WO2016010457A1

WO2016010457A1 - Rotary vane engine

Info

Publication number: WO2016010457A1
Application number: PCT/RU2015/000425
Authority: WO
Inventors: Вячеслав Иванович НЕГРУЦА
Original assignee: Вячеслав Иванович НЕГРУЦА
Priority date: 2014-07-14
Filing date: 2015-07-07
Publication date: 2016-01-21
Also published as: RU2014128521A

Abstract

The proposed invention is based on a transmission method achieved via a central shaft and multistage eccentric shafts (stationary, rotating or pivoting), which provide for the regular rotation of a rotor around the central shaft, with an irregular rotation of the walls of working chambers around the eccentric shafts, thus creating variable volumes of the working chambers during circumferential rotation. A rotating/reciprocating interaction between joints and an application area allows for minimal losses due to frictional forces, and rotation stabilizers allow for distributing the rotational moment around the circumference and for reducing vibration, the above factors contributing to increased efficiency of the device. The use of bellows chambers allows for using an additional working force which is generated when re-aligning the walls of a bellows chamber which are straightened under pressure. Spring elements are used for stabilizing components which are rotating irregularly around the shafts, said spring elements forming a rotation stabilizer and being intended for eliminating vibration, while also allowing for distributing, amongst components which rotate along the perimeter, the irregularity of an angular rotational moment. The function of a propulsive device can be provided as a separate structure, having the function of converting rotational motion to reciprocating motion in the presence of an external source of a rotational moment, while also acting as walls of chambers of an engine, and, simultaneously, as walls of chambers of the propulsive device.

Description

R0T0RN0-L0PASTNY ENGINE

DESCRIPTION

FIELD OF TECHNOLOGY. The invention relates to mechanical engineering and can be used in the field of engine building, the automotive industry as well as pumps and compressors.

BACKGROUND OF THE INVENTION Rotary vane engines (RLD) - the materials presented in this application are options for improving the analogue (the same author), patent application RU 2013149049 dated 05. 11. 2013, published in the official FIPS bulletin (Rospatent), "Inventions. Utility models ", N ° 13 of May 10, 2015. An engine containing a rotor, working chambers in the form of accordions located between the walls of the chambers, is equipped with hinges mounted on the walls of the chambers or on the rotor, and the axis of rotation of the rotor and the walls of the chambers are connected by a knee - this application does not use the entire volume between the two chambers.

In the proposed embodiment, the stated disadvantage is eliminated which contributes to an increase in efficiency.

And also from the prior art there is known an engine containing a rotor, working chambers in the form of accordions located between the walls of the chambers, capable of rotating around a circle around the axis of rotation of the rotor and providing an increase and decrease in the volume of the working chambers (see RU 2491438 C2, 27. 08 . 2013, F01C 9/00).

The disadvantages of the known device are that the walls of the working chambers, moving in a circle around the axis of rotation of the rotor, carry out multidirectional movement, and have dead points of inertia of movement, which leads to ineffective loads and energy losses.

SUMMARY OF THE INVENTION The objective of the invention is to remedy the above disadvantages - the axis of the central shaft, on which the rotor rotates, as well as the rotating second shaft with an eccentric axis, have hinges which, through the application zones for the hinge, control the angle of rotation of the chamber walls and the volume of the working chambers formed between two adjacent chamber walls.

The technical result consists in ensuring the balance of mechanisms, balancing angular moments of rotation and ensuring more efficient operation.

The technical result of the present invention is to replace the friction zones between the parts with rotating and rotational-translational ones, that is, eliminate friction between the parts during operation and balance the angular moments of rotation with a rotation stabilizer to reduce vibration and achieve stable rotation of the mechanism parts, which helps to reduce losses and increase The efficiency of the mechanism.

In the proposed embodiment, the central shaft is the support of the holding wall of the chambers and due to this, a lever is created for the moment of rotation being created, with emphasis on the central shaft, and there is no reason for the occurrence of reverse torque in the central shaft itself, since the axis of the shaft is this very center of the point lever support. Eliminate dead points of inertia in the work of parts - this is achieved by the fact that work takes place cyclically around a circle with unidirectional rotation of all parts, and from the beginning to the end of the cycle of the work process.

The constructive and technical tasks to be solved by the invention are as follows: the walls of the chambers are fixed to the shaft - this allows us to lay a minimum clearance to the walls of the housing, and relative to the rotor, the wall of the chamber sways - the losses are minimal; working parts are attached to the shafts, which minimizes structural clearances and reduces losses; at the rotation stage, when the distance between the chambers is minimal — the angular velocity is less than the working rotor rotation speed (depending on the difference between the axes of the central shaft and the second (or third shaft) it can be several times smaller) - which contributes to the effective moment of supply of the exploded fuel ; the possibility of re-supplying additional pressure to the working chamber at the stage of the working cycle (pressure expansion chamber under pressure is the working process), especially in the area when the shoulder of the chamber wall impact on the rotor hinge reaches its maximum value and the exposure angle is the most effective, that is, at 180 ° - supply of additional working pressure to the working chamber (as it expanded and the pressure dropped) - the result is an increase in power; the use of an additional supply of a high-pressure mixture: 1) from a jet engine nozzle - contributes to an increase in operating pressure, i.e. power; use of standardized channels for fuel supply, ignition connection, high pressure mixture supply, jet nozzle connection, connection of pump hoses, spent mixture discharge channels, hoses for pushing the compressed volume from the pump, as well as plugs for closing the channels not used in the functional purpose variant; symmetry of use of parts - allows you to turn parts 180 ° over wear; symmetry of the use of parts - allows you to use the mechanism in the opposite direction - the working reverse rotation (when connecting the corresponding channels (fuel, ignition, exhaust, etc.) on the case); to lay down the number of chamber walls with their ability to be removed or added during operation, that is, change the number of working chambers in one circuit of working chambers (KRK) (observing the symmetry of the location on the shafts, for example, a set with 10 walls can work: 10, 5, 2; or a set of 12 with options: 12, 6, 3, 2). In both cases there is an option with an odd number of cameras for the push-pull cycle, it remains to choose a more suitable one with 5 or 3 cameras; RLD with separated working chambers and having two circuits of the working chambers of the CRC - one works with the engine function, the other - the pump; RLD operation with the possibility of exchanging working chambers: the pump works as an engine, and the engine works as a pump; for stabilizer of rotation - the possibility of using forms and types of springy elements existing in the production; the proposed transmission method with rotating shafts allows during operation the ability to control: a) the radius of the joint with the application area; b) the differences between the axes of the central, second and third shafts - this allows you to choose the RLD mode: power or speed;

2) technical: to exclude the idling process (fuel economy) when the engine is running - since during short-term stops, the inertial force of the moment of rotating parts works; inertial force of the moment of rotation all the masses of parts - use as accelerating force from a place, charging the battery; use braking (before stopping) or on descents to disperse the inertial force of rotating masses; the use of a high pressure mixture from: heating plants, gas and oil production, underground thermal pressure as a source of rotation for drilling to a depth or connecting to an electric generator; the proposed transmission method with rotating shafts allows during operation the ability to control: the radius of rotation between the shaft axes and, accordingly, the minimum distance between the walls of the chambers, which means to regulate the compression ratio of the supplied fuel — and use any fuel: gas, gasoline with a different octane rating, diesel fuel (turning off ignition system));

Signs characterizing the device of the invention: the axis of the shafts around which the working parts rotate are offset and because of this the rotation around the shafts is unidirectional, but differently accelerated and cyclically repeated, the interaction between the parts is rotational and / or rotational-translational.

The technical result is due to the fact that the rotor rotates on the central shaft, is located on the side of the chamber wall and interacts with each other rotationally and / or rotationally. The chamber wall, rotating around the second shaft, uses it not only as a support for rotation, but also as a support for the lever to create a working torque.

The walls of the working chambers are interconnected by the same springy elements - a rotation stabilizer: accumulating energy, deforming while decreasing the distance between the walls of the chambers and giving up the accumulated energy with increasing distance between the walls of the chambers, which helps to stabilize angular moments with variable angular rotation.

BRIEF DESCRIPTION OF THE DRAWINGS. The invention is illustrated by drawings, which do not cover and do not limit the entire scope of the claims of this technical solution, but are only illustrative materials of a particular case of execution:

Figure 1 - Rotary vane engine - RLD. Scheme (in statics) of the invention. Figure 2 - Diagram of the dynamics of the RLD example - two walls of the chambers (cross section).

Figure 3 - Diagram of the dynamics of the RLD example - four walls of the chambers (cross section)

Design description - Rotary Vane Engine (RLD):

Figure 4 - Device RLD with hinges on the rotor (longitudinal section).

Figure 5 - Device RLD with hinges on the rotor (cross-section section AA).

Figure 6 - Option hinge device (node B).

Figure 7 - RLD device with hinges on the rotor (cross section of section BB).

Figure 8 - Device RLD with the supply of the working mixture through the second shaft (cross section). Figure 9 - RLD device with engine function and pump function (longitudinal section).

Figure 10 - Device RLD with hinges on the walls of the chambers (in volume).

Figure 11 - RLD device with hinges on the walls of the chambers (longitudinal section). Figure 12 - Device RLD with hinges on the walls of the chambers (cross section, section. G-G).

RLD device + Propulsion

Figure 13 - RLD device + Propulsion with a third shaft, (in volume):

Figure 14 - Device RLD + Propulsion with a third shaft, (cross section)

Figure 15 - RLD device + Mover with imbalance, (cross section).

Figure 16 - Device RLD + Propulsion with an imbalance (schematically in volume).

RLD - transmission methods

Figure 17 - RLD - transmission method with rotating shafts, (in volume).

Figure 18 - RLD - transmission method with rotating shafts, (section cross section DD).

Figure 19 - RLD - transmission method with a different shape of the application zone example 1.

Figure 20 - RLD - transmission method with a different shape of the application zone example 2.

Figure 21 - RLD - method of transmission with a rotating rod 360 °.

Figure 22 - RLD - transmission method with a rotary bar 180 °.

Figure 23 - RLD - transmission method with a third shaft and a baffle, (in volume).

Rotation stabilizer device

Figure 24 - Device rotation stabilizer - compression springs.

Figure 25 - Device rotation stabilizer, - bending springs.

Figure 26 - Device rotation stabilizer, - bellows spring chamber.

Figure 27 - Device rotation stabilizer, - springy containers.

Design description - Rotary Vane Engine (RLD) with bellows chambers: Figure 28 - RLD device with bellows chambers and a spacer (longitudinal section of the chamber walls).

Figure 29 - Device RLD with bellows chambers and a spacer, (section E ^' -E ^' ).

Figure 30 - RLD device with bellows chambers and a spacer, (section E ^" -E ^" ).

Figure 31 - The device RLD with bellows cameras and double separating spacers.

(cross section).

Figure 32 - Device RLD with bellows cameras with an offset focus (cross section).

Figure 33 - Device RLD with bellows chambers having visors with the supply of the working mixture of high pressure through the second shaft 2. (transverse section, nodes F and F ^' )

Figure 34 - The device RLD sealed with bellows chambers having bellows hoses for supply and exhaust, (longitudinal section).

Figure 35 - Sealed RLD device with bellows chambers having bellows feed and outlet hoses, (cross section, section 3-3, unit I).

Design description - Rotary Vane Engine (RLD) - working chambers inside the chamber wall:

Figure 36 - RLD device with a working chamber inside the chamber wall - the general principle, (in volume, node K). Figure 37 - RLD device with a working chamber inside the chamber wall — supply from above from the housing, (longitudinal section, section L-L).

Figure 38 - RLD device with a working chamber inside the chamber wall - supply from above from the housing, (cross section, section L-L).

Figure 39 - Option 23 according to option 22, the RLD device, the working chamber inside the chamber wall is the bottom feed from the housing, (longitudinal section, cross-section MM)

Figure 40 - Option 23 according to option 22, the RLD device, the working chamber inside the chamber wall is the bottom feed from the housing, (cross section, cross-section MM, node H)

Design description - Rotary Vane Engine (RLD) - working chambers inside the rotor:

Figure 41 - RLD device - working chamber inside the rotor - the general principle, (in volume) Figure 42 - RLD device - working chamber inside the rotor - supply from the top, (longitudinal section, section 0-0)

Figure 43 - RLD device - working chamber inside the rotor - supply from above from the housing, (cross section, section 0-0)

Figure 44 - RLD device - the working chamber inside the rotor - the bottom feed from the shaft or housing, (longitudinal section, section PP)

Figure 45 - RLD device - working chamber inside the rotor - supply from the bottom from the shaft or housing, (cross section, section П-П, unit Р)

Figure 46 - RLD device - working chamber inside the rotor - supply and pressure relief through shafts creating traction, (longitudinal section)

Figure 47 - Option hinges for RLD. (cross section, node C)

Electro Rotor Vane Engine - (electro RLD) Figure 48 - Device electro RLD with electric hinge, (cross section)

Figure 49 - Electro RLD device with an electric hinge, (section TT)

Figure 50 - Electro RLD device with an electric hinge, (U-U section)

Figure 51 - Electro RLD device with an electric hinge, (longitudinal section)

RLD device working chamber inside the chamber wall - supply from below from the second shaft.

Figure 52 - RLD device working chamber inside the chamber wall - supply from below from the second shaft, (longitudinal section, cross-section Ф-Ф)

Figure 53 - RLD device, the working chamber inside the chamber wall - supply from below from the second shaft, (cross section, cross-section Ф-Ф, unit X - overlay of the visors of the chamber walls during rotation, (enlarged))

CONVENTIONS ON FIGURES

1. central shaft 2. second shaft

3. bearings-2 4. axis of rotation of the second shaft

5. rotor 6. chamber walls bearings-1 8. hinge

application area 10. working pressure

torques 12. shoulder

case 14. working chamber

channel for supplying fuel 16. channel for ignition

channel for discharging waste 18. channel for supplying a mixture of high pressure mixture

forces camera 20. cavity

pressure chamber 22. ignition chamber

bellows wall chamber 24. electro-hinged

partition wall 26. sectors for supplying a mixture of high sector for the channel exhaust pressure

mixture 28. visor wall

pressure supply valves 30. waste gas discharge valve with sealed bellows bearing 32. bellows high pressure mixture hose mixture feed hose

sealed bellows bearing 34. bellows hose to discharge the waste hose

sealed second shaft bearing 36. valve disc

the third shaft 38. the walls of the chambers of the third shaft bearings-5 40. the area of application of the third shaft the hinges for the third shaft 42. the hinge on the third shaft of the application area for the third shaft 44. imbalances

hinges-imbalances 46. the path of rotation of the imbalances centrifugal force 48. guide-rim

electromagnetic field 50. reduced centrifugal force electric motor-regulator of the central 52. electric motor-regulator of the second shaft of the shaft

bearings-3 54. eccentric central shaft; eccentric second shaft 56. electric motor-regulator of the third shaft

wired-channel 58. barbell

rotation circle 60. rotating disk

stiffening partition 62. springs-1

bending springs-2 64. springy bellows chambers stops 66. strut

articulated pin 68. springy containers

bellows stop 70. open entry 71. carriages 72. carriage bearings

73. spring carriages 74. piston hinge

75. hinge-carriage-piston 76. bearing-4

77. bearings-hinges 78. first-bearing-hinges

79. second-ball-bearing 80. spring-1

81. spring-2 82. groove-emphasis

83. focusing groove 84. stator-electric winding

85. hinged-electromagnetic winding 86. supply of electric current to the rotor

87. supply to the walls of the chambers of electric current 88. rotor-2

89. walls of chambers-2 90. walls of chambers-3

91. central-shaft-2 92. second shaft-2

93. the third shaft-2 94. The walls of the chambers-4

95. The walls of the chambers of the third shaft-2 96. The walls of the chambers-5

97. chamber walls-6 98. chamber walls-7

99. chamber walls-8 100. chamber walls-9

101. chamber walls-10 102. rotor-3

103. rotor-4 104. rotor-5

105. the wall of the chamber-11 106. the shaft-cavity-1

107. shaft-cavity-2 108. shaft-cavity-3

109. central shaft-2 110. shaft-cavity-4

111. central shaft-3 112. peaks-2

113. spark plug 114. bus power supply

EMBODIMENTS FOR CARRYING OUT THE INVENTION.

Rotary vane engine - RLD. Scheme (in statics) of the RLD invention according to the invention (figure 1): a central shaft 1 on which the rotor 5 rotates is connected to an offset second shaft 2 and around which the walls of the chambers 6 rotate on bearings 1 7. The wall of the chambers 6 has an application zone 9 , for impact (during rotation) on the hinge 8 (similar to the rocker mechanism), which is located on the rotor 5, this makes the rotor 5 rotate around the central shaft 1.

Scheme of the dynamics of the RLD (figure 2, 3): on the walls of two adjacent walls of the chambers 6 and 6 ^{', a} working pressure of 10 and 10 ^{' is} pressed, the same in strength and multidirectional in vector. The walls of the chambers 6 and 6 ^' having an emphasis on the second shaft 2, created torques 11 and 1 G, The walls of the chambers 6 and 6 ^' , through the application zones 9 and 9 ^' (which is part of the wall of the chamber 6 and 6 ^' ), press on the hinges 8 and 8 ^' (respectively), which are mounted on the rotor 5. The created torques 11 and 1 G act in different directions on the rotor 5. The magnitude of the created torques 11 and 1 G depends on the arm 12 and 12 ^' (the distance from the point of exposure to the working pressure of 10 and 10 ^' to the point of abutment in hinges 8 and 8 ^' ). Since the axis of rotation of the rotor 4 ^' and the axis of rotation of the second shaft 4 is offset, the shoulders 12 and 12 ^{' of the} application in a circle changes from maximum to minimum magnitude - and thereby changing the magnitude of the torque from largest to smallest. The resulting moments of rotation: is the difference between the moment of rotation 11 and the moments of rotation of 1 G or the difference between the shoulder 12 and the shoulder 12 ^{'- the} rotor 5 rotates around a circle around the central shaft 1 in the direction of influence of the largest shoulder - in the diagrams, in figures 2 and 3, this shoulder 12. The larger the difference between the maximum and minimum shoulder 12 and 12 ^' , the greater the difference between the torques 11 and 11 ^' , and as a result: the more efficient the engine.

Legend (figure 2) - take the position of the hinge 8 at the minimum radius equivalent to the position at 0 ° (zero degree), and the position of the hinge 8 at the maximum radius equivalent to the position at 180 ° (half-turn - 180 ° degrees).

Design description: Option 1 - RLD device with hinges 8 on the rotor 5 and the application zone 9 on the walls of the chambers 6 (figures 4, 5, 6, 7).

Description of the design of the RLD in a static state: the central shaft 1 is located in the housing 13; on the central shaft 1, the rotor 5 rotates with the axis of rotation of the rotor 4 ^' ; rotating rotors 8 are fixed on the rotor 5; the second shaft 2 is eccentrically attached to the central shaft 1 (on bearings-2 3 or without them); around the second shaft 2 on the bearings-1 7 the walls of the chambers 6 rotate; the axis of the second shaft 4 is the axis of the circle along which the walls of the chambers 6 rotate; the axis of rotation of the rotor 4 ^' and the axis of the circle of rotation of the wall of the chamber 6 are offset; the walls of the chamber 6 have an application zone 9 on each side (a niche, a notch); application zones 9 are designed for interaction (transmission / reception of loads) with joints 8 (with rotational-translational function); the space (that is, the volume) between two adjacent walls of the chambers 6 form a working chamber 14, designed to generate working pressure; the case 13 has unified channels (15, 16, 17, 18), that is, the same holes for cutting without screwing up different covers (interchangeable) depending on the functional purpose; a channel for supplying fuel 15; channel for ignition 16; channel for supplying a mixture of high pressure 18; channel for discharging the spent mixture 17.

Description of the design of the RLD in a static state: the central shaft 1 is located in the housing 13, the rotor 5 rotates on it and it has fixed hinges 8, the second shaft 2 with the axis 4, which is offset from the central shaft 1, is attached to the central shaft 1 with the axis of rotation of the rotor 4 ^' and accordingly from the axis of rotation of the rotor 4 ^' , the second shaft 2 is located on the central shaft 1 on bearings-2 3 (designed to reduce the loads of rotation on bearings-1 7 of the chamber walls 6), on the second shaft 2 are located on bearings-1 7 of the chamber walls 6 and they have on their side application zones 9 ( I’m looking, a recess), which are designed for interaction (transmission / reception of loads) with hinges 8 (with rotational-translational function) which are located to transfer these loads to the rotor itself 5. The space (i.e. volume) between two adjacent walls of the chambers 6 form a working chamber 14, designed for operating pressure. The housing 13 has unified channels (15, 16, 17, 18), that is, the same holes on the thread for screwing different caps (interchangeable) depending on functional purpose: a channel for supplying fuel 15, a channel for ignition 16, a channel for supplying a mixture of high pressure 18, a channel for discharging the spent mixture 17 and a dummy channel designed to close the hole if not necessary. A variant of the hinge 8 consists of (figure 6, assembly B): the hinge itself (shaft) 8 and the first-bearing-hinge 78 or a system of carriage-bearings 72 providing rotation in the application zone 9, so as to minimize dynamic impact between opposite walls of the application zone 9 from a change in the direction of workloads during RLD operation. The hinge 8 itself rotates on the rotor 5 to reduce rotational workloads in the application zone 9.

A possible option is to consider when the central shaft 1 and the second shaft 2 form one part (there is no bearing 2 3), and when the hinge 8 to the rotor 5 is fixed rigidly, without its own rotation on the rotor 5.

INDUSTRIAL APPLICABILITY RLD (figures 4, 5, 6, 7): from the housing 13 through the channel for supplying fuel 15 to the working chamber 14 is supplied fuel, inserted into the channel of the housing 13, the ignition channel 16 ignites the fuel. The created working pressure in the working chamber 14 acts on the walls of the chambers 6 with equal force but in different directions. The walls of the chambers 6 that rotate freely around the second shaft 2 (on bearings-1 7) can rotate only under the trajectory of rotation of the hinges 8, since they are inserted into the application zone 9 (which is part of the chamber 6 wall itself). Two adjacent walls of the chambers 6 forming the working chamber 14 and subject to the created working pressure resting against the hinges 8 (through the application zone 9) and pivotally resting on the second shaft 2 create two torques opposite in direction and different in power due to the difference in the arm acting on hinge 8. The resulting moment of rotation - the torque with the largest shoulder, which created the greatest moment of rotation - through the hinge 8 makes the rotor 5 rotate. The process is ongoing while the volume of the working chamber 14 is increasing. During increasing the volume of the working chamber 14, the pressure drops, to increase the working pressure through the channels for supplying a mixture of high pressure 18 (located in the channels of the housing 13) additional pressure is supplied. When rotating to a position when two adjacent walls of the chambers 6 have the same radius of influence on the hinges 8, because of this, the increase in the volume of the working chamber 14 is over - the work process is over. The wall of the working chamber 6 reached the channel for ejecting the spent mixture 17 — the mixture from the working chamber 14 from the centrifugal force and from the compression pressure (since the walls of the chambers 6 approach each other, and therefore the volume of the working chamber 14 decreases) is removed from the RLD engine. The walls of the chamber 6 came close to the minimum distance, the volume of the working chamber 14 decreased to a minimum, the spent volume was removed as far as possible - the working cycle (cycle) was completed. Rotating further, a new cycle begins and the working chambers 14 alternating around the circumference provide a constant rotational load on the rotor 5.

The position of all rotating parts during the operation of the RLD engine is always fixed, this allows you to use the fuel, air, and ignition systems already in production, in the same way, through the distribution crankshaft of the ignition system and fuels are other supporting systems.

A variant of the RLD engine is possible - additional installation in the channels of the housing 13 of the second channel for supplying fuel 15 and the second ignition channel 16 or installation in the housing 13 of the channel with the nozzle of the reactive combustion chamber.

INDUSTRIAL APPLICABILITY RLD, option with pump function (RLD pump) (figures 4, 5, 6, 7):

Features: in the case 13, which has unified channels, that is, the same holes on the thread for screwing different caps (interchangeable) depending on the functional purpose, the channels for discharging the spent mixture 17 are screwed in, since the discharge of the spent mixture in its function provides for a large throughput, it means that the same channel is able to fulfill the function of a channel for suctioning the working mixture 17 ^' . In the rotation sector, with an increase in the volume of the working chamber 14, instead of: a channel for supplying fuel 15, an ignition channel 16, channels for supplying a high pressure mixture 18. Pump hoses are connected to these channels for the spent mixture. The operation of the RLD-pump - from the external source the rotor 5 is rotated, having hinges 8 which are inserted into the application zones 9 which are part of the chamber 6. The walls of the chamber 6 are rotated away from the adjacent walls of the chambers, expanding the working chamber 14 and through the channel for suction of the working chamber inserted into the housing 13 mixtures 17 ^' suck in the working mixture - the working process continues while the volume of the working chamber 14 increases. Up to the position when two adjacent walls of the chambers 6 have the same radius of influence on the hinges 8, because of this the increase in the volume of the working chamber 14 is over I - the workflow is over. The wall of the working chamber 6 reached the channel for ejection of the spent mixture 17 — the mixture from the working chamber 14 from the centrifugal force and the compression pressure (since the walls of the chambers 6 approach each other, and therefore the volume of the working chamber 14 decreases) is removed from the RLD. The walls of the chamber 6 approached to a minimum distance, the volume of the working chamber 14 decreased to a minimum, the compressed volume was removed as far as possible - the working cycle (cycle) was completed. The rotor rotating further begins a new cycle and the working chambers 14 alternating around the circumference ensure the continuous operation of the RLD pump.

If in the case 13 there are channels that are not involved in the work, then a unified channel-plug is designed to close the hole in the absence of need.

Option 2 according to option 1 - the operation of the RLD engine with a two-stroke cycle (figures 4, 5, 6, 7).

A dynamic feature is a two-stroke cycle RLD engine: it has an odd number of working chambers 14. Fuel is not supplied to each sequentially rotating alternating working chamber 14 - but through one. Similarly, fuel is ignited, through the channel for ignition of fuel 16, - not sequentially alternating working chambers 14 are ignited, but through one. In addition, alternation goes to neighboring working chambers. For example, with a design with 5 cameras (1-2-34-5):

- fuel is fed into the chambers - 1-3-5-24-1-3-5-2-4. . .

- ignition is supplied to the chambers - 24-1-3-5-24-1-3-5. . . An example of the dynamics of a two-stroke RLD engine (consider the Ne-1 camera). The first step: fuel is fed into the working chamber - expansion of the working chamber (half-turn) - compression of the working chamber with fuel (end of the turn and the first step) - ignition is supplied, the working process is ignited (half-turn of the second step) - compression of the working chamber the waste mixture is removed (end second turn and second beat). It turns out two-cycle cycle of the RLD engine.

Option 3 according to option 1 - device RLD-engine with the supply of the working mixture of high pressure through the second shaft (figure 8).

Symbol (Fig. 8): the walls of the chambers 6, the housing 13, channels for ejecting the spent mixture 17, channels for supplying the high pressure mixture 18, shaft-cavity-1 106.

Features: let's take a rotation around the circumference of the wall of the chambers 6 and the working chambers 14 rotating on the same shaft with the same functional purpose - the circuit of the working chambers of the CRC - the second shaft is connected to the central shaft and form one solid part shaft-cavity-1 106. Through them passes through ( for supply on both sides) a channel for supplying a high pressure mixture 18. In the sector of rotation of the walls of the chambers 6 where the working chambers 14 are expanding, there are holes in the channel that connects the volume of the working chambers 14 with the volume of the channel for supplying a high pressure mixture 18. When a high pressure mixture is supplied, it passes into the working chamber 14 and undergoes a working process under high pressure on the walls of the chambers 6.

Example 3: use the through channel through the central shaft and the second shaft 2 as a gun barrel for firing blank cartridges (shells) creating high pressure or ammunition, cartridges - before writing off as unsuitable (not to disappear good), shoot with all the free pressures side and not directed, as in cases of target destruction, as a result, the lethal force will be minimal, that is, there will be no lumbago but an ejection. Combustion waste is removed by pressure and centrifugal force.

Option 4 according to option 1 - RLD device with engine function and pump function (figure 9):

Features: in option 1, the operation of the RLD engine and the RLD pump was considered, which the mechanism performed alternately, that is, the same circuit of the working chambers of the KRK did not perform different functions simultaneously. Consider the option of arranging two CRCs in parallel with separate functional assignments (identical or different functions - but separately). This option 4, from option 1, differs in that the device has an additional central shaft 1 with an additional rotor 5 on which rotating through hinges 8 are located interacting with the application zones 9 (on both sides of the rotor 5) on the walls of the chambers 6 of the adjacent KRK. To ensure sealing between two adjacent KRK: the rotor 5 may be larger in diameter for insertion into a housing niche or add an additional sealed bearing at the same time providing additional emphasis to the long component shaft (consisting of central shafts 1 and second shafts 2).

Option 5 according to option 4, - RLD with application zone 9 on rotor-2 88 and hinges 8 on the walls chambers-2 89 (figures 10, 11, 12): Description of the design of the RLD in a static state: the central shaft 1 is located in the housing 13; on the central shaft 1 rotor-2 88 rotates; rotor-2 88 has an application zone 9 (niche, recess); an eccentric second shaft 2 is attached to the central shaft 1; around the second shaft 2 rotate the walls of the chambers-2 89; on the walls of the chambers 6, rotating hinges 8 are fixed on the sides; application zones 9 are designed for interaction (transmission / reception of loads) with hinges 8 (with rotational-translational function); the space (volume) between two adjacent walls of chambers-2 89 (shown conditionally on the diagram) form a working chamber 14, designed to generate working pressure; the housing 13 has unified channels, that is, the same holes on the thread for screwing different caps (interchangeable) depending on the functional purpose; a channel for supplying fuel 15; channel for ignition 16; channel for supplying a mixture of high pressure 18; channel for discharging the spent mixture 17.

INDUSTRIAL APPLICABILITY of the RLD with the application zone 9 on the rotor 5 and the hinges 8 on the walls of the chambers 6. Features of the variant are different in that the hinges 8 are mounted on the walls of the chamber-2 89 (which rotate on the second shaft) and interact with the application zone 9 which is located on the rotor -2 88 rotating on the central shaft 1. The working pressure in the working chamber 14 presses on the walls of the chamber-2 89, which has hinges 8 on its sides and acting on the application zone 9 makes the rotor-2 88 rotate. In the presented diagram, an option is indicated with two KRK of different working volume with interchangeable functions of the engine-pump, when 13 corresponding channels are installed on the housing.

Rotary Vane Engine (RLD) + Mover. Option 6 to option 1.

The constructive and technical problems to be solved by the invention: the possibility of choosing to use the device with two shafts or with three shafts - saving in wear of parts and excess supplied energy (rotating an unnecessary shaft); the possibility of choosing a transmission with the alignment of the axes of the shafts and use the rotation of the mass of parts (since they are located symmetrically along the axes) as a moment of inertia accumulator using an electric accumulator for charging or during subsequent acceleration;

The implementation of the invention.

Design description RLD + Mover in a static state, diagram - figures 13, 14: an eccentric second shaft 2 is attached to the central shaft 1; an eccentric third shaft 37 is attached to it; on the central shaft 1, a rotor 5 rotates on which hinges 8 are symmetrically fixed; around the second shaft 2, around the circumference, on the bearings-1 7 the walls of the chambers-3 90 rotate, which have an application zone 9 from the side of the hinges 8, and hinges for the third shaft 41 are fixed on the opposite side; around the third shaft 37 according to the circumference, on the bearings-5 39 the walls of the chambers of the third shaft 38 rotate, which have a side, on the hinge side for the third shaft 41 - the area of application of the third shaft 40;

INDUSTRIAL APPLICABILITY RLD + Propulsor with a third shaft, figures 13, 14. The rotational moment of the rotor 5 and with it the hinges 8, which interact with the application zone 9 and through it acting on the wall of the chamber-3 90 - makes it rotate around the circumference of the second shaft 2. The wall of the chamber-3 90 simultaneously, through the hinge for the third shaft 41 acts on the application zone of the third shaft 40 and thereby forces the walls of the chambers to rotate the third shaft 38 in a circle around the third shaft 37. That is, the rotational moment with a certain angular velocity is transmitted from the rotor 5 - hinge 8 - application area 9 - hinge for the third shaft 41 - application area of the third shaft 40 - the walls of the chambers of the third shaft 38. Since axis in the rotations of the elements are shifted, then the angular velocity changes and depends on the radius of application of the transmission of torque between the elements. The rotation axes are deliberately offset unidirectionally so that the maximum acceleration is summed in one sector. The figure 14 shows a diagram of the position of the rotating parts with the coincidence of directions for two reasons; displacement of the shafts (determined by the geometric arrangement (structurally)) and; maximum acceleration (in the sector where the maximum angles between the rotating elements (because the maximum angles between parts, because the maximum acceleration)). In this direction, the maximum centrifugal force of the propulsion is created. Option 7, option 6, Mover with an imbalance - (figures 15, 16):

Description of the design of the mover with unbalance in a static state: around the third shaft 37 the walls of the chambers of the third shaft 38 rotate; imbalances 44 are attached to the walls of the chambers of the third shaft 38 by means of hinges-imbalances 45; imbalances 44 rotate with the walls of the chambers of the third shaft 38 because they cannot change their position in the plane along the plane of rotation around the circumference; imbalances 44 can change their rotation path of imbalances 46 by rotation around hinges-imbalances 45, in a plane perpendicular to the plane of rotation, but centrifugal force 47 holds its position; imbalance 44 is made of materials acting on a magnetic field; in the housing 13 around the circumference (or in a specific sector) mounted guide-rim 48, which runs parallel to the plane of rotation of the imbalance 44 at a minimum distance for the ability to act on it, for example by an electromagnetic field.

INDUSTRIAL APPLICABILITY OF RRLD + Mover with an imbalance, figures 15 (across), 16 (schematically in volume). The chamber wall of the third shaft 38 rotates around the third shaft 37 in the same plane as the imbalance 44. The imbalance held by the hinges 45 and under the influence of the centrifugal force 47, the imbalance 44 rotates around a circle having a radius of rotation equal to the maximum distance from the shaft axis to the center of mass of the unbalance 44 (unbalance position 44 is parallel to the direction of centrifugal force (without deviation)). The imbalance 44 rotates at a minimum distance from the guide-rim 48. When the guide-rim 48 creates an electromagnetic field 49 on a certain sector of rotation, the affected imbalance 44 deviates from the plane of rotation by turning around the hinge-imbalance 45, while the centrifugal force 47 changes - it decreases by the cosine of the deflection angle and becomes reduced centrifugal force 50. A change in the centrifugal force only in a certain sector causes an unbalanced vibration of rotation due to the difference in the centrifugal force on the opposite side, and the ability to control centrifugal force in a certain area allows you to adjust the vibration process:

1) equalize the centrifugal force to stop the vibration;

2) control vibration when performing production tasks;

3) control the vibration in time, that is, vibration during the direct execution of working actions, and when idling, the device does not vibrate;

4) to regulate the direction and force of the mover or balance the centrifugal force around the circumference.

ROTARY-VANE ENGINE (RLD) AND TRANSMISSION METHODS (method of transmitting rotation and torque)

Objectives of the invention a new method of transmission in mechanisms, machines and devices that have cycles: increases-decreases; expand-contract; transform the rotation variable into stable; transform stable rotation into a variable.

The technical result to which the claimed invention is directed: using a transmission method with a choice of different transmission modes and / or using a variable torque, a transmission method that does not have friction between working parts, capable of operating in idle mode without consuming resources and with the ability to accumulate inert energy use parts rotation for subsequent acceleration or give to other mechanisms; a transmission method using the rotation method as a method that contributes to the least wear of parts by interacting between parts with unidirectional rotational actions, all parts have a smooth surface and a fixed location of the parts allows the transmission to be manufactured with a minimum technical clearance.

The technical result is achieved by the fact that the work cycle of the parts is carried out in a circle, which helps to eliminate dead spots in the work. As well as the ability to use the inertia of rotation, which helps to increase work efficiency. Using rotational and rotational-translational interaction between parts, that is, eliminate friction between parts during operation and balance the angular moments of rotation with a rotation stabilizer - to reduce vibration and achieve stable rotation of the mechanism parts, which helps to reduce losses and increase the efficiency of the mechanism.

The constructive and technical problems to be solved proposed by the invention are: elimination of friction between parts - interacting rotationally or rotationally-translationally; ensuring stable rotation, that is, reduce vibration, using a rotation stabilizer; the opportunity to choose to use the device with two shafts or with three - saving in wear of parts and excess supplied energy (by rotating an unnecessary shaft); the possibility of choosing a transmission with a combination of the axes of the shafts in order to use the inertia of the rotation of the mass of parts (since they are located symmetrically along the axes) as a moment of inertia accumulator using an electric accumulator for charging or during subsequent acceleration; The implementation of the invention.

Option 8 is a transmission method with rotating shafts, figures 17, 18: central-shaft-2 91 built-in housing 13 on bearings-3 53, and can rotate around its own external impact (for example, the electric motor-regulator of the central shaft 51 located in the housing 13). An eccentric central shaft 54 is integrated in the central shaft-2 91, which is connected to the second shaft-2 92. The eccentric central shaft 54 rotates about its axis relative to (starting from) the central shaft-2, (for example, a built-in electric motor-regulator the second shaft 52 located in the housing of the eccentric-central shaft 54). An eccentric second shaft 55 is built into the eccentric central shaft 54 and is able to rotate about its axis relative to (starting from) the eccentric central shaft 54, (for example, the electric motor-regulator of the third shaft 56 located in the case of the eccentric central shaft 54 is integrated) the second shaft 55 is eccentric connected to the third shaft-2 93. Electric current is supplied to the electric motors at the end of the mechanisms and the housing through the wire-channel 57.

INDUSTRIAL APPLICABILITY of RLD and features Option 8 transmission method with rotating shafts, figures 17, 18.

The walls of the chambers-4 94 (of the second shaft-2 92) and the walls of the chambers of the third shaft-2 95 (of the third shaft-2 93) rotate around a circle with differently accelerated angular rotation, which is determined initially structurally - by the radius of the hinges 8 - interacting with the application zone 9 on the second shaft-2 92 and, accordingly, the interaction of the application area for the third shaft 43 on the second shaft-2 92 with the hinge on the third shaft 42 also depends on it. Even when the engine, mechanism, device does not work for a short time. It is proposed to change the axis of rotation of the second shaft-2 92 and the third shaft-2 93 to align with the axis of the central shaft-2 91, to maximize the use of rotating forces of inertia of the parts during short stops. For this purpose, parts are provided that facilitate rotation of the axes of rotation of the second shaft-2 92 and the third shaft-3 93 to align with the axis of the central shaft-2 91. This is achieved by designing the central shaft-2 91 having an eccentric central shaft 54 connected to the second shaft-2 92. The eccentric central shaft 54 located on bearings-3 53 is therefore able to rotate about its axis of rotation, while being connected to the second shaft-2 92, the second shaft-2 92 also rotates relative to the axis of rotation of the central shaft-2 91. In the case of the alignment of the rotation axes of the second shaft-2 92 and the central shaft-2 91 then the radii of rotation to the joints 8 around the circumference will be the same, and accordingly the point of application in the application zone 9, that is, the walls of the chambers-4 94 rotate symmetrically around the circle with minimal friction loss during rotation and a large inertia of the rotating masses - you can use this force to charge the electric battery, the beginning of movement (during stops). This feature reduces wear on parts. The rotation of the eccentric central shaft 54 relative to the central shaft-2 91 is carried out by an external mechanism, or for example a fixed motor-regulator of the second shaft 52 which when current is supplied by wires through a wire-channel 57, rotation through a transmission system interacting with the central shaft-2 91 turns by the required angle. Moving the second shaft-2 92 to align the axis of rotation with the axis of the central shaft-2 91 does not move in a straight line (in radius), but along the arc of rotation of the eccentric central shaft 54; for adjustment, the possibility of turning the central shaft-2 91 relative to the housing 13 from external influence, for example, the electric motor-regulator of the Central shaft 51, which is located on the housing and interacting with the transmission system, rotates the Central shaft-2 91 relative to the housing 13. A transmission system through gears such so that the central shaft rotates from one engine and calculates the gear ratio, the next gear rotates the eccentric central shaft 54 - but this is another transmission.

Similarly, the third shaft-2 93 is aligned with the eccentric second shaft 55 located inside the eccentric central shaft 54 which is able to rotate around its axis to align with the axis of rotation of the second shaft-2 92. And when the rotation axis of the second shaft-2 92 is aligned with the axis rotation of the central shaft-2 91 therefore the axis of rotation of the third shaft-3 93 is aligned with the axis of rotation of the central shaft-2 91. As a result, the entire mass of working parts in the mechanism rotates symmetrically and therefore becomes stable and we can use the rotate total inertia force. To effect the rotation of the eccentric second shaft 55, an external action is used, for example, the built-in electric motor-regulator of the third shaft 56 located on the eccentric central shaft 54 which, through the transmission system, makes the eccentric second shaft 55 and, accordingly, the third shaft-2 93 rotate to the required angle.

The ability to select the radius of application of torque from maximum to zero allows you to use the transmission method without a gearbox, which increases the efficiency of engines, mechanisms, devices.

Option 9 is a transmission method with various forms of the application zone, figures 18, 19: on the second shaft 2, the walls of the chamber 6 with application zones 9 rotate; rotary joints 8 interacting with the walls of the chambers 6 through the application zone 9; the working chamber 14 is the volume between the walls of the chambers 6 used for the working process (if the engine is the expansion of the working pressure, and if the pump is suction); mechanism elements with an index ^' (apostrophe) shows the comparative changed position of the mechanism element.

One of the only factors considering the choice of the transmission method in this method is the choice of the interaction of the hinge 8 and the diligence zone 9, and one of the options is the selection of the shape of the application zone 9 no matter where they are located in the mechanism on the rotor or on the chamber wall, in any case, the working action occurs around the second shaft 2. Figures 8, 19 show: the second shaft 2, the walls of the chambers 6 rotating around it, the application zone 9, the hinge 8, and the working chamber 14 including these elements are indicated with a ^' (apostrophe) for comparative visual analysis changes. INDUSTRIAL APPLICABILITY of the RLD and features Option 9 transmission method with a different form of application area, figures: 18 example 1; 19 of example 2.

The implementation of the transmission method with the option of changing the shape of the chamber wall and the shape of the application area are two examples. When rotating around the circumference, the distance between the two walls of the chambers 6 varies depending on the changing radius from the hinge 8 to the axis of rotation of the second shaft 2. Increasing this radius and decreasing it symmetrically around the circumference of 360 ° increases the half turn of 180 °, and the next half turn of 180 ° decreases asymmetrically. to starting position.

But changing the shape of the wall of the chamber 6 and the shape of the zone of the application 9 allows you to constructively select a certain cycle of changing the parameters of increasing-decreasing the distance between the walls of the chambers 9, when the radius of the application from the hinge 8 to the axis of rotation of the second shaft 2 is asymmetric.

The figure 18 example 1, the violation of the asymmetric rotation, clearly shows the result of the violation of the asymmetric position of the parts - the application zones 9 ^' / 9 ^" , the walls of the chambers 6 ^' / 6 ^" and the volume between the two walls of the chambers 14 ^' / 14 ^" .

In figure 19, example 2, violation of the asymmetric rotation of parts. Where the result is achieved by selecting the location of the application zone 9 on the walls of the chamber 6 - zones of the application 9 ^' / 9 ^" , the walls of the chambers 6 ^' / 6 ^" and the volume between the two walls of the chambers 14 ^' / 14 ^" .

Option 10 according to option 9 is a 360 ° rotary bar transmission method of Figure 21: on the central shaft 1, a rotor 5 rotates on which hinges 8 are fixed; on the second shaft 2, the walls of the chambers-2 89 rotate on which hinges 8 are also fixed; the second shaft 2 is fixed to the central shaft 1 in an eccentric manner, therefore the rotation of the walls of the chambers-2 89 around the circumference around the second shaft, due to the interaction with the hinges 8 on the rotor, is not uniform; hinges 8, which are mounted on the rotor 5, and hinges 8, which are mounted on the wall of the chamber-2 89, are connected by a rod 58; all details of the mechanism are pivotally connected, that is, they rotate relative to each other; the circle of rotation of the rotary joints 8 and the circle of rotation of the joints 8 on the walls of the chamber 6 are the same but offset; the length of the rod 58 connecting the hinges is equal to the displacement length of these rotation circles, therefore, the distance between the interacting hinges is the same over the entire circumference and they changing their position relative to each other form their rotation circle 59, shown in figures 20, 21 by a dashed line; the rotation of the hinges 8 is one-sided, which provides an asymmetry in changing the distance between the cameras.

Characterized in that the rotor has a unidirectional hinge 8, and on the walls of the chambers-2 89, a unidirectional hinge 8 is fixed, and connected by a rod 58.

Implementation of the transmission method with two hinges rotating 360 ° (Figure 21): when the rotor 5 is rotated, a unidirectional hinge 8 attached to it connected through a rod 58 with a unidirectional hinge 8 mounted on the walls of the camera-2 89 forces the camera wall to rotate. The offset axis of rotation of the hinges 8 on the rotor 5 and on the second the shaft 2 is provided with a variable distance between the walls of the chambers 2. Rotating in a circle around the central shaft 1 and the second shaft 2, two hinges 8 connected to the rod 58 rotate in a circle around one another forming a circle with a radius of the length of the rod 58. 360 ° rotation is provided two prerequisites:

1) the diameter of the circle along which the rotor hinges rotate and the diameter along which the hinges (figure 21, pos. 59) of the chamber walls rotate must be the same;

2) hinges without reverse to rotate only in one direction - either only clockwise or only counterclockwise.

3) to prevent jamming during a transition of 180 ° (in cases where the pressure on the wall of the chamber-2 89 is less than the pressure on the hinge 8), the application area with a modified shape should be used.

Option 11 according to option 10 is a diagram of the transmission method with two hinges rotating 180 ° (figure 22): the figure shows: the central shaft 1, the second shaft 2, the rotor 5, the walls of the chambers-2 89, the hinge 8, the rod 58, the circumference of rotation 59 .

Characterized in that: the rotation of the hinges 8 is two-way; the circle of rotation of the rotary joints 8 is less than the circle of rotation of the joints 8 on the walls of the chambers, because of this, the rod 53 cannot rotate up to 180 °, that is, it performs rotation-rolling movements relative to the joints; because of this rotation of the wall of chambers-2, 89 is not asymmetrical around the circumference.

Option 11 according to example 10, characterized in that the hinge 8 rotates in both directions around its axis and the diameter of the circle along which the rotor hinges rotate and the diameter along which the hinges of the chamber walls rotate are different. 180 ° rotation is ensured by the condition: the rod should be larger or more equal than the distance between the joints 8.

Option 12 according to option 10 and option 11 - transmission with a third shaft and a partition, (in volume) :, figure 23:

Description of the design of the RLD Variant 12 of Variant 10 and Variant 11 - transmission with a third shaft and a baffle, (in volume):, diagram - figures 23: around the second shaft 2 the walls of chambers-3 90 rotate with hinges for the third shaft 41; with the second shaft 2, a third shaft 37 is eccentrically connected around which the walls of the chambers of the third shaft-2 95 rotate having a hinge on the third shaft 42; the hinges for the third shaft 41 and the hinge on the third shaft 42 are connected by a rod 58 and / or connected in a rotating disk 60; rotating discs 60 are sealed in a stiffening partition 61; the stiffening partition 61 is designed to provide tightness between the circuit of the working chambers (CLC) of the second shaft and the CLC of the third shaft, while providing an emphasis on the location of the second shaft 2.

INDUSTRIAL APPLICABILITY OF RLD and features Option 12 according to option 10 and option 11 is a transmission method with a third shaft and a baffle, figure 23: during the working rotation of the CRC of the second shaft 2, mounted on the walls of the chamber-3 90, hinges for the third shaft 41 through the rod 58, act on the hinges on the third shaft 42, which are fixed to the chamber wall of the third shaft-2 95. The hinges for the third shaft 41, the rod 58, and the hinges on the third shaft 42 - are housed in a sealed rotating disk 60 which is located in the stiffening partition 61, separating the KRK of the second shaft 2 and the KRK of the third shaft 37 and ensures tightness between them.

INDUSTRIAL APPLICABILITY RLD + ROTATION STABILIZER - no analogues found. The purpose of the rotation stabilizer is a way to ensure stable and uniform rotation around the circumference of several elements in which the center of mass of rotation does not coincide with the center of the axis of rotation (imbalances), and as a result, the angular moment of rotation around the circumference is not balanced, creating an increased load on the operation of the device.

The technical result of the present invention is to ensure stable rotation, that is, to distribute a variable rotational moment around a circle - by accumulating braking energy of rotation by springs and / or other compressing (bending) elements that are capable of accelerating an alternating torque, to give this energy by unloading (straightening, extension ) thereby contributing to a stable moment of rotation around the circle.

The constructive and technical problems to be solved by the invention are as follows: to facilitate the distribution of inertial forces during rotation around the circumference of elements in which the rotation mass does not coincide with the axis around which they rotate; distribution of a variable moment of rotation around a circle for stable rotation and reduction of loads on device parts; as a result, eliminate vibration during operation of the device; as a result, it is more economical to use the device: due to reduced loads on the parts, reduced wear; as well as reducing loads on external elements - foundation, skeleton, frame and so on; ensuring stable rotation contributes to the development of a large inertial force of the device parts, which can be used as additional energy (battery charging, acceleration during short braking, stops)

Option 13 - The method of stabilization of rotation - compression of the springs, figure 24:

Description of the method of stabilization of rotation - compression of the springs: on the dump 2 on bearings-1 7 the walls of the chambers 6 rotate; the walls of the chambers 6 are connected by compressing / expanding springs-1 62: one end into one wall of the chamber 6, the other is fixed to the adjacent wall of the chamber 6; the option is considered when the walls of the chambers 6 are identical in mass and radius from the axis of rotation, that is, the imbalances are the same; the springs-1 62 fixed between them, forming a rotation stabilizer, are the same (in terms of compression / tension) and therefore under their influence the distance between the walls of the chambers 6 is the same - the position is symmetrical, figure 24, top diagram; in case of violation of the symmetry of the arrangement of the walls of the chambers 6, the springs are compressed in the sector of decreasing distance and are unclenched in the sector of the circle where the distance between the walls of the chambers 6 has increased, figure 24, the lower diagram, the position of the springs-1 62 (forming a rotation stabilizer) - different in compression / tension.

INDUSTRIAL APPLICABILITY of the RLD and the features of Option 13 The method of stabilization of rotation is compression of the springs, figure 24: when rotating the walls of the chambers 6 located on the second the shaft 2, the spring-1 62 seeks to maintain the distance between the walls of the chambers 6 at the same distance (figure 24); in cases of violation of the symmetry of rotation - in the sector where the distance decreased, the spring compressed (received compression energy), and in the sector where the distance between the walls of the chambers 6 increased - the spring opened (received tensile energy), in this case: in the first compression case, the spring at one end receives the braking energy from the wall of the chamber 6 and accumulates this energy by its compression, and rests against the adjacent wall of the chamber 6 with the other end and presses with the potential (i.e. accumulated) compression energy. When the wall of the chamber 6 reaches the acceleration sector, this potential energy acts; it helps accelerate the wall of the chamber 6 to the stage when the expansion of the spring has ended, that is, to a neutral state.

Then the stretching begins; in the second case of stretching, the spring is stretched by the wall of the chamber 6 at one end and at the same time, the spring being fixed by the other end to the adjacent wall of the chamber 6: it takes the energy of the acceleration of the wall of the chamber 6 by its stretching (accumulating energy by stretching) and pulls the neighboring chamber 6 giving the potential energy to the other end stretching, that is, contributes to the braking of the accelerated wall and gives this energy to accelerate the adjacent wall 6.

The result is: each wall of the chamber 6, when changing its symmetrical position, changes the state of the springs on the one hand and on the other hand; each wall of the chamber 6 is potentially held with decreasing angular acceleration and is pushed with increasing angular acceleration. The decrease and increase in acceleration is the angular acceleration when rotating in a symmetrical location when the state of the springs is neutral.

Thus, the non-uniformity of angular acceleration acting on the shaft, transmission to the rotation source with destructive variability, with the help of the rotation stabilizer (consisting of spring elements) and the rotation stabilization method, stabilizes and provides stable rotation.

Option 14 according to option 13, the method of stabilization of rotation - bending springs, figure 25:

Description of the design of the method of stabilization of rotation by bending springs, diagram - figure 25: on the second shaft 2 is a bearing-1 7 to which bending springs-2 63 are symmetrically attached; bearing-1 7 rotates around the second shaft from the action of bending springs-2 63 fixed to it; bending springs-2 63 the second end is fixed to the wall of the chamber 6; the walls of the chambers 6 rotate around the second shaft 2 - unevenly; uneven rotation changes the symmetry of the wall of the chambers 6 and thereby bends the bending springs-2 63, as they are symmetrically located and fixed to the bearing-1 7; bending springs-2 63 are fixed to the wall of the chambers 6 with the second end, they act on the wall of the chambers 6 holding it to symmetry since they themselves are mounted symmetrically on the bearing.

INDUSTRIAL APPLICABILITY of RLD and features Option 14 according to option 13, Method for stabilizing rotation - bending springs, figures 25: in the sector of rotation of the chamber wall 6 with acceleration, bending springs-2 63 are bent in the direction of rotation being fixed at one end to the chamber wall 6, and the second end being fixed to bearing-1 7, pulls bearing-1 7 to rotate and rotate other bending springs-2 63 fixed to it, respectively the rest of the springs act on the walls of the chambers 6 respectively fixed to them. A freely rotating bearing-1 7 rotates in the position of the average angular rotation of all springs fixed to it under the influence of the springs, therefore, it is transmitted through the bearing-1 7 mu- lated bending / unbending energy of bending springs-2 63, the spring bending from the acceleration of the chamber wall 6 bends in the direction of rotation and causes the bearing-1 7 to rotate because of this, another bending spring-2 63 bends in the opposite direction to the behind chamber wall 6 contributing to it overclocking.

Option 15 according to option 13, the method of stabilization of rotation - bellows cameras, figure 26:

Description of the design of the method of stabilization of rotation - bellows cameras, diagram - figure 26; around the second shaft 2 the walls of the chamber 6 rotate on bearings-1 7; the walls of the chambers 6 are connected by springy bellows chambers 64 which perform the working process and / or are only springy rotation stabilization elements; springy bellows chambers 64 with the ability to spring compress / decompress accumulating and giving off the energy of uneven rotation around the circumference

INDUSTRIAL APPLICABILITY RLD and features Option 15 according to option 13, Method for stabilizing rotation with bellows chambers, figure 26: springy bellows chambers 64 are inserted from the side of the walls of chambers 6, subject to centrifugal force to be removed in the direction of increasing radius, and abut against stops 65 on the walls chambers 6 holding a springy bellows chamber 64 at the ends from a shift in the direction of increasing radius, and in the middle are held by spacers 66 having a hinge pin 67 providing holding the mass of the bellows chambers s to the radius and reducing the possibility of deformation of the geometric shape due to the flexibility of bending the spacers 66 into the hinge pin 67. In figure 26 a diagram of uneven rotation around the circumference. At the stages of decreasing the distance between the walls of the chambers 6, the compression energy is accumulated, and with increasing tension. Performing a method of stabilizing rotation similarly to option 13.

Option 16 according to option 13, the method of stabilization of rotation - springy containers, figure 27:

Description of the construction; method of stabilization of rotation — springy-containers — springy-containers; diagram — figures 27; the function of compression / tension with the transfer of accumulated energy to the walls of the chambers 6 rotating on the second shaft 2 on bearings-1 7 - perform springy tanks 68.

INDUSTRIAL APPLICABILITY of the RLD and the features of Option 16 according to option 13, the method of stabilizing rotation by springy containers, figure 27: when the symmetry of the position of the walls of the chambers 6 changes, the shape rotates around the circle and the shape changes accordingly changes and the internal pressure from which the effect on the walls of the chambers 6 is enhanced: during compression, repulsion of the walls of the chambers 6; when stretched, the walls of the chambers are pulled together 6. Being located in contact with the working chamber, in which high temperature increases the pressure inside the adherent containers 68, the interaction with the walls of the chambers 6 is enhanced.

Option 17 — RLD with bellows chambers and a spacer strut, FIG. 28, 29, 30:

Description of the design of variant 17 of the RLD in a static state (the location of the hinge 8 and the application zone 9 is not considered since the options for their location do not affect the operation of new parts of the RLD), the diagram is shown in figures 28, 29, 30: the second shaft 2 around which the chamber walls rotate 5 96; the wall of chamber-5 96 is divided into two separate working chambers: the first fire chamber 22 ^' and the second fire chamber 22 ^" ; each separate working chamber: the first fire chamber 22 ^' and the second fire chamber 22 ^" , has its own separate input / output (offset by direction of rotation) from the side of the housing for supplying and discharging the contents of the fire chambers 22 ^' , 22 ^" ; two adjacent walls of chambers-5 96 are connected by bellows chambers 19 ^' and 19 ^" , fixed to the chambers of fire 22 ^' , 22 ^" ; the bellows chamber 19 is divided into two separate parts - spacer 66, forming: the first bellows chambers 19 ^'and a second bellows chamber ^19'; the first bellows chamber 19 ^'is connected to the first ignition chamber 22 ^' ; the second bellows chamber 19 ^"is connected to the second ignition chamber 22 ^" ; a spacer 66 is attached to the second shaft 2, bearing 1 1 for rotation around the circumference of the second shaft 2 and holds the bellows chamber 19 when subjected to centrifugal force; a separating spacer 66 is fixed to the bearing-1 7 by a hinge pin 67 for free tilt behind the deforming bellows chamber 19 and further has another hinge pin 67 in the middle to prevent the bellows chamber 19 from bending from tilting the separating spacer 66 itself; the housing 13 has two contours of standardized channels, that is, the same holes on the thread for screwing different caps (interchangeable) depending on the functional purpose; channel for supplying fuel 15 ^' and 15 ^" ; channel for ignition 16 ^' and 16 ^" ; channel for supplying a mixture of high pressure 18 ^' and 18 ^" ; channel for discharging the spent mixture 17 ^' and 17 ^" ; the channels are duplicated for the ignition chamber 22 ^' and the ignition chamber 22 ^" since the operating cycles: fuel supply, ignition, supply of a high pressure mixture and emission of the spent mixture differ for the ignition chamber 22 ^' (which rotates around the front of the spacer 66) and the ignition chamber 22 ^" (which rotates around the circumference behind the spacer 66)

INDUSTRIAL APPLICABILITY of the RLD and the features of the variant 17 RLD with a bellows chamber 19 of the figure 28, 29, 30.

The previous schemes described options in which the working pressure occurs in a limited space, but not closed, the difference is that a certain percentage is lost during operation of the mechanism in the gaps between the working parts and the housing. To change these circumstances, it is proposed to arrange a bellows chamber 19 in the working chamber, the working volume is reduced, but the pressure will increase and tightness is ensured, and besides the useful pressure on the walls of the chambers, pressure is added to the walls of the forces of the phone chamber 19, which under the influence of pressure and straightening their walls are lengthened by adding additional working pressure to the walls of the chamber, and the power in the mechanism. Modern industry produces bellows products, including rotary (angular), with parameters: diameters from 40 mm to 1400 mm, pressure conditions from 0.1 to 2.5 Pa, resistant to aggressive environments. It remains only to successfully insert them between the walls of the chambers of this mechanism with the possibility of periodic replacement after running out of life, and since the bellows work during rotation, the entire load is in the direction of centrifugal force, so you need to insert it into the chamber wall from the side of the chamber wall.

Figure 28 - in this engine diagram, the high pressure mixture (combustible fuel and ignition) is supplied and the exhaust gases are discharged through the wall of the chamber-5 96. In the housing 13 there is a channel for supplying the high pressure mixture 18 which enters the bellows chamber 19 fixed to the wall chamber 6, under pressure, the bellows chamber 19 straightens increasing the distance between the walls of chambers-5 96 on which a hinge is attached acting through the application zone which is located on the rotor forcing it to rotate around the central shaft la After the expansion cycle, the bellows chamber 19 is compressed and the spent mixture is removed through the channel for ejecting the high pressure mixture 17. It is possible to use several bellows chambers connected at the junction by spacers 66 to maintain the shape and hold the camera from centrifugal force during rotation, without interfering with the free flow of volume from one chamber to another. Spacers 66 rotates around the second shaft 2 on the bearing-1 7 and are attached to the bearing freely to deflect the working forces of the camera, its purpose is to keep the bellows chambers 19 under centrifugal load. The mixture falling between the bellows chambers from the centrifugal force is discharged through the channels for ejecting the spent mixture 17.

Figure 29, cross section E ^* E ^" and figure 30, cross section E ^" E ^" - on the second shaft 2 static (or rotating around its axis), on the bearing-1 7 are separating spacers 66, mounted to the bearing-1 7 and having two pivot pins 67, which allows them to be deflected in the plane of rotation. The separating spacer 66 prevents centrifugal force and divides the bellows chambers 19 into two separate bellows chambers 19 ^' and 19 ^" , while minimizing the deformation of the bellows chambers 19 and thanks to the two pivot pins 67 19 ^' . The wall of chamber-5 96 has two separate ignition chambers 22 ^' and 22 ^", respectively, for the bellows chamber 19 ^' and 19 ^" .

Fuel supply in the ignition chambers 22 ^' and 22 ^" is fed through the fuel supply channels 15 located from the slopes in the direction of rotation of the chambers for more efficient fuel supply. In the housing for increasing power there are several channels for supplying fuel 15 around the circumference. To ignite the fuel from the jet the nozzle is supplied already burning jet. The ability of the fuel supply channel 15 to feed an already burning jet stream as a jet the nozzle and the variation of the options for supplying a fuel or jet stream to the expanding bellows chambers 19 ^' and 19 ^"make it possible to ensure the supply of maximum pressure and ensure maximum useful work of the RLD.

When diesel fuel is supplied, ignition is excluded.

When in the divided bellows chambers 19 ^' and 19 ^" , high pressure mixtures are supplied throughout the sector while the chambers expand (until the moment compression begins).

Around the circumference on subsequent sectors, since the pressure in the bellows chambers 19 ^' and 19 ^" decreases as the pressure expands, the jet 24 is supplied from the jet nozzle to increase the pressure in the chambers and increase the useful work.

The volume outside the bellows chambers 19 and limited by the housing 13 can be used as the volume of the pump while cooling the bellows chambers 19.

Option 18 according to option 17 device RLD with bellows chambers and double separating spacers, figures 31:

Description of the design of embodiment 17: an RLD device with bellows chambers and double separating spacers: characterized in that: one more spacer 66 is added, which divides the bellows chamber 19 into three parts: the bellows chamber - 19 ^' ; bellows chamber (pump or cooling) - 19 ^" ; bellows chamber - 19 ^" ; Camera ignition 22 ^'and the chamber ignition 22 ^"is inserted into the spark plug ^113' and 113 ^'and the housing 13, bus power supply ^114' and ^114", respectively (transmission power of terminals in a similar conventional motor) every combustion chamber 22 ^'and the ignition chamber 22 ^" They have their own fuel and ignition system displaced along and around the circumference of the housing 13 to the sectors of the rotation circle corresponding to the cycle.

INDUSTRIAL APPLICABILITY of RLD and features Option 18 according to option 17 device RLD with bellows chambers and double separating spacers:

Features: the area between the two partitions makes it possible to constructively construct the volume of the working chamber without adding additional chamber walls while allocating minimal space for separating spacers having one common bearing on the shaft (second and / or third), as well as improving cooling of the working chamber, increasing the volume in options involving the use of the device as an additional function of the pump, in addition, an increase in the mass of rotating parts using a rotation stabilizer gives a greater The inertial power of the mechanism.

Option 19 to option 17 to option 6 - RLD with a bellows chamber with an offset focus (figure 32).

Description of the design of the RLD in a static state: the second shaft 2 around which the walls of the cameras-6 97 rotate; the wall of chamber-6 97 is divided into two separate working chambers by the partition of chambers 25 having an inclination: the first ignition chamber 22 ^' and the second ignition chamber 22 ^" ; the inclination of the partition of the chambers 25 is selected so that the angle of inclination contributes to an increase in the impact on the wall of the chamber-6 97 rotation (increasing the torque) and reduced impact on the wall of the chamber-6 97 against the course of rotation (increasing emphasis); the inclination of the septum of the chambers 25 is selected so that the angle of inclination facilitates combining the direction of the moment of rotation with the tangent wall of the chamber-6 97 (for increasing the moment of rotation), and on the opposite wall of the chamber-6 97 (against the direction of rotation) the angle of the direction of the moment of rotation deviates from the tangent rotation to strengthen the emphasis; the separation is offset so that the first ignition chamber 22 ^' along the rotation has a larger radius from the axis of rotation of the second shaft 2 (to increase the torque), and the second ignition chamber 22 ^" has a smaller radius from the axis of rotation of the second shaft 2 (to strengthen the stop) ; each separate ignition chamber: the first ignition chamber 22 ^' and the ignition chamber 22 ^" , has its own separate input / output (shifted in the direction of rotation) from the side of the housing for supplying and discharging the contents of the ignition chambers 22 ^' and 22 ^" ; two adjacent chamber walls - 6 97 joined forces iPhone cameras 19 fixed to the fire chambers 22 ^' and 22 ^" ; the bellows chamber 19 connects two adjacent walls of the chamber 6 that is, connects the first ignition chamber 22 ^' from one wall of the chamber-6 97 and the second ignition chamber 22 ^" from the adjacent wall of the chamber-6 97; a spacer 66 is attached to the second shaft 2, bearing -1 7 to rotate around the circumference of the second shaft 2 and holds the bellows chamber 19 when subjected to centrifugal force; the spacer 66 is fixed to the bearing-1 7 by an articulated finger 67 for free tilt behind the deforming bellows chamber 19 and additionally has another hinge th finger 67 in the middle to prevent the bellows chamber 19 from bending from tilting the separating strut 66 itself; the housing 13 has unified channels, that is, identical holes on the thread for screwing different caps (interchangeable) depending on the functional purpose; fuel supply channel 15; channel for ignition 16; a channel for supplying a high-pressure mixture 18; a channel for discharging the spent mixture 17; supplying fuel, igniting the fuel, supplying a high-pressure mixture and then discharging the spent mixture is carried out only and h of the working chamber 22 ^' , the ejection channel occurs in the sector of combining the working chamber 22 ^' and the channel for ejecting the spent mixture 17

INDUSTRIAL APPLICABILITY of the RLD and the features of Option 19 according to version 17 of the RLD with a bellows chamber 19 with an offset emphasis (figure 32).

At the beginning of the description of the invention, "The rotational dynamics diagram of the rotor 5 (figure 3)," it was noted that: "The magnitude of the created torques 11 and 1 G depends on the arm 12 and 12 ^{'of the} application (the distance from the point of influence of the working pressure 10 and 10 ^' to the stop point in hinges 8 and 8 ^' ).

Having the design of the RLD with a bellows-type working chamber 19, it is possible to constructively lay the shoulder of pressure application for more efficient operation of the RLD. To this end, the emphasis of the bellows chamber 19 on the wall of the chamber-6 97 (opposite to that which performs the useful work of rotation) is shifted closer to the axis of rotation around the second shaft and the angle of the plane of the stop changes. The greater the difference between the maximum and minimum torques created by two opposite walls of the cameras-6 97 - the more efficient the engine. Option 20 for option 3 - RLD with a pressure supply through the second shaft (figure 33).

Description of the design of the RLD in a static state: shaft-cavity-2 107 has a cavity 20 and channels for supplying a high-pressure mixture 18; the wall of the chamber-7 98 is divided into two separate working chambers by the partition of the chambers 25: the first pressure chamber 21 ^' and the second pressure chamber 21 ^" ; the wall of the chamber-7 98 has two peaks of the wall 28 on both sides at the base of rotation with the shaft-cavity-2 107 ; the canopies of the wall 28 are made in the form of a curved fork so that when superimposed they can be clothed on each other blocking the outlet of pressure through the channel for supplying the high-pressure mixture 18 in the sectors of the distant walls of the chambers-7 98 from each other, that is, increasing the distance between them; each pressure chamber: the first pressure chamber 21 ^' and the second pressure chamber 21 ^" , has its own separate exit (displaced in the direction of rotation) from the side of the housing to discharge the contents of the pressure chambers 2G and 21 ^" ; two adjacent walls of the chambers-7 98 are connected by bellows chambers 19, fixed to the chambers pressure 2G and 21 ^" ; the bellows chamber 19 connects two adjacent walls of the chamber-7 98, that is, it connects the first pressure chamber 2Got of one wall of the chamber-7 98 and the second pressure chamber 21 ^" from the adjacent wall of the chamber-7 98; the housing 13 has unified channels, i.e. the same openings threaded for screwing various lids (interchangeable) according to the functional purpose, a channel for discharging the spent mixture 17; emission waste mixture is carried out only from the pressure chamber 21 ^', for discharging channel occurs in the alignment chamber sector pRESSURE tions 21 ^'and the channel for discharging the spent mixture 17

Scheme: shaft-cavity-2 107 having an internal cavity 20, with a high-pressure mixture supply channel 18 for supplying a high-pressure mixture to the pressure chambers 21 ^' and 21 ^" (into the walls of the chambers-7 98), the RLD case 13 having channels for exhausting the spent mixtures 17.

INDUSTRIAL APPLICABILITY of RLD: pressure is supplied from the external source to the cavity 20 of the shaft-cavity-2 107, which through the channel of the high-pressure shaft 18 enters the pressure chambers 2G and 21 ^" of the chamber wall-7 98, then to the bellows chamber 19, under pressure on the walls chamber-7 98 and rectifying bellows chambers 19 do useful work. When the walls of chambers-7 98 come closer from compression and under the influence of centrifugal force through the channel for ejecting the spent mixture 17, the mixture is removed. The walls of chambers-7 98 have visors of the wall 28 on both sides overlapping at n iblizhenii with neighboring peaks chamber wall 7-98 to prevent the working pressure output of the second shaft 2 when rosstoyanie cavity between the walls 7-chambers 98 increases.

The position of two adjacent walls of the chambers-798 (figure 33, the node Ж-Ж and the node Ж ^' -Ж ^' ) when the distance between the visors of the wall 28 is equal to the distance of coincidence of the teeth of the visor is; while decreasing the distance of two adjacent walls of chambers-7 98 by the beginning of the sector of the feed channel of the high-pressure mixture 18 ^' ; the teeth approach - intersect - overlap - close (all this happens at the beginning of the sector of the supply channel of the high-pressure mixture 18 ^' - and closes the outlet of the high-pressure mixture from the cavity 20 into the free space between the walls of the chambers-7 98) (figure 33, node Ж ^' - G ^' ); by increasing the distance of two adjacent walls chambers-7 98 - the end of the sector of the feed channel of the high pressure mixture 18; the teeth move apart, the gap between the walls of the chambers-7 98 expands, but the open sector of the high-pressure mixture supply channel 18 has already ended (figure 33, unit Ж-Ж).

Option 21 device RLD-sealed with bellows chambers having bellows hoses for supplying and discharging the mixture, figures 34, 35, 36; section 3-3, II node:

Design description Option 21 RLD-tight device with bellows chambers having bellows supply and exhaust hoses - figures 34, 35, 36; section 3-3, II; walls of chambers-8 99 divided into two separate pressure chambers 21 ^' and 21 ^" and connected by bellows chambers 19; bellows chambers 19 are held by struts 66, which are mounted on bearings-1 7; walls of chambers 6 are connected by a stabilizer of rotation from bending springs-2 63; the second shaft 2 rotates on the sealed bearing of the second shaft 35 in the housing 13; in the housing 13 on the second shaft 2 there is a sealed bearing of the second shaft 35 on which one end of the bellows hose for supplying the high pressure mixture 32 is inserted into the channel for supplying the mixture pressure 18; the bellows hose for high pressure mixture 32 is clamped on the other hand by the sealed bellows hose bearing 33; on the sealed bellows hose 33 there is a bellows hose for discharging the spent mixture 34 which enters the channel for discharging the spent mixture 17 and is clamped on top of the sealed bellows waste hose 31; high pressure mixture bellows hose 32 (sandwiched between the sealed second shaft bearing 35 and the sealed bellows hose bearing 33) - method rotate on the circumference of the second shaft 2; a bellows hose for discharging the spent mixture 34 (sandwiched between the sealed bearing of the bellows hose 33 and the sealed bearing of the bellows hose of the spent mixture 31) is able to rotate around the circumference of the second shaft 2; high pressure mixture bellows hose 32 and spent mixture discharge hose 34 having pressure supply valves 29 and exhaust mixture discharge valve 30 - are connected to the second end by pressure chambers 2G and 21 ^" ; pressure supply valves 29 and exhaust valve 30 are regulated by a disk - valves 36 fixed together with the channel for supplying the high pressure mixture 18 and the channel for ejecting the spent mixture 17 in the housing 13, with the adjustment of the open sectors for supplying the mixture of high pressure 26 and the sector for the channel for ejection nerd mixture 27.

INDUSTRIAL APPLICABILITY of RLD and features Option 21 RLD-sealed device with bellows chambers having bellows supply and exhaust hoses, figures 33, 34; section 3-3, II assembly: the high-pressure mixture is fed through the channel for supplying the high-pressure mixture 18, on the valve disc 36 the cut sectors for supplying the high-pressure mixture 26 passes pressure to the rotating pressure-supply valves 29 during the registration period. During this period, the pressure through the bellows hose to supply the high pressure mixture 32 enters the pressure chamber 21 ^" and then into the bellows chamber 19. The working volume is filled with a high pressure mixture including the volume of the pressure chamber 21 ^' which is connected to the bellows hose exhaust mixture 34 having an exhaust valve 30, but closed since the same period (sector for the exhaust channel 27 on the valve disc 36 is closed). There is a working process of expanding the working chambers, the pressure on the walls of the chambers-8 99, that is, the rotation around the circumference of the second shaft 2. The bellows hose for supplying the high pressure mixture 32 and the bellows hose for ejecting the spent mixture 34 connected at one end to the chamber walls rotate behind it and their rigidity pulls the second end to rotate around a second shaft: a sealed bearing of the second shaft 35, a sealed bellows hose of the spent mixture 31 and a sealed bellows hose bearing 33. Inertia of mass of rotation and center tachometric force these masses rotate and causes the second shaft 2. On the rotary shaft of the second chamber walls 2-8 99 periodically accelerated or tormozat in this periodicity bellows hoses operate simultaneously rotating stabilizer function, ie:

- when braking, they bend, accumulating acceleration;

- during acceleration, they straighten out giving the accumulated energy.

During the period of reaching the volume compression sector, the sector on the valve disk 36 is combined: the exhaust valve 30 for the exhaust mixture with the sector for the exhaust channel 27, at the same time the sectors for supplying the high pressure mixture 26 are over. The spent mixture under compression of the working chambers and from centrifugal force is ejected through a bellows hose to discharge the spent mixture 34 and the channel for discharging the spent mixture 17.

The working cycle is over.

Features: the use of this option is expected in conditions of compliance with the tightness of the device and environmental protection from harmful emissions.

Option 22 var. 1 - RLD in which the working chamber is located inside the chamber wall and pressure is supplied from above from the housing, FIG. 36, 37, 38; node K, section L-L:

Description of the design of the RLD in a static state: a central shaft 1 is inserted into the housing 13, which is connected to an eccentric second shaft 2; on the central shaft 1, a rotor 5 rotates on which hinges 8 are fixed; hinges 8 are inserted into the application zone 9 located in the wall of the chamber-9 100; a bellows wall chamber 23 is inserted in the application zone 9; figure 36, node K: a bellows-shaped wall chamber 23 is fixed to the wall of the chamber-9 100 in a bellows stop 69 from the side of the housing 13, with an open entrance 70 for injection / discharge of the working mixture; with the opposite side, the bellows wall chamber 23 abuts against a rotationally fixed joint 8 located on the carriage 71 with the carriage bearings 72 resting on the spring carriage 73 against the walls of the application zone 9; channels for supplying fuel 15, a channel for ignition 16, and channels for discharging the spent mixture 17 are located in the housing

INDUSTRIAL APPLICABILITY RLD in which the working chamber is located inside the chamber wall and pressure is supplied from above from the housing:

Through the channel for supplying fuel 15 fuel is supplied to the open inlet 70 to the bellows wall chamber 23. Fuel is ignited through the ignition channel 16, pressure is created in bellows to the wall chamber 23, which is elongated and with support in the bellows stops 69, presses on the carriage 71 and the hinge 8. The hinge 8 tangentially presses on the wall of the chamber-9 100 forcing it to rotate around the second shaft 2, which is the emphasis at the same time rotates and the hinge 8 as an element clamped in the application zone 9 and being attached to the rotor 5 with the second end, forces the rotor 5 to rotate. A working process is ongoing.

Having reached the maximum radius, the bellows wall chamber 23 begins to compress. In this sector, on the housing 13 are valves for discharging the spent mixture 17. The pressure drops and idle, rotating the bellows chamber 19 is compressed to a minimum radius. The working cycle is over.

Features RLD in which the working chamber is located inside the chamber wall and pressure is supplied from above from the housing.

1) The application zone 9 and the bellows wall chamber 23 are at an angle from the line of passage of the radius of the circle of rotation to increase the angle of the tangent effect of the hinge 8 on the wall of the chamber 6, that is, to increase the efficiency of the RLD.

2) The volume between the walls of the chambers 6 can be used as a working chamber 14 of the pump.

3) The bellows-wall chamber 23 can be replaced by a piston-joint 74 - figure 40, assembly H and figure 44, assembly P: inside the chamber-9 wall 100, there are p-carriage-piston 75 joints connected to the carriage 84 on bearings carriages 72 resting on spring carriages 73.

Option 23 according to option 22, the RLD device, the working chamber inside the chamber wall (chamber wall-10 101) - supply from below from the housing, figures 39, 40:

Design description Option 23 according to option 22, the RLD device, the working chamber inside the chamber wall is a bottom feed from the housing, characterized in that: (figure 40, node MM), a piston-hinge 74 connected to the carriage 71 is connected to the application area 9 with hinge 8; in the area of the second shaft 2, at the level of the lower part, the pressure chamber 21, channels 13 for supplying fuel 15, a channel for ignition 16, and channels for discharging the spent mixture 17 are located in the housing 13

INDUSTRIAL APPLICABILITY RLD and features Option 23 according to option 22, RLD device working chamber inside the chamber wall (chamber walls-10 101) - supply from below from the housing: fuel is supplied through pressure channel 15 to pressure chamber 21, ignited through ignition channel 16 - is created the working pressure acting on the piston-joint 74 and which pushes the joint 8 displacing it along an increasing radius. The hinge 8 in this case presses tangentially against the wall of the chamber-10 101 which rotates around the second shaft 2. Based on the base of the pressure chamber 21, which rests on the second shaft 2, the hinge 8 is forced to rotate around the second shaft 2 and the rotor 5 is attached to it . Workflow in progress.

Having reached the maximum radius in the sector of the channel for the discharge of spent fuel 17, the pressure chamber 21 begins to decrease by squeezing the spent mixture from the working chamber. Having reached the minimum radius, the working cycle is completed. Features: the location of the fuel supply channels 15, the ignition channel 16 in the area with a small radius, where the linear speed is less, allows you to supply more fuel, increase the working chamber, respectively, and the power of the device.

Option 24 according to option 22 - RLD in which the bellows chamber is located inside the rotor and the pressure is supplied from above from the housing, figures 41, 42, 43, section 0-0:

Description of the design of the RLD in a static state: a central shaft 1 is inserted into the housing 13, which is connected to an eccentrically inserted second shaft 2; on the central shaft 1 rotor-3 102 rotates in which there are application zones 9; a bellows wall chamber 23 is inserted in the application zone 9; hinges 8 (the other end is inserted into the application zone 9) located in the wall of the chamber-2 89; the bellows-wall chamber 23 is fixed to the rotor-3 102 in the direction of the housing 13 with an open entrance for injection / discharge of the working mixture through standardized channels; the housing 13 has unified channels, that is, the same holes on the thread for screwing different caps (interchangeable) depending on the functional purpose; a channel for supplying fuel 15; channel for ignition 16; channel for supplying a mixture of high pressure; channel for discharging the spent mixture 17.

INDUSTRIAL APPLICABILITY RLD in which the bellows chamber is located inside the rotor and the pressure is supplied from above from the housing, figures 41, 42, 43, section 0-0:

Through the fuel supply channel 15, fuel is supplied to the bellows wall chamber 23. Fuel is ignited; pressure is created in the bellows wall chamber 23, which lengthens and presses on the hinge 8, increasing the shoulder acting on the wall of the application zone 9 (i.e., sinking rotor-3 102) - there is a torque of the rotor-3 102 rotating around the central shaft 1, the hinge 8 mounted on the wall of the camera-2 89 makes it rotate - there is a working process.

Features RLD in which the bellows chamber is located inside the rotor and the pressure is supplied from above from the housing, figures 41, 42, 43, section 0-0:

The application zone 9 and the bellows wall chamber 23 are at an angle from the line of passage of the radius of the circle of rotation to increase the efficiency of the RLD. The volume between the walls of the chambers-2 89 is used as a working chamber 14 of the pump.

Option 25, according to options 20, 23, the RLD device, the working chamber inside the rotor - supply from below from the shaft or housing, figures 44, 45, section П-П, unit Р, 46:

Design description Option 25 according to options 20, 23 RLD device working chamber inside the rotor - supply from below from a shaft or housing, figures 43, 44, 45; inside the rotor-4 103 rotating on the central shaft-2 109 are located the application zone 9; the application zone 9 forms a pressure chamber 21 in which the hinge-carriage-piston 75 through the hinge 8 interacts with the walls of the chambers-2 89 rotating on the second shaft 2; hinge-carriage-piston 75 consisting of: hinge 8, piston-hinge 74, carriage 71, carriage bearings 72 pressed by spring carriages 73 to prevent a dynamic impact on the wall of the application zone; in the central shaft 1 pass channels for supplying a high pressure mixture 18 and a channel for discharging the spent mixture 17; the pressure chamber 21 has an open channel from the side of the central shaft-2 109, which, when rotated around the circle, intersects with channels for supplying a high-pressure mixture 18 and channels for discharging the spent mixture 17; in the housing 13 there is a channel for supplying fuel 15 and a channel for ignition 16 and having an intersection with the open channel of the pressure chambers 21

INDUSTRIAL APPLICABILITY of RLD and features Option 25 according to options 20, 23 RLD device working chamber inside the rotor - supply from below from the shaft or housing: through the supply channel of the high pressure mixture 18 to the pressure chamber 21, the working pressure is formed which presses on the hinge-carriage-piston 75. The volume of the pressure chamber 21 under pressure expands with emphasis on the central shaft 1, shifts the hinge-carriage-piston 75 in the direction of the increasing radius of rotation around the central shaft and rotating the walls of the chambers-2 89 of the shaft-cavity-3 108 creates a torque turning chivaya rotor 103. There is a 4-operating rotation. Having reached the maximum radius, it intersects with the sector of the channel for the discharge of the spent working pressure 17. Under the pressure of the decreasing volume of the pressure chamber 21, the spent mixture is pushed out. In the minimum radius sector, the work cycle has ended.

Option: the fuel pressure 21 enters the chamber through the fuel supply channel 15, ignition from the ignition channel — a working pressure has formed. There is a working move. When reaching the maximum radius on the housing 13, the discharge channel of the working mixture begins. Under the pressure of the decreasing volume of the pressure chamber 21, the spent mixture is pushed out. In the minimum radius sector, the work cycle has ended.

Features: the RLD case does not have any details, this contributes to good streamlining. Work as a pump: from one end of a volume that draws in from the environment (air, water) and its subsequent repulsion through the opposite end provides silent traction. As a result, we have: a streamlined body and silent traction force, figure 46.

Option 26 of the hinge device for RLD, figure 47, node C:

Design description Variant 26 of the hinge device for RLD: on the rotor 5 on the bearing-4 76, the hinge 8 is fixed; the hinge 8 consists of: the axis of the bearings-hinges 77, on which the first-bearing-hinge 78 rotates, it is placed spring-1 80 on which the second-n bearing-hinge 79 is placed; the hinge 8 is inserted into the area of the application 9 and acts on the wall of the area of the application 9 having a spring-2 81 separating from the body of the wall of the chamber 6

INDUSTRIAL APPLICABILITY of the RLD and features Option 26 of the hinge device for the RLD, figure 47, node C: the wall of the chamber 6 rotates differently, therefore the impact of the application zone 9 on the hinge 8 is multidimensional and multidirectional. To exclude dynamic interactions (shock) between the device parts, compensating elements are provided; the body of the chamber wall 6 and the application zone 9 have a spring-2 81 gasket between them, which is a cross section of a corrugated sheet and a pressed metal sheet according to the material; the hinge 8 is in contact with the surface of the area of the application 9 through the second-bearing-hinge 79 which in diameter occupy half the width of the section of the area of the application and abuts against the same the second bearing is a hinge 79, thus in the housing the walls of the chamber are constantly in contact with surfaces to exclude dynamic shocks: spring-2 81 - the wall of the application zone 9; second-bearing-hinge 79 - the second-bearing-hinge 79 - the wall of the application zone 9 - spring -2 81; the second-bearing-hinge 79 rotates on the first-bearing-hinge 78 through a spring-1 80 in order to mitigate dynamic multi-accelerated and multi-directional workloads; rotation of the second-bearing-hinge 79 and unidirectional rotation of the first o-bearing-hinge 78 with it reduces the additional load on the device from the inertial masses of rotation of the bearings, since the angular velocity of one decreases due to the rotation of the second; the hinge 8 is mounted on the rotor 5 through the bearing-4 76 allowing it to rotate around its axis when working around the circumference of rotation of the rotor 5

Features: in options for changing the position of the hinge 8 and the application zone 9, from the rotor 5 to the wall of the chambers 6, the mitigating effect of the above elements is preserved. Thus, the wear of the parts is reduced, noise reduction is ensured and contributes to the efficiency of the device.

Option 27 of the device electro-RLD with an electric hinge, figures 48, 49, 50, 51.

Design Description Option 27 of an electro-RLD device with an electric hinge 24; on the rotor-5 104 are located the zone of application 9; in the area of application 9, the surrounding stator-electric coil 84 creates an electromagnetic field; electric current is supplied from the housing 13 to the rotor-5 104 in a standard manner as in an electric motor, the supply of electric current 86 to the rotor (figure 51) is located as close as possible to the axis of rotation of the rotor where the linear speed is less; in the application zone 9 is inserted, attached to the wall of the chamber-2 89, (through the bearing-4 76) an electric hinge 24, consisting of a carriage 71 with a hinged electromagnetic coil 85 on which current is supplied through the walls of the chambers-2 89 from the housing 13 by a standard in a manner similar to a rotor of an electric motor, the supply of electric current 87 to the walls of the chambers (figure 51) is located as close as possible to the axis of rotation of the chambers where the linear velocity is less; the carriage 71 is fixed to an electric hinge 24 rotating on a bearing-4 76 fixed to the wall of the chamber-2 89; the carriage 71 has bearings with a guide stop-groove 83 moving parallel to the guide groove-stop 82 mounted on the rotor-5 104

INDUSTRIAL APPLICABILITY of RLD and features Option 27 of an electric-RLD device with an electric hinge: from the housing 13, current is supplied to the rotor of electric current 86 through the stator-electric coil 84, where an electromagnetic field is created around the application zone 9 for interaction with the electromagnetic field created by the hinged electromagnetic winding 85, located around the carriage 71, which is fastened with an electric hinge 24 rotating on a bearing-7 76 mounted on the wall of the chamber-2 89. Carriages 71 are bearings with guides bearing stop-groove 83, moving parallel to the guide groove-stop 82 fixed to the rotor-5 104. The bearing with the guide stop-groove 83 is designed to prevent the stator-electric winding 84 from touching the hinged-electromagnetic winding 85, when they come together it abuts against the guide notch 82. Features: option 27 provides non-contact interaction of the electric hinge 24 and zone 9, which contributes to the high-speed operation of the device, the ability to use inert rotation by the same generator, silent operation according to the designation purpose, combine with the mechanical contours of the working chambers of the RLD-engine and RLD-pump.

Variant 28, according to variant 23, the RLD device, the working chamber inside the chamber wall — supply from below from the second shaft, figures 52, 53 (section Ф-Ф, unit X — overlapping of the visors of the chamber walls during rotation, (increased)):

Design description Variant 28 according to variant 23, the RLD device, the working chamber inside the chamber wall — supply from below from the second shaft: in the housing 13, a central shaft-3 111 is inserted connected to the shaft-cavity-4 110 inside of which there are: a channel for supplying a high-pressure mixture 18 and channel for discharging the spent mixture 17; the walls of the chambers-11 105 have visors-2 112 enveloping the shaft surface-cavity-4 110 and overlapping with the visors-2 112 of the adjacent chamber, since at each wall of the chambers-11 105 the visors-2 112 are offset from the visors-2 112 on one side on the other hand (figure 53, node X - overlay visors of the walls of the cameras during rotation, (increased)); in the walls of the chamber-11 105 there is an application zone 9 in which the bellows-wall chamber 23 is located, having a stop and an inlet channel for the mixture from the shaft-cavity-4 110 side, and with a second end abutting in the hinge 8; the hinge 8, interacting with the application zone 9 is rotationally-translationally mounted on the rotor 5, which rotates around the central shaft-3 111; the sector of the open channel for supplying the high-pressure mixture 18 coincides with the sector of increasing the radius of rotation of the hinge 8 relative to the axis of rotation of the shaft-cavity-4 110 and the same sector of increasing the volume of the bellows wall chamber 23; on the opposite side: in the sector of decreasing the radius of rotation of the hinge 8 relative to the axis of rotation of the shaft-cavity-4 110 and the same sector of decreasing the volume of the bellows wall chamber 23 - on the second shaft there is a sector of the channels for ejection of the spent mixture 17, which passes through the shaft-cavity-4 110 central shaft-3 111 on the opposite side (to create a pushing pull force, as an option)

Dynamics of operation and features. Option 28 according to option 23. RLD device; working chamber inside the chamber wall — supply from below from the second shaft, figures 52, 53 (cross-section Ф-Ф, unit X — overlapping visors of the chamber walls during rotation, (increased)): through the channel for supplying the high-pressure mixture 18, passing inside the shaft-cavity-4 110 and having open channels matching the channel for supplying the mixture to the bellows-wall chamber 23, which pushes the hinge 8 under pressure increasing its radius relative to the shaft-cavity-4 110. Hinge 8 presses against walls under pressure cu camera-11 105 in the application zone 9. With an emphasis, the expanding bellows-wall chamber 23 forces the hinge 8 to tangentially push toward increasing its radius of rotation relative to the shaft-cavity-4 110, being connected to the rotor 8, this forced rotation is transmitted to the rotor 5. Before increasing the maximum radius of the hinge 8 relative to the shaft-cavity-4 110, the pressure enters the bellows chamber from the feed channel of the high-pressure mixture 18. There is a working stroke. At the end of the stroke, begins to decrease the radius of rotation of the hinge 8 and it presses on the bellows-wall chamber 23 squeezing out the spent mixture. In this sector, channels for discharging the spent mixture 17 are located on the shaft-cavity-4 110 and the extruded volume through the shaft channel-cavity-4 110 passing through the central shaft-3 111 and the housing 13 is removed under pressure. The working cycle is over.

Features: work on this version of the RLD pump is identical without additional details.

Claims

FORMULA

Item 1. A rotary vane engine (RLD) containing hinges mounted on the walls of the chambers or on the rotor, working chambers in the form of accordions located between the walls of the chambers, while the axis of rotation of the rotor and the walls of the chambers are connected by a knee, characterized in that the axis of the central shaft on which the rotor rotates, as well as the rotating second shaft with an eccentric axis, have hinges which, through the application zones for the hinge, control the angle of rotation of the walls of the chambers and the volume of the working chambers formed between two adjacent walls of the chambers.

Paragraph 2. RLD according to claim 1, characterized in that the device has an odd number of working chambers, and the fuel supply and ignition of the fuel are not carried out sequentially in each chamber, and each function is performed through one working chamber neighboring in location.

Paragraph 3. RLD according to claim 1, characterized in that the channel for supplying the high pressure mixture to the working chamber passes through the central shaft and the second shaft.

Paragraph 4. RLD according to claim 1, characterized in that it has an additional central shaft with an additional rotor on which rotating through hinges are located interacting with the application areas, on both sides of the rotor, on the walls of the chambers of the adjacent Circuit of the Working Chambers, to ensure sealing between two adjacent The contours of the working chambers, the rotor may be larger in diameter for cutting into a housing niche or added an additional sealed-bearing at the same time providing additional emphasis to the long component shaft, to tory consists of a central shaft and second shafts.

Paragraph 5. RLD according to claim 4, characterized in that the hinges are fixed to the walls of the chamber-2, which rotate on the second shaft, and interact with the application zone, which is located on the rotor-2, rotating on the central shaft.

Paragraph 6. RLD according to claim 1, characterized in that the power rod, with the quality of the propulsion device, comes from a differently accelerated rotation of the walls of the chambers of the third shaft around the eccentric third shaft and from differently accelerated rotation of the walls of the chambers-3 around the eccentric second shaft, which are connected eccentrically with the central shaft and the rotation of the walls of the chambers is transmitted from the interaction of the hinges to the application areas of these chamber walls.

Paragraph 7. RLD according to claim 6, with the quality of the propulsion device characterized in that imbalances are attached to the walls of the cameras that change the rotation path in a plane perpendicular to the direction of rotation around this circle and thereby change the radius of rotation of the imbalances around the circle.

Paragraph 8. RLD according to claim 4, characterized in that the transmission method from variable angular rotation to constant angular rotation, or vice versa, is carried out from the central shaft-2 having an eccentric central shaft, which by its rotation controls the distance of the axis of rotation of the second shaft-2 having an eccentric second shaft designed to control the rotation distance of the axis of rotation of the third-shaft-2, and consisting of a rotor rotating on a central shaft, wall-chambers-4 rotating around a second-shaft-2 and wall-chambers-third shaft-2 rotating around a third-shaft-2, which rotate around each other to rotate around their axes translational hinges on the areas of application of the walls of the chambers.

Clause 9. RLD according to claim 8, characterized in that the transmission method is carried out by changing the shape of the chamber wall and / or the shape of the application zone.

Paragraph 10. RLD according to claim 8, characterized in that the transmission method is carried out through hinges transmitting rotation around a circle connected to hinges receiving this rotation through a rod, while the rotation of these hinges is 360 ° rotationally unidirectional.

Paragraph 11. RLD according to claim 10, characterized in that the transmission method is carried out through hinges transmitting rotation around the circumference connected to hinges receiving this rotation through the rod, while the rotation of these hinges around the circumference is rotationally differently directed, up to 180 ° in one direction then in the opposite direction direction.

Paragraph 12. RLD according to claim 10, characterized in that the transmission method is carried out through the hinges of the walls of the cameras interacting with each other to transmit rotational movement around the circumference and connected by a rod located in a rotating sealed disk inserted into a rotating partition, which ensures tightness in the housing between the contour of the working chambers the second shaft and the contour of the working chambers of the third shaft.

Paragraph 13. RLD according to claim 1, characterized in that the method of stabilizing rotation is carried out by springs-1 fixed between two adjacent walls of the chambers, similarly and symmetrically with fixed springs-1 between other adjacent walls of the chambers rotating in the same circle.

Paragraph 14. RLD according to claim 13, characterized in that the method of stabilizing rotation carries out bending springs-2 by fastening one end to the same bearing rotating around the same shaft as the walls of the chambers to which the second end of bending springs-2 is fixed.

Clause 15. RLD according to Claim 13, characterized in that the rotation stabilization method is carried out by springy bellows chambers fixed between two adjacent chamber walls during non-uniform rotation around the circumference by their compression-tension accumulate-give off a variable torque.

Paragraph 16. RLD according to claim 13, characterized in that the method for stabilizing rotation is carried out through spring containers of the same shape, which are in contact with the working chambers.

Clause 17. RLD according to claim 1, characterized in that the device has a bellows chamber fixed between two adjacent walls of chambers-5 and is divided into two separate working chambers by one holding spacer rotating on the second shaft.

Clause 18. RLD according to claim 17, characterized in that the bellows chamber fixed between two adjacent walls of the chambers-5 is divided by two holding struts into three parts, two parts carry out the working process through the walls of the chambers-5 and the middle part performing the working process between these walls of the chambers-5, and also a spark plug is inserted into the ignition chambers.

Paragraph 19. RLD according to claim 17, characterized in that the bellows chamber located between two adjacent walls of the chambers-6, is fixed to that wall of the chamber-6, which is opposite to the direction of the working rotation around a circle with a smaller radius from the axis of rotation of the second shaft, than fastening to the second wall of the chamber-6, which actually performs this working rotation around the circumference around the axis of the second shaft.

Paragraph 20. RLD according to claim 3, characterized in that the shaft-cavity-2 has a cavity for supplying working pressure to the power of the camera through the wall of the chamber-7 having visors of the wall overlapping with the visors of the wall adjacent to the wall of the chamber-7 superimposed at the beginning of the channel sector high pressure mixture supply, and the channel for supplying high pressure mixture moving away at the end of the open sector.

Clause 21. RLD according to claim 17, characterized in that the high-pressure mixture is supplied and subsequently ejected through sealed corresponding bellows hoses rotating in a circle on the second shaft in compliance with the tightness of the device.

Paragraph 22. RLD according to claim 1, characterized in that the bellows wall chamber is fixed to the wall of chamber-9 against the stops on the side of the casing with an open entrance for injection / discharge of the working mixture, and with the opposite side the bellows wall chamber abuts against a rotary-translational hinge abutting against the walls of the application zone, while the application zone and the bellows wall chamber are at an angle from the line of passage of the radius of the circle of rotation, and also, the bellows wall chamber can be replaced by a hinge piston inside the wall of the chamber-9, at The volume between the walls of the chambers can be used as a working chamber of the pump.

Paragraph 23. RLD according to Claim 22, characterized in that in the zone of the second shaft, at the level of the lower part, there is a pressure chamber and channels for supplying fuel, a channel for ignition and channels for discharging the spent mixture in the housing.

Paragraph 24. RLD according to claim 22, characterized in that the bellows wall chamber is located inside the area of application of the rotor-3 rotating around the central shaft, and the hinge interacting with the bellows wall chamber is fixed to the wall of the chamber-2.

Paragraph 25. RLD according to claim 24, characterized in that inside the rotor-4, rotating on the central shaft-2, there are application areas that form a pressure chamber in which the hinge interacts with the walls of the chambers-2 rotating on the second shaft, in the central shaft -2 pass channels for supplying a high-pressure mixture and a channel for discharging the spent mixture, the pressure chamber has an open channel from the side of the central shaft-2, and in the case there is a channel for supplying fuel and a channel for ignition and having an intersection with the open channel of the chambers yes Lenia and / or working in the pump function from one end of the central shaft 2 retractor volume from the environment and its subsequent repulsion shaft through-cavity 3 provided silent traction. Paragraph 26. RLD according to claim 1, characterized in that the hinge consists of an axis of bearings-hinge, on which the first-bearing-hinge rotates, it springs-1 on which the second-bearing-hinge is placed, the hinge is inserted into the application area and acts on the wall of the application zone having a spring-2 separating from the body of the chamber wall.

Paragraph 27. RLD according to claim 5, characterized in that on the rotor-5 there is an application zone with its surrounding stator-electric coil to create an electromagnetic field, an electric hinge consisting of a carriage attached to the wall of the camera-2 is inserted, which interact with the application area through an electromagnetic field providing non-contact interaction.

Paragraph 28. RLD according to claim 23, characterized in that the shaft-cavity-4 has a channel for supplying a high-pressure mixture and an exhaust channel for exhausting the mixture, and the walls of the chambers-11 have visors-2 enveloping the surface of the shaft-cavity-4 and overlapping with visors -2 of the adjacent chamber, in addition, a channel for supplying a high-pressure mixture passing inside the shaft-cavity-4, as well as exhaust channels for the spent mixture, which passes through the shaft-cavity-4 into the central shaft-3 from the opposite side, to create pushing traction force.