阅读说明：本技术 带气囊伞帽的旋翼机 (Rotorcraft with air bag umbrella cap ) 是由 于建国 于 2021-03-02 设计创作，主要内容包括：本发明涉及一种新型旋翼机,包括机身和安装在所述机身的顶部的旋翼,所述旋翼的正上方安装有气囊伞,所述气囊伞是伞状撑开的气囊,所述气囊内充填有密度小于空气的气体,所述气囊伞通过支架安装在所述机身上,所述支架相对所述机身角度可调,所述机身采用内外双层结构,内外层之间分散设有若干抗震弹簧,所述抗震弹簧的两端分别抵在内层的外表面与外层的内表面上,内层和外层之前的其余空腔采用泡沫塑料填充。本发明能实现垂直升降和悬停,即使在完全失去动力的情况下也能够以自由降落方式安全落地,飞行姿态稳定性和安全性显著提高。(The invention relates to a novel gyroplane which comprises a fuselage and a rotor wing arranged at the top of the fuselage, wherein an air bag umbrella is arranged right above the rotor wing, the air bag umbrella is an umbrella-shaped expanded air bag, gas with the density smaller than that of air is filled in the air bag, the air bag umbrella is arranged on the fuselage through a support, the angle of the support relative to the fuselage is adjustable, the fuselage adopts an inner-outer double-layer structure, a plurality of anti-seismic springs are dispersedly arranged between the inner layer and the outer layer, two ends of each anti-seismic spring respectively abut against the outer surface of the inner layer and the inner surface of the outer layer, and the rest cavities in front of the inner layer and the outer layer are filled. The invention can realize vertical lifting and hovering, can safely land in a free-fall mode even under the condition of completely losing power, and obviously improves the stability and the safety of the flight attitude.)

1. The utility model provides a take novel gyroplane of gasbag umbrella cap, includes the fuselage and installs the rotor at the top of fuselage, its characterized in that: an air bag umbrella is arranged above the rotor wing, the air bag umbrella is an umbrella-shaped opened air bag, and gas with density smaller than that of air is filled in the air bag.

2. A novel rotorcraft with an air bag parachute cap as claimed in claim 1, wherein: the aircraft is characterized in that a bracket is further arranged, the edge of the airbag umbrella is fixed on the bracket to keep the opening state, the bracket is installed on the aircraft body, and the rotor wing is completely positioned in the shade range of the umbrella-shaped object in the front-back direction.

3. A novel rotorcraft with an air bag canopy as claimed in claim 2, wherein: the gasbag umbrella is bilateral symmetry structure, the left and right sides edge of support is equipped with left wing board and the right wing board that the horizontal direction extends left and right respectively, the rotor is in completely in the left and right direction the shade within range of gasbag umbrella, left wing board and right wing board.

4. A novel rotorcraft with an air bag canopy as claimed in claim 2 or 3, wherein: in the unfolded state, the edge of the air bag umbrella is circular or oval with the front-back length larger than the left-right width.

5. A novel rotorcraft with an air bag parachute cap as claimed in claim 4, wherein: the outer surface of the umbrella-shaped object is a streamline smooth curved surface, the streamline gradient of the surface close to the front is relatively slow, the streamline gradient of the surface close to the rear is relatively steep, and the whole umbrella-shaped object is in a shape of a peak cap.

6. A novel rotorcraft with an air bag parachute cap as claimed in claim 1, wherein: the air bag is provided with a plurality of air bag units, each air bag unit is sealed, and each air bag unit is provided with an air inlet with a reverse valve.

7. A novel rotorcraft with an air bag parachute cap as claimed in claim 1, wherein: still be equipped with engine and clutch, the rotor passes through the clutch with the engine is connected.

8. A novel rotorcraft with an air bag parachute cap as claimed in claim 1, wherein: the circular area corresponding to the rotor wing does not exceed the projection area of the air bag umbrella on the corresponding plane vertical to the axis of the rotor wing.

9. A novel rotorcraft with air bag umbrellas as defined in claims 1, 2, 3, 4, 5, 6, 7, or 8, wherein: the fuselage adopts inside and outside bilayer structure, is the cabin within the inlayer, and the dispersion is equipped with a plurality of antidetonation springs between the inlayer, every the both ends of antidetonation spring are supported respectively on the surface of inlayer and outer internal surface, and all the other cavities before inlayer and the skin adopt foamed plastic to fill.

10. A novel rotorcraft with an air bag canopy as claimed in claim 9, wherein: the angle of the bracket relative to the machine body is adjustable.

Technical Field

The present invention relates to a rotorcraft, and more particularly, to a rotorcraft that can be vertically lifted and safely landed in a free-fall manner even when power is completely lost, and is applicable to a manned aircraft.

