CN214356638U - Speed selecting mechanism of propeller speed regulator - Google Patents

Abstract

The utility model discloses a speed selecting mechanism of a propeller speed regulator, wherein the upper part of a speed selecting and stopping component is sleeved between a speed selecting handle and the upper part of a reducing screw shaft; the outer end of the large cylinder at the upper end of the upper shell component is sleeved with a reset torsion spring; the tapered part at the middle lower part of the reducing screw shaft is assembled in the inner hole of the upper spring seat in an interference manner; a lower spring seat is arranged on the upper end surface of the valve core; the diameter-thickened lower end of the reducing screw shaft is positioned below the bottom surface of the insert, and the spring fixed on the upper spring seat and the lower spring seat penetrates through the reducing screw shaft; the valve core is arranged in the valve sleeve, and a bearing with a centrifugal block hook end butted on a boss on the bottom surface of the valve core is assembled in a gap on the valve core on the lower end surface of the valve cap; a convex shoulder is arranged on the outer circle of the valve core, and an oil groove I and an oil groove II are arranged on the outer circle of the valve core above and below the convex shoulder; and the valve sleeve is provided with a high-pressure oil inlet and a high-pressure oil outlet which are communicated with the oil groove I and an oil return port which is communicated with the oil groove II. Use the utility model discloses a screw rotational speed is stepless adjustable in certain extent, can guarantee reliable operation under the selected required screw rotational speed.

Description

Speed selecting mechanism of propeller speed regulator

Technical Field

The utility model relates to a screw speed regulator speed selection mechanism.

Background

The higher the rotating speed of the propeller is, the greater the generated thrust is, and the greater the thrust is required when the airplane takes off, and the less the thrust is required when the airplane flies in a cruise plane. The existing propeller speed regulators only have one balance rotating speed, and the rotating speed is the same as that of the existing propeller speed regulators when the existing propeller speed regulators are in constant balance rotating speed by balancing the centrifugal force of a balancing weight and the spring force, so that the existing propeller speed regulators cannot be selected, and the existing propeller speed regulators can stably and efficiently complete the takeoff task when the balance rotating speed is set to be higher under the condition of completing the takeoff task, so that an engine is not easily damaged; therefore, a proper balance rotating speed is selected according to the actual condition of the airplane, but no matter how, as long as the balance rotating speed meeting the take-off requirement can be met, a large amount of fuel oil is wasted during the cruise flight, so that the requirement that the propeller speed regulator which can select the speed and can realize the adjustable and controllable balance rotating speed is required to ensure that the thrust of the propeller is high when the airplane takes off and the thrust of the propeller is low when the airplane cruises flight. The flight of the airplane is ensured by adjusting the rotating speed and the blade angle of the propeller, the propeller only has one high-efficiency blade angle, the working efficiency of the propeller is lower when the propeller works in other blade angle states, the blade angle needs to be changed to absorb the power of an engine in order to keep the rotating speed of the propeller at a fixed rotating speed under the condition that the flight working condition is changed, the working efficiency of the propeller is lower, and in order to always maintain the working efficiency of the propeller at a higher efficiency, a speed-selectable controllable propeller speed regulator capable of realizing adjustable and controllable balance rotating speed is urgently needed to be researched so that the blade angle is always kept at the position of the high-efficiency blade angle.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the above-mentioned problem that exists among the prior art, provide a structure simple relatively, the installation is dismantled conveniently, has the optional speed, can realize the adjustable controllable screw speed regulator speed selection mechanism of balanced rotational speed, and the screw rotational speed that uses this speed selection mechanism is stepless adjustable in the certain limit, can guarantee reliable operation under the selected required screw rotational speed.

In order to achieve the above object, the technical solution of the present invention is: a speed selection mechanism of a propeller speed regulator comprises an upper shell assembly, a lower shell assembly, a bottom plate, a speed selection handle, a speed selection stop assembly, a reset torsion spring, a maximum speed stop piece, a feathering stop piece, a reducing screw shaft, an upper spring seat, a lower spring seat, a spring, a bearing, a centrifugal counterweight assembly, a valve sleeve, a valve core bonnet assembly and an inserting piece, wherein the reducing screw shaft, the upper spring seat, the lower spring seat, the spring, the bearing, the centrifugal counterweight assembly, the valve sleeve, the valve core bonnet assembly and the inserting piece are positioned in inner cavities of the upper shell assembly and the lower shell assembly; one end of the speed selection handle is provided with a spline hole, and the other end of the speed selection handle is provided with a connecting structure with the propeller rod; the upper part of the speed selection stop assembly is sleeved between a spline hole of the speed selection handle and the upper part of the reducing screw shaft, an external spline of the speed selection stop assembly is connected with an internal spline of the speed selection handle, an internal spline of the speed selection stop assembly is connected with an external spline of the upper part of the reducing screw shaft, and a limiting flanging is arranged on the internal spline; the maximum speed stop piece and the feathering stop piece are respectively fixed on two small cylinders on the upper end surface of the upper shell assembly; the outer end of the large cylinder at the upper end of the upper shell component is sleeved with a reset torsion spring of which the upper end is fