge arrangement, and it can be around the folding up and down of the axle center of hinge axis.In the flight course, after back skylight is flicked by external force, ingeniously use air drag and terrestrial gravitation is closed the skylight.
The utility model is simple in structure, compact, volume is little, in light weight, safe and reliable, can realize highly difficult send action, reliable in action is convenient to make, assembling and using, and can be widely used on the various toy aircraft.
Below in conjunction with accompanying drawing the utility model is further described.
Description of drawings
Fig. 1 is the sectional structure schematic diagram of the utility model embodiment 1;
Fig. 2 is the three-dimensional assembly structure schematic diagram of Fig. 1.
The specific embodiment
Embodiment 1, and a kind of pilot ejection parachute device of toy aircraft is provided, and is the pilot ejection parachute device of remote-control toy aircraft.
With reference to Fig. 1 and Fig. 2, a kind of pilot ejection parachute device of toy airplane comprises toy airplane, described toy aircraft driving cabin in, also be provided with a pilot and seat 8, an ejection mechanism and an arrestment mechanism; Described ejection mechanism and arrestment mechanism are fixed on the base 4, described base 4 be the cylinder that an opening makes progress, its top also is provided with a side stand 12 that is used for fixing described arrestment mechanism; Be equipped with one guide pillar 7 in the cylinder of described base 4, the upper surface of this guide pillar 7 also is provided with a circle flange, on the bottom is fixed at the bottom of described base 4 cylinders; Also be arranged with a spring 5 on the described guide pillar 7, the upper end of spring 5 is blocked by described guide pillar 7 flanges, and the lower end is blocked by the bottom of base 4 cylinders; Described pilot is fixed on the seat 8, and this seat 8 is the cylinders that Open Side Down, and described guide pillar 7 can insert in these seat 8 cylinders, and the barrel dliameter of these seat 8 cylinders also is provided with a circle flange less than the barrel dliameter of base 4 cylinders on its lower surface; On the described guide pillar 7, spring 5 tops also are arranged with a packing ring 6, the diameter of this packing ring 6 is greater than the barrel dliameter of described seat 4 cylinders; The slide block 2 that described arrestment mechanism is provided with an expanding-contracting action mechanism 1 and is connected with this mechanism, this slide block 2 is under battery, and it stretches out and can block described seat 8 cylinder flanges under the state, and can leave described seat 8 cylinder flanges under the contraction state;
Under the battery, described guide pillar 7 is built in described base 4 cylinders and seat 8 cylinders, described packing ring 6 and pressuring spring 5 are oppressed in seat 4 cylinder lower surfaces, also accumulation of energy in described base 4 cylinders of indentation, seat 8 cylinders tip upside down on described base 4 cylinders, and the flange on its lower surface is blocked by the slide block 2 that described arrestment mechanism stretches out;
During emission, described arrestment mechanism is controlled its slide block 2 retractions, away from described seat 8 cylinder lower surface flanges, this moment, spring 5 released energy, packing ring 6 promotes the lower surface of seat 8 cylinders and then promotes seat 4 together with the pilot who is arranged on this seat 8, upwards launches, and leaves aircraft.
The housing top of described aircraft also is provided with a preceding skylight 10, and these 10 rear portions, preceding skylight are hinged with one back skylight 9 by a jointed shaft 11; The folding up and down of skylight 9, described back.After back skylight 9 was flicked by seat 8, it was closed under the effect of air drag and earth attraction automatically.
In the present embodiment, what described arrestment mechanism adopted is an electromagnetism actuating mechanism 1, and it comprises a magnetic coil, and is arranged on the iron core push rod 14 at this coil middle part, on the outside end face of this push rod 14, is fixed with described slide block 2; Also be arranged with a slide block back-moving spring 3 on this push rod 14.
On the described seat 8, also be provided with a parachute and open mechanism 13.
Described guide pillar 7 bottoms, be fixed on 4 of described bases by screw at the bottom of.
Described arrestment mechanism is by screw, and its bottom is fixed on the described side stand 12.
Embodiment 2, a kind of pilot ejection parachute device of toy aircraft is provided, its basic structure is identical with embodiment 1, its difference is, what described arrestment mechanism adopted is a motor tooth punch-out equipment structure, it comprises a motor, and a tooth case that is connected with this motor, and it is elastic that described tooth case can drive a connected push rod; On the outside end face of this push rod, be fixed with described slide block; Also be arranged with a slide block back-moving spring on this push rod.
As the described identical or approximate construction of the utility model the foregoing description, the pilot ejection parachute device of resulting other toy aircraft is all within the utility model protection domain.
Claims (7)
1, a kind of pilot ejection parachute device of toy aircraft comprises toy aircraft, it is characterized in that: in the driving cabin of described toy aircraft, also be provided with a pilot and seat thereof, an ejection mechanism and an arrestment mechanism; Described ejection mechanism and arrestment mechanism are fixed on the base, described base be the cylinder that an opening makes progress, its top also is provided with a side stand that is used for fixing described arrestment mechanism; Be equipped with one guide pillar in the cylinder of described base, the upper surface of this guide pillar also is provided with a circle flange, on the bottom is fixed at the bottom of the described base cylinder; Also be arranged with a spring on the described guide pillar, the upper end of spring is blocked by described guide pillar flange, and the lower end is blocked by the bottom of base cylinder; Described pilot is fixing, and this seat is a cylinder that Open Side Down on the seat, and described guide pillar can insert in this seat cylinder, and the barrel dliameter of this seat cylinder is less than the barrel dliameter of base cylinder; Also be provided with a circle flange on its lower surface; On the described guide pillar, spring top also is arranged with a packing ring, the diameter of this packing ring is greater than the barrel dliameter of described seat cylinder; The slide block that described arrestment mechanism is provided with an expanding-contracting action mechanism and is connected with this mechanism, this slide block is under battery, and it stretches out and can block described seat cylinder flange under the state, and can leave described seat cylinder flange under the contraction state;
Under the battery, described guide pillar is built in described base cylinder and the seat cylinder, described packing ring and pressuring spring are oppressed in seat cylinder lower surface, also accumulation of energy in the described base cylinder of indentation, the seat cylinder tips upside down on the described base cylinder, and the flange on its lower surface is blocked by the slide block that described arrestment mechanism stretches out;
During emission, described arrestment mechanism is controlled its slide block retraction, away from described seat cylinder lower surface flange, this moment, spring released energy, packing ring promotes the lower surface of seat cylinder and then promotes seat together with the pilot who is arranged on this seat, upwards launches, and leaves aircraft.
According to the pilot ejection parachute device of the described toy aircraft of claim 1, it is characterized in that 2, the housing top of described aircraft also is installed with a preceding skylight, this rear portion, preceding skylight is hinged with skylight, a back by a jointed shaft; Skylight, described back can be around the folding up and down of the axle center of its jointed shaft.
According to the pilot ejection parachute device of claim 1 or 2 described toy aircraft, it is characterized in that 3, described arrestment mechanism is an electromagnetism actuating mechanism, it comprises a magnetic coil, and be arranged on the iron core push rod at this coil middle part, on the outside end face of this push rod, be fixed with described slide block; Also be arranged with a slide block back-moving spring on this push rod.
4, according to the pilot ejection parachute device of claim 1 or 2 described toy aircraft, it is characterized in that, described arrestment mechanism can also be a motor tooth punch-out equipment structure, it comprises a motor, and a tooth case that is connected with this motor, it is elastic that described tooth case can drive connected push rod; On the outside end face of this push rod, be fixed with described slide block; Also be arranged with a slide block back-moving spring on this push rod.
5, according to the pilot ejection parachute device of claim 1 or 2 described toy aircraft, it is characterized in that, on the described seat, also be provided with a parachute and open mechanism.
6, according to the pilot ejection parachute device of claim 1 or 2 described toy aircraft, it is characterized in that, described guide pillar bottom, be fixed on described base tube by screw at the bottom of.
According to the pilot ejection parachute device of claim 1 or 2 described toy aircraft, it is characterized in that 7, described arrestment mechanism is by screw, its bottom is fixed on the described side stand.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620057467 CN2882742Y (en) | 2006-04-10 | 2006-04-10 | Pilot ejection parachuting device of toy aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620057467 CN2882742Y (en) | 2006-04-10 | 2006-04-10 | Pilot ejection parachuting device of toy aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2882742Y true CN2882742Y (en) | 2007-03-28 |
Family
ID=37955803
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620057467 Expired - Fee Related CN2882742Y (en) | 2006-04-10 | 2006-04-10 | Pilot ejection parachuting device of toy aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2882742Y (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105034886A (en) * | 2015-08-31 | 2015-11-11 | 唐慧华 | Multifunctional seat with alarm button |
| CN105109443A (en) * | 2015-08-31 | 2015-12-02 | 唐慧华 | Multi-point array arrangement and control tilting preventing device |
| CN105235621A (en) * | 2015-09-01 | 2016-01-13 | 高海 | Internal mechanism avoiding non-interference system |
| CN105235622A (en) * | 2015-09-01 | 2016-01-13 | 高海 | Top cover lift-pull space releasing mechanism |
| CN108992944A (en) * | 2018-07-03 | 2018-12-14 | 李芳� | A kind of town squares children entertaining seat |
-
2006
- 2006-04-10 CN CN 200620057467 patent/CN2882742Y/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105034886A (en) * | 2015-08-31 | 2015-11-11 | 唐慧华 | Multifunctional seat with alarm button |
| CN105109443A (en) * | 2015-08-31 | 2015-12-02 | 唐慧华 | Multi-point array arrangement and control tilting preventing device |
| CN105235621A (en) * | 2015-09-01 | 2016-01-13 | 高海 | Internal mechanism avoiding non-interference system |
| CN105235622A (en) * | 2015-09-01 | 2016-01-13 | 高海 | Top cover lift-pull space releasing mechanism |
| CN108992944A (en) * | 2018-07-03 | 2018-12-14 | 李芳� | A kind of town squares children entertaining seat |
| CN108992944B (en) * | 2018-07-03 | 2020-07-31 | 佛山市祥聚座椅制造有限公司 | Interesting seat for children in municipal square |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Longchang Toy Co., Ltd., Dongguan City Assignor: Liang Zhongming Contract fulfillment period: 2009.3.20 to 2014.3.19 Contract record no.: 2009990000477 Denomination of utility model: Pilot ejection parachuting device of toy aircraft Granted publication date: 20070328 License type: Exclusive license Record date: 20090513 |
|
| LIC | Patent licence contract for exploitation submitted for record |
Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2009.3.20 TO 2014.3.19; CHANGE OF CONTRACT Name of requester: DONGGUAN LONGCHANG TOY CO., LTD. Effective date: 20090513 |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20070328 Termination date: 20110410 |