Background

The power for the rotorcraft to ascend is mainly generated by blowing a rotor wing to rotate by front airflow in the flying process, so that the rotorcraft generally needs a longer running distance to slowly ascend when taking off, namely cannot vertically ascend. Similarly, it cannot descend vertically and hover in the air. Moreover, when the gyroplane flies near the ground or is in the process of lifting or descending, the lift force generated by the rotation of the rotor wing is limited and unstable, so that the attitude stability of the gyroplane is poor, and the safety of the gyroplane is directly influenced.

Disclosure of Invention

The invention aims to provide a rotorcraft with an airbag umbrella cap, which can realize vertical lifting and hovering and can safely land in a free-fall mode under the condition of completely losing power.

The main technical scheme of the invention is as follows:

the utility model provides a take gyroplane of gasbag umbrella cap, includes the fuselage and installs the rotor at the top of fuselage, the gasbag umbrella is installed to the top of rotor, the gasbag umbrella is the gasbag that the umbelliform propped open, be filled with the gas that density is less than the air in the gasbag.

The gyroplane with the airbag umbrella cap is further provided with a support, the edge of the airbag umbrella is fixed on the support to keep the opening state, the support is installed on the airframe, and the rotor wing is preferably completely located in the shade range of the umbrella-shaped object in the front-back direction.

The gasbag umbrella can be bilateral symmetry structure, the local edge in the left and right sides of support is fixed respectively and is equipped with left wing board and the right wing board that the horizontal direction extends left and right, the rotor is preferably in completely in the left and right sides orientation the shade within range of gasbag umbrella, left wing board and right wing board.

In the unfolded state, the edge of the airbag umbrella can be circular or approximately elliptical with the front-back length larger than the left-right width.

The outer surface of the air bag umbrella is preferably a streamline smooth curved surface, the streamline gradient of the surface close to the front is gentle, the streamline gradient of the surface close to the rear is steep, and the whole air bag umbrella is in a shape of a peaked cap.

The air bag is preferably of unitary construction provided with a plurality of air bag units, each air bag unit being individually sealed and each air bag unit being individually provided with an air inlet having a reverse valve.

The gas filled in the air bag is preferably helium.

The gyroplane with the airbag umbrella cap is also preferably provided with an engine and a clutch, and the rotor is connected with the engine through the clutch.

The circular area corresponding to the rotation of the rotor wing does not exceed the projection area of the airbag umbrella on the corresponding plane vertical to the axis of the rotor wing.

The fuselage preferably adopts inside and outside bilayer structure, is the cabin inside the inlayer, can disperse between the inlayer and the ectonexine to be equipped with a plurality of antidetonation springs, the both ends of antidetonation spring are supported respectively on the surface of inlayer and outer internal surface, and all the other cavities before inlayer and the skin adopt foamed plastic to fill.

The angle of the support relative to the fuselage is preferably adjustable.

The invention has the beneficial effects that:

the rotor wing can keep a vertical posture all the time by adopting the lifting force provided by the air bag umbrella, and then the power rotor wing is matched with the air flow to enable the air bag umbrella to obtain upward power, and the higher the rotating speed of the rotor wing is, the larger the upward power obtained by the air bag umbrella is, so that the rotor wing can take off and land vertically and hover. The requirements for taking off and landing sites are greatly reduced, the power is saved obviously, the range is prolonged, and the application field of the gyroplane is further expanded.

Utilize the clutch will the rotor is connected with the engine, let the rotor initiatively rotate, it makes the gasbag umbrella obtain ascending power to drive the air current, the rotor rotational speed is higher, ascending power that the gasbag umbrella obtained is just big more, make the parachute effect especially obvious, even on the gyroplane is close to the height on ground, the gasbag umbrella also can provide enough, stable lift, this lift is enough to keep the balance and the stability of fuselage gesture, consequently, can solve current gyroplane well and be close to the ground (including flight and lift-off and landing process) fuselage gesture shakiness or even have the problem of the risk of turning on one's side, the stability and the security of gyroplane have greatly been promoted.

Because the air bag parachute can always provide upward power and is not influenced by the state of the rotor wing, even if no power is available, the gyroplane can slowly descend in a free-falling mode and finally safely land, and therefore the safety is obviously improved.

Due to the adoption of the inner container type machine body, the anti-seismic performance is remarkably improved, the service life of the machine body is long, the riding experience is good, and the safety is also improved from the other aspect.

Drawings

FIG. 1 is a schematic block diagram of one embodiment of the present invention;

FIG. 2 is a top view of the embodiment of FIG. 1 (see-through effect);

fig. 3 is a rear view in elevation of the embodiment of fig. 1.

Reference numerals: 2. an air bag umbrella; 2-1, an airbag unit; 3. a support; 4. a left wing panel and a right wing panel; 5. a rotating shaft; 6. a rotor; 10. a power fan; 11. a tail wing; 12. a landing gear; 13. a cabin door; 14. an anti-seismic spring; 15. a foam.

