RU2567695C1 - Flying winded helicopter - Google Patents

Abstract

FIELD: aircraft engineering.SUBSTANCE: step-up planetary gearing comprises pinions, winder is composed of a ratchet wheel arranged at airframe to run in one direction and including ratchet teeth and inner gearing teeth on inner surface and notches on outer surface. Note here that ratchet pawl is made on airframe. Note also that helical spring outer end is secured at said airframe while inner end is coupled with the shaft of spider provided with cover. Note that upper and lower rotors have upper and lower blades. Every of said upper and lower blades can be made of a single part or separately and coupled by appropriate fastener. Upper rotor hub and cover can be composed by single part or made separately. Upper rotor upper blades can be integrated with cover while lower rotor lower blades can be integrated with airframe. Device can incorporate several helical springs.EFFECT: increased range owing to reduced weight and overall dimensions, improved manufacturability.8 cl, 4 dwg

Description

The invention relates to the field of flying models and is directed to the use of kinetic energy sources in flying models and can be used to demonstrate the possibility of flying through the use of kinetic energy stored in the spring, as well as to create reduced flying models.

Known aircraft using flapping wings "dragonfly" (RF patent No. 2375253, CL B64C 33/02, A63H 27/28, 2008), consisting of a body with articulated wings, a power plant and drive flapping wing movements. The power plant is made in the form of an engine with a gearbox, and two crank mechanisms are used for the drive, which drive the power shafts into oscillatory movements, which through the chain gears provide flapping movements of four symmetrical flat wings. Each wing is equipped with a rotation mechanism located in the root of the wing on the central spar, which is installed in the fork and rotates in it during oscillatory movements of the wing using two ratchet mechanisms, each of which consists of two disks. One disk is rigidly fixed on the wing spar and has two diametrically opposite depressions with supporting surfaces for engagement, and the other disk with a dog and spring can rotate freely and is made in the form of a pulley, in the creek of which one end of the cable is rigidly fixed, and the other end of the cable through pulleys mounted on a fork, mounted on a control lever.

A significant drawback of this aircraft is the presence of reciprocating movements in the operation cycle, which leads to the occurrence of vibrations. The disadvantage is the presence of chain transmissions, many articulated nodes and other parts, which reduces the reliability of the whole mechanism as a whole and increases the weight of the whole structure.

Also known is the "rotorplane" (RF patent No. 22585824, class B64C 29/00, B64C 29/02, 2001) containing a fuselage located between two rotors with wings, the longitudinal axes of which are located in horizontal planes, a mechanism for changing the angle of attack of the wings and engine. Each wing is made up of individual blades with a thin profile symmetrical with respect to the chord, mounted at intervals and connected into a single wing by ribs on which the axles are installed, which enter the holes of the struts, rigidly connected to the rotor shaft. Behind each rotor, parallel to the axis of its shaft, on the frame mounted on the tail boom, a reflective wing shield is installed, the portion of which is facing the rotor is made of a deformable material. The mechanism of changing the angle of attack of the wing has a sleeve, on the cylindrical surface of the free end of which rings are mounted, connected by a thrust with a spike on the rib of each wing. The other part of the sleeve is located in the windows of the vertical and horizontal sliders, which are moved together with the sleeve by screws with a drive relative to the axis of the rotor shaft passing inside this sleeve. A ring is mounted on the end part of the rotor shaft to eliminate the weight load; it is rigidly connected by supports to the rack on the tubular part of the rotor shaft and enters a cylindrical surface in the grooves of the rollers with axles mounted on the fuselage.

A significant drawback of this device is the presence of two horizontal rotors with wings, which during rotation will experience significant loads and therefore must be strong enough and therefore heavy, which will increase weight and size and will not allow a sufficiently reliable and light aircraft.

Known "flying saucer" (RF patent No. 2365522, CL B64C 39/06, B64C 27/20, B64C 29/02, 2006). The aircraft consists of a domed cabin, a ceiling, an engine room with motors, a gearbox, a vertical lift rotor, a vertical shaft, a bearing support, a coil and three support wheels. In the design of the aircraft, a compound annular wing is used, the fixed wing of which is attached to the engine room below the ceiling of the ceiling. The movable wing is part of the vertical lift screw, connected motionlessly with the hub by ribs and pivotally with the rotor blades.

A significant drawback of this aircraft is the presence of an air flow system, enclosed in the body of the device, which increases its size and weight.

The closest in technical essence and the achieved result to the invention is a “flying clockwork helicopter” (RF patent No. 2452871, F03G 1/00, A63H 1/06, 06/10/2012), comprising a housing, a first vertical lift rotor, characterized in that it contains a multiplier, a spiral spring, a second rotor of vertical lift, a ratchet, a winding key, while the first rotor of a vertical lift is connected to the housing through a multiplier and a spiral spring, and with a winding key - through a ratchet, while the second rotor of a vertical lift is located on Oppus.

The disadvantage of the closest analogue is the low manufacturability of the design and significant weight and size indicators.

The objective of the invention is to simplify the design, reduce weight and size, by placing ratchet dogs on the case and, as a result, increase the diameter of the ratchet wheel, use the internal gear gear made in the ratchet wheel, and use the notches on the ratchet wheel as the crown.

The technical result is an increase in flight range by reducing weight and size indicators, improving the manufacturability of the design.

The problem is solved, and the technical result is achieved by the fact that in a flying winding helicopter containing a winding key and a casing connected to the upper rotor fixed by the rotor hub on the pinion shaft through a multiplier and a spiral spring and with the lower rotor located on the casing, according to the invention, the multiplier is made planetary and contains satellites, the crown is made in the form of a ratchet wheel located on the housing with the possibility of rotation in one direction and containing on the inside the surface of the ratchet teeth and the teeth of the internal gearing, and on the outer surface of the notch, and the ratchet dog is made on the housing, while the outer end of the coil spring is fixed to the housing, and the inner end is connected to the shaft of the carrier containing the cover, while the upper and lower bearing the screws have respectively upper and lower blades.

In addition, according to the invention, each of the upper and lower blades can be made in one piece.

In addition, according to the invention, each of the upper and lower blades can be made separately and interconnected by a fastening element.

In addition, according to the invention, the upper rotor bush and the cover can be made separately.

In addition, according to the invention, the upper rotor bush and the cover can be made in one piece.

In addition, according to the invention, the upper blades of the upper rotor can be made in conjunction with the cover.

In addition, according to the invention, the lower blades of the lower rotor can be made in conjunction with the housing.

In addition, according to the invention, there may be several coil springs.

The invention is illustrated by drawings. In FIG. 1 shows a kinematic diagram of a flying clockwork helicopter with blades made separately and interconnected by a fastening element; FIG. 2 shows a kinematic diagram of a flying clockwork helicopter with upper and lower blades, each of which is made of one piece, in FIG. 3 is a kinematic diagram of a flying clockwork helicopter with an upper rotor hub combined with a cap; FIG. 4 shows a kinematic diagram of a flying clockwork helicopter with two oppositely fixed springs.

A flying clockwork helicopter contains an upper rotor (not shown in the drawing) containing the upper blades 1, the upper rotor bushing 2, mounted on the pinion shaft 3, mounted in the carrier 4 with a cover 5 (Fig. 1). The ratchet wheel 6 is mounted on the housing 7 and has the possibility of engagement with it. The carrier 4 is installed in the housing 7 and in the ratchet wheel 6. The lower rotor screw (not shown in the drawing) contains lower blades 8 mounted on the housing 6. The spiral spring 9 is fixed by its external coil in the housing 6, and its center (internal coil) is fixed in the carrier 4. The carrier 4, the cover 5 with the satellites 10 installed therein, included in the gearing and connected with the ratchet wheel 6 and the pinion shaft 3, are a multiplier (not shown in the drawing).

The upper rotor with the upper blades 1 and the lower rotor with the lower blades 8 can be made in the form of one part (each) or separately (Fig. 2), the sleeve of the upper rotor 2 and the cover 5 can be made separately or with one part (Fig. . 3). The upper blades 1 of the upper rotor can be made in conjunction with the cover 5. The lower blades 8 of the lower rotor can be made in conjunction with the housing 6. Instead of one coil spring 9, there can be several coil springs (Fig. 4).

The proposed device operates as follows.

The upper rotor with upper blades 1 and the lower rotor with lower blades 8, rotating in opposite directions, balance the reactive moment and create thrust, which is the lifting force that ensures the flight of a flying clockwork helicopter. The source of energy is a coil spring 9, the rotation of which is converted through the multiplier into the rotation of the pinion shaft 3 with the upper rotor installed on it. The spiral spring plant 9 is carried out by rotating the ratchet wheel 6 located between the upper and lower rotors. In this case, the upper rotor is held together with the ratchet wheel 6, and the housing 7 with the lower rotor rotates in the opposite direction.

So, the invention allows to increase the flight range, using the energy stored in the coil spring with its subsequent transfer to two rotors and obtaining lifting force, and also allows to increase the manufacturability of the design and reduce weight and size indicators by placing ratchet dogs on the case and, as a result, increasing the diameter of the ratchet wheel, using the internal gear made in the ratchet wheel, and using the notches on the ratchet wheel as a winding key.

Claims (8)

1. A flying clockwork helicopter containing a crown, a ratchet and a housing connected with an upper rotor fixed by a rotor hub on the pinion shaft via a multiplier and a spiral spring, and with a lower rotor located on the housing, characterized in that the multiplier is planetary and contains satellites, the crown is made in the form of a ratchet wheel located on the housing with the possibility of rotation in one direction, and containing ratchet teeth and internal gear teeth on the inner surface, and on the outer surface is notches, and the ratchet dog is made on the housing, while the outer end of the coil spring is fixed on the housing, and the inner end is connected to the shaft of the carrier containing the cover, while the upper and lower rotors have upper and lower blades, respectively. 2. A flying clockwork helicopter according to claim 1, characterized in that each of the upper and lower blades is made of one piece. 3. A flying clockwork helicopter according to claim 1, characterized in that each of the upper and lower blades is made separately and interconnected by a fastening element. 4. A flying clockwork helicopter according to claim 1, characterized in that the upper rotor bush and the cover are made separately. 5. A flying clockwork helicopter according to claim 1, characterized in that the upper rotor bushing and the cover are made in one piece. 6. A flying clockwork helicopter according to claim 5, characterized in that the upper rotor blades of the upper rotor are made in conjunction with the cover. 7. A flying clockwork helicopter according to claim 5, characterized in that the lower blades of the lower rotor are made in conjunction with the body. 8. A flying clockwork helicopter according to claim 1, characterized in that it contains several coil springs.

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