CN205140268U - Can realize aircraft system of flight experience - Google Patents
Can realize aircraft system of flight experience Download PDFInfo
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- CN205140268U CN205140268U CN201520492316.7U CN201520492316U CN205140268U CN 205140268 U CN205140268 U CN 205140268U CN 201520492316 U CN201520492316 U CN 201520492316U CN 205140268 U CN205140268 U CN 205140268U
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Abstract
The utility model provides a can realize aircraft system of flight experience, includes the aircraft, and the aircraft includes cockpit, fuselage and all -wing aircraft, and the fuselage is preceding to be equipped with the fan, and the fan is equipped with the blade, is equipped with the dead lever between fan and the fuselage, is equipped with spacing rope between fuselage front end and the dead lever, and the fuselage is equipped with the limit for height rope with the ground interfacial, and the blade rotational energy of fan drives all -wing aircraft work for the fuselage suspension that can make progress. The utility model discloses can realize the training of premature pilot and provide flight experiencing etc. It has characteristics such as with low costs, factor of safety height. The utility model discloses a blade of fan rotates the all -wing aircraft work that drives for the fuselage suspension that can make progress, a real flight is experienced in can be used to the training of premature pilot and providing people's life, and its cost of manufacture is low, and the security performance is high, has higher spreading value.
Description
Technical field
The utility model relates to vehicle technology field, is related specifically to a kind of aircraft that can carry out flight experience and early stage pilot training.
Background technology
Aircraft is special aircraft due to it, and common people have no chance to be sitting in familiarization flight on aircraft.Domestic have many airhogs to adopt the baby planes such as autogiro to realize the experience of flight at present, and it needs superb airmanship and flight cost, and most people does not all have this chance to realize flight experience.In addition, because the manufacturing cost of aircraft is very high, pilot's training cost is high, and comparatively speaking, to beginner and experiencer, its safety coefficient is low.Therefore develop a kind of aircraft, early stage pilot training can be realized and in providing people to live, a real flight experience is very important.
Utility model content
The utility model, for above-mentioned prior art Problems existing, provides a kind of aircraft system, can realize early stage pilot training and provide flight experience etc., has that cost is low, safety coefficient high.
The technical scheme that the technical matters that the utility model solves adopts is:
A kind of aircraft system that can realize flight experience, comprise aircraft, aircraft comprises driving cabin, fuselage and all-wing aircraft, it is characterized in that being provided with blower fan before fuselage, blower fan is provided with blade, is provided with fixed bar between blower fan and fuselage, limit rope is provided with between front fuselage and fixed bar, be provided with limit for height rope between fuselage and ground, the blade rotation of blower fan can drive all-wing aircraft work, and fuselage can upwards be suspended.
All-wing aircraft is the parts that aircraft produces lift, and the utility model drives all-wing aircraft work by the blade rotation of blower fan, and fuselage can upwards be suspended, and may be used for early stage pilot's training and a real flight experience in providing people to live.Fuselage is fixed on fixed bar by limit rope, ensures that aircraft is out of hand, moves backward, be provided with limit for height rope between fuselage and ground, set the spacing height taken off, ensure its safety.
Flight theory is produce speed per hour by separate unit or multiple stage high-power blower to exceed certain wind speed, according to bernoulli law: air-flow produces pressure differential by the upper and lower surface of wing and forms lift.Therefore unpowered manned aircraft is in static state, as long as relative wind reaches suitable speed, and just can fly up under the control of pilot, rest on certain altitude, air quantity can control height, i.e. free landing flight in given airflow range, it drops to ground can grease it in.This flight experience aircraft combination unit, be adapted at most indoor operation, because indoor flight is not just subject to extraneous climate effect, this covering device is mainly used for early stage pilot's training and a real flight experience in providing people to live, and security performance is very high.
During concrete enforcement, aircraft is autogiro, delta-winged aircraft or fixed wing aircraft.Because above-mentioned three kinds of aircrafts are all lightweight aircraft, by test, autogiro, delta-winged aircraft or fixed wing aircraft are most appropriate to the aircraft as the utility model.
During concrete enforcement, autogiro comprises undercarriage, empennage, and all-wing aircraft is rotor, and undercarriage is positioned at below fuselage, and empennage is located at afterbody.The blade rotation of blower fan drives rotor rotational, and autogiro can upwards be suspended.
During concrete enforcement, the underbelly of delta-winged aircraft is undercarriage, and undercarriage is that triangular shape is distributed with three wheels, and all-wing aircraft is delta wing.The wing of delta-winged aircraft has that angle of sweep is large, aspect ratio is little and the feature such as relative thickness is little.Major advantage is that wing is lightweight, good rigidly, volume are large.
During concrete enforcement, fixed wing aircraft comprises the horizontal tail wing and undercarriage, and undercarriage is positioned at below fuselage, and all-wing aircraft is the left and right wing being located at fuselage both sides, and the horizontal tail wing is located at afterbody.The blade rotation of blower fan drives left and right wing, and autogiro can upwards be suspended.
During concrete enforcement, above-mentioned aircraft is provided with operating control, and operating control can control lifting and the flight angle of aircraft.
Operating control is normally indulged by operation behaviour bar, and aircraft handling person can realize aircraft lifting and landing and flight angle by behaviour's bar is vertical.As autogiro, driver can operate bar vertical control rotor etc., realizes aircraft lifting and landing and flight angle.As delta-winged aircraft, driver can operate bar vertical control delta wing etc., realizes aircraft lifting and landing and flight angle.As fixed wing aircraft, driver can operate bar vertical control the horizontal tail wing and aileron etc., realizes aircraft lifting and landing and flight angle.Aircraft handling person realizes flight experience further by operating control, for pilot's training and in providing people to live real flight experience control its lifting, its security performance is very high.
Because propulsion system of the present utility model are blower fan, therefore, aircraft can save some propulsion system such as generator, to reduce manufacturing cost, meanwhile, can weight reduction, be conducive to the power reducing blower fan, reduce cost further, improve security performance.The functions such as the utility model can integrate that science and technology of aviation is universal, aviation practice teaching and airline travel, for fan provides good flight experience.
The beneficial effects of the utility model are: the utility model drives all-wing aircraft work by the blade rotation of blower fan, fuselage can upwards be suspended, can be used for early stage pilot's training and a real flight experience in providing people to live, its cost of manufacture is low, security performance is high, has higher promotional value.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, utility model is further illustrated.
Fig. 1 is the structural representation of the utility model embodiment one;
Fig. 2 is the structural representation of the utility model embodiment two;
Fig. 3 is the structural representation of the utility model embodiment three.
In figure: 1, blower fan 2, blade 3, fixed bar 4, limit rope 5, limit for height rope 6, driving cabin I7, rotor 8, empennage 9, undercarriage I10, fuselage I11, driving cabin II12, fuselage II13, undercarriage II14, delta wing 15, fuselage III16, the horizontal tail wing 17, driving cabin III18, undercarriage III19, the horizontal tail wing.
Embodiment
Embodiment one:
In Fig. 1, aircraft take autogiro as example, a kind of aircraft system that can realize flight experience, autogiro comprises driving cabin I6, undercarriage I9, empennage 8, fuselage I10 and rotor, undercarriage is positioned at below fuselage I10, empennage 8 is located at fuselage I10 afterbody, operating control is provided with in driving cabin I6, operating control comprises behaviour's bar to be indulged, driver can operate bar vertical control rotor 8, realize aircraft lifting and landing and flight angle, blower fan 1 is provided with before fuselage I10, blower fan 1 is provided with blade 2, fixed bar 3 is provided with between blower fan 1 and fuselage I10, limit rope 4 is provided with between fuselage I10 front end and fixed bar, limit for height rope 5 is provided with between fuselage I10 and ground, blade 2 rotational of blower fan 1 drives rotor 7 to work, fuselage I10 can upwards be suspended.
Embodiment two:
In Fig. 2, aircraft take delta-winged aircraft as example, a kind of aircraft system that can realize flight experience, delta-winged aircraft comprises driving cabin II11, undercarriage II13, fuselage II12 and delta wing 14, fuselage II12 bottom is undercarriage II13, undercarriage II13 is that triangular shape is distributed with three wheels, operating control is provided with in driving cabin II11, operating control comprises behaviour's bar to be indulged, driver can operate bar vertical control delta wing 14, realize aircraft lifting and landing and flight angle, blower fan 1 is provided with before fuselage II12, blower fan 1 is provided with blade 2, fixed bar 3 is provided with between blower fan 1 and fuselage II12, limit rope 4 is provided with between fuselage II12 front end and fixed bar, limit for height rope 5 is provided with between fuselage II12 and ground, blade 2 rotational of blower fan 1 drives delta wing 14 to work, fuselage II12 can upwards be suspended.The wing of delta-winged aircraft has that angle of sweep is large, aspect ratio is little and the feature such as relative thickness is little.Major advantage is that wing is lightweight, good rigidly, volume are large.