Detailed Description

The invention discloses a novel unbreakable gyroplane, which comprises a gyroplane body and a rotor wing 6 arranged at the top of the gyroplane body, wherein an air bag umbrella 2 is arranged above the rotor wing, the air bag umbrella is an umbrella-shaped expanded air bag, and gas with density smaller than that of air, such as helium, is filled in the air bag. The term "umbrella shape" as used herein refers to a state in which the air bag is projected so as to cover the rotor in a position as extended as possible, and is not intended to limit the shape of the air bag, and the air bag umbrella may have any shape. The air bag parachute can standardize the posture of the gyroplane, so that the gyroplane can keep a vertical posture when losing power or falling on the water surface. According to the structural characteristics, the invention can also be called a 'crash-proof gyroplane with an airbag umbrella cap'.

In addition, the circular area corresponding to the rotating rotor wing preferably does not exceed the projection area of the air bag umbrella on the corresponding plane vertical to the axial lead of the rotor wing, so that the air flow driven by the rotating rotor wing almost completely flows to the air bag umbrella and serves as the source power for supporting the air bag umbrella, and the energy utilization rate is maximized.

Because the air bag umbrella can provide upward power which is not influenced by whether the rotor wings stop rotating or not as long as the air bag umbrella is in a normal state, the upward power provided by the air bag umbrella in the vertical direction can counteract partial gravity of the rotorcraft, so that the vertical posture of the rotorcraft can be standardized, and the rotorcraft can hover in the air can be facilitated.

The rotorcraft with the airbag umbrella caps can also be provided with an engine and a clutch, and when needed, the rotor is connected with the engine through the clutch, so that the rotor becomes a rotor with power. The engine provides a power source for the rotorcraft at a particular stage or process that causes the rotor to temporarily actively rotate. The power-driven rotor wing is mainly used for assisting in vertical take-off and landing.

In the take-off process, the rotor wing and the engine can be connected by the clutch, the rotor wing rotates actively to drive airflow to enable the air bag umbrella to obtain upward initial power, and the rotor wing also generates a certain lifting force, so that the rotor wing and the air bag umbrella are matched with each other to realize vertical take-off. Because the rotor wing and the air bag umbrella simultaneously provide ascending power, the vertical takeoff process can be shortened.

At the landing in-process, it will to utilize the clutch with the same reason the rotor is connected with the engine, let the rotor initiatively rotate, it makes the gasbag umbrella obtain ascending power to drive the air current, the rotor rotational speed is higher, ascending power that the gasbag umbrella obtained is just big more, make the parachute effect especially obvious, even on the gyroplane is close to the height on ground, the gasbag umbrella also can provide enough, stable lift, this lift is enough to keep the balance and the stability of fuselage gesture, consequently can solve current gyroplane well and be being close to the ground (including flight and take-off and land the process) fuselage gesture unstability or even have the problem of the risk of turning on one's side, greatly promoted the stability and the security of gyroplane, embody "not dead" characteristics well.

The gyroplane with the airbag umbrella cap is further provided with a bracket 3, the edge of the airbag umbrella is fixed on the bracket to keep the unfolded state, the bracket is installed on the fuselage, and in the embodiment shown in the attached drawings, the bracket can be connected to a rotating shaft 5 of the rotor. The support can include plane support ring and a plurality of bracing piece, the upper end of a plurality of bracing pieces with the plane support ring is connected, the lower extreme of a plurality of bracing pieces with the pivot of rotor is connected, a plurality of bracing pieces center on pivot a week interval distribution of rotor just inclines the setting separately. The rotor wings should be completely within the covering range of the airbag umbrella in the front-rear direction. In the embodiment shown in the drawings, the diameter of the rotor is not larger than the maximum dimension of the umbrella in the fore-and-aft direction in the unfolded state.

The bracket is used for ensuring the effective expansion of the area of the air bag umbrella and can adjust the posture of the air bag umbrella.

Taking the embodiment shown in the attached drawings as an example, the bracket can be fixedly installed relative to the rotating shaft, and the plane supporting ring of the bracket is kept parallel to the plane of the rotor wing. When the rotor tilts as required, the air bag umbrella tilts along with the rotor synchronously. The support also can adopt angularly adjustable mode to install on pivot or the fuselage to can be independent of the rotor is adjusted the inclination alone, makes the gyroplane can respond to more kinds, more complicated air current situation freely with more nimble and safe flight gesture in flight process.

The airbag umbrella is preferably of a bilaterally symmetrical structure.

The left and right side edges of the bracket are respectively fixedly provided with a left wing plate and a right wing plate 4 which extend leftwards and rightwards in the horizontal direction. The left wing plate and the right wing plate are also part of the bracket, and in this embodiment, are respectively fixed on the edges of the middle sections at the left and right sides of the plane support ring, and of course, the air bag umbrella and the left and right wing plates are also relatively fixed. The left and right wing plates may serve as extensions of the airbag umbrella in the left-right direction. The rotor wing is completely located in the shade range of the air bag umbrella, the left wing plate and the right wing plate in the left-right direction. In the embodiment shown in the figures, in which the centre of the bracket is fixed to the axis of rotation of the rotor, the diameter of the rotor is not greater than the distance between the points of the left and right wing plates that are furthest apart.

In the unfolded state, the edge of the airbag umbrella can be circular or elliptical with the front-back length larger than the left-right width, wherein the circular and elliptical shapes include the circular and elliptical shapes in strict geometric sense and the approximate circular and elliptical shapes, and the latter is more common in practice. The planar support ring of the bracket is correspondingly made into a circle or an ellipse according to the shape of the edge of the air bag umbrella.

The outer surface of the air bag umbrella is preferably a streamline smooth curved surface, the streamline gradient of the surface close to the front is gentle, the streamline gradient of the surface close to the rear is steep, and the whole air bag umbrella is in a shape of a peaked cap. The air bag umbrella can also be called an umbrella-shaped cap, an umbrella cap and an air bag umbrella cap. The utility model provides a novel gyroplane indicates the gyroplane of taking gasbag umbrella cap promptly. The air bag umbrella with the shape can further effectively reduce wind resistance in flight, reduce power loss and improve action flexibility.

The machine body is preferably of an inner-outer double-layer structure and can be also called as a liner type machine body. The cabin is arranged in the inner layer and is made of high-strength materials, a plurality of anti-seismic springs 14 are arranged between the inner layer and the outer layer in a dispersing mode, two ends of each anti-seismic spring are respectively abutted to the outer surface of the inner layer and the inner surface of the outer layer, and other cavities in front of the inner layer and the outer layer are filled with foamed plastics 15. The fuselage is provided with a hatch 13, and the undercarriage 12 is fixed at the bottom of the fuselage. By adopting the fuselage structure with the flexible anti-vibration characteristic, the influence of vibration on the fuselage can be effectively reduced, the service life of the fuselage is prolonged, the riding comfort level is also improved, the strength and the anti-vibration performance of the fuselage are obviously improved, and the safety of the gyroplane is further improved.

The rear half part of the body and the front part of the tail wing 11 can be also provided with a rear power fan 10 which is mainly used for providing forward power for the gyroplane.

The air bag is preferably of an integral structure provided with a plurality of air bag units, namely the air bag umbrella is an umbrella-shaped opened air bag combination. Each air bag unit is sealed, and an air inlet with a reverse valve is arranged on each air bag unit. When the air bag is inflated, the whole air bag units are inflated synchronously, and when the air bag is full, the reverse valve is closed automatically. By adopting the structure of a plurality of air bag units, once a certain air bag unit leaks air, other air bag units are still in a normal inflation state, and the reliability is better.

The flight characteristics of the invention are as follows:

1. taking off and vertically rising:

at the moment, the rotor wing is connected with the engine to rotate actively, so that the air flow is driven to rotate and then is conveyed to the air bag umbrella, and the air bag umbrella obtains upward power. The rotor itself also generates a certain lift force to enable the gyroplane to take off vertically.

2. Horizontal forward flight:

when the power fan is lifted vertically and separated from the ground, the power fan works to generate forward thrust, the power of the active rotation of the engine can be reduced at the moment, the rotor wing is close to a powerless rotation state, and the whole gyroplane flies forward and lifts under the combined action of the power fan, the rotor wing and the air bag umbrella.

3. Gliding and flying:

because the air bag umbrella can adjust the posture through the bracket to glide and fly, the rotor wing can also provide the lift force, so that the rotor wing machine has various functions of gliding and flying.

4. Vertical landing:

when the rotorcraft of the present invention lands, the rotors gradually receive power from the engine that slows the landing without requiring forward coasting.

5. Hovering in the air:

similar to the vertical lifting process, the rotor wing is connected with the engine to actively rotate to drive the air flow to rotate, the air flow upwards impacts the air bag umbrella, and the acting force of the rotor wing and the air bag umbrella is synthesized to form lifting force capable of overcoming the gravity of the gyroplane, so that the gyroplane can hover in the air.

The manned aircraft is the most safe rotorcraft which has the advantages of least energy consumption and highest cost performance, can safely land in a free-fall mode under the condition of completely losing power, and the manned aircraft has more important requirements on safety and flight attitude stability, so the technical scheme of the invention particularly adopted on the manned rotorcraft can highlight the advantages of the manned aircraft.