Embodiment three:
In Fig. 3, aircraft take fixed wing aircraft as example, a kind of aircraft system that can realize flight experience, fixed wing aircraft comprises driving cabin III17, undercarriage III18, the horizontal tail wing 19, the left and right wing 16 of fuselage III15 and fuselage III15 both sides, undercarriage is positioned at below fuselage III15, left and right wing 16 is provided with aileron, the horizontal tail wing 16 is located at fuselage III15 afterbody, operating control is provided with in driving cabin III17, operating control comprises behaviour's bar to be indulged, driver can operate the bar vertical control horizontal tail wing 19 and aileron, realize aircraft lifting and landing and flight angle, blower fan 1 is provided with before fuselage III15, blower fan 1 is provided with blade 2, fixed bar 3 is provided with between blower fan 1 and fuselage III15, limit rope 4 is provided with between fuselage III15 front end and fixed bar, limit for height rope 5 is provided with between fuselage III15 and ground, blade 2 rotational of blower fan 1 drives left and right wing 16 to work, fuselage III15 can upwards be suspended.
All-wing aircraft is the parts that aircraft produces lift, and the utility model drives all-wing aircraft work by the blade rotation of blower fan, and fuselage can upwards be suspended, and may be used for early stage pilot's training and a real flight experience in providing people to live.Be provided with fixed bar between blower fan and fuselage, ensure that aircraft is out of hand, move backward, between fuselage and ground, be provided with limit for height rope, set the spacing height taken off, ensure its safety.The manned aircraft of these three kinds of embodiments can be carried out spacing between aircraft and ground, and in such as limit for height 3 meters, aircraft also can ensure personal security when fan trouble under freely falling body, and safeguard one is software energy-absorbing seat, and two is efficient damping undercarriages.The utility model flight experience aircraft combination unit, is adapted at indoor operation most, because indoor flight is not just subject to extraneous climate effect, this covering device is mainly used for early stage pilot's training and a real flight experience in providing people to live.
Because propulsion system of the present utility model are blower fan 1, therefore, the aircraft of three kinds of embodiments can save some propulsion system such as generator, to reduce manufacturing cost, meanwhile, can weight reduction, be conducive to the power reducing blower fan 1, reduce cost further, improve security performance.
The blower fan 1 of above three embodiments produces the wind speed that speed per hour exceedes 60 kilometers per hour, also can adopt multiple stage high-power blower.Aircraft is in static state, as long as relative wind reaches suitable speed, and just can fly up under the control of pilot, rest on certain altitude, i.e. free landing flight in given airflow range.
Finally, it should be pointed out that above embodiment is only the more representational example of the utility model.Obviously, the utility model is not limited to above-described embodiment, can also have many distortion.Every above embodiment is done according to technical spirit of the present utility model any simple modification, equivalent variations and modification, all should think and belong to protection domain of the present utility model.
Claims (6)
1. one kind can realize the aircraft system of flight experience, comprise aircraft, aircraft comprises driving cabin, fuselage and all-wing aircraft, it is characterized in that being provided with blower fan before fuselage, blower fan is provided with blade, is provided with fixed bar between blower fan and fuselage, limit rope is provided with between front fuselage and fixed bar, be provided with limit for height rope between fuselage and ground, the blade rotation of blower fan can drive all-wing aircraft work, and fuselage can upwards be suspended.
2. a kind of aircraft system that can realize flight experience according to claim 1, is characterized in that aircraft is autogiro, delta-winged aircraft or fixed wing aircraft.
3. a kind of aircraft system that can realize flight experience according to claim 2, is characterized in that autogiro comprises undercarriage, empennage, and all-wing aircraft is rotor, and undercarriage is positioned at below fuselage, and empennage is located at afterbody.
4. a kind of aircraft system that can realize flight experience according to claim 2, is characterized in that the underbelly of delta-winged aircraft is undercarriage, and undercarriage is that triangular shape is distributed with three wheels, and all-wing aircraft is delta wing.
5. a kind of aircraft system that can realize flight experience according to claim 2, it is characterized in that fixed wing aircraft comprises the horizontal tail wing and undercarriage, undercarriage is positioned at below fuselage, and all-wing aircraft is the left and right wing being located at fuselage both sides, and the horizontal tail wing is located at afterbody.
6. a kind of aircraft system that can realize flight experience according to the arbitrary claim in claim 1 to 5, is characterized in that above-mentioned aircraft is provided with operating control, and operating control can control landing and the flight angle of aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520492316.7U CN205140268U (en) | 2015-07-04 | 2015-07-04 | Can realize aircraft system of flight experience |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520492316.7U CN205140268U (en) | 2015-07-04 | 2015-07-04 | Can realize aircraft system of flight experience |
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| CN205140268U true CN205140268U (en) | 2016-04-06 |
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| CN201520492316.7U Active CN205140268U (en) | 2015-07-04 | 2015-07-04 | Can realize aircraft system of flight experience |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104992586A (en) * | 2015-07-04 | 2015-10-21 | 徐斌 | Airplane system capable of realizing flight experience |
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2015
- 2015-07-04 CN CN201520492316.7U patent/CN205140268U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104992586A (en) * | 2015-07-04 | 2015-10-21 | 徐斌 | Airplane system capable of realizing flight experience |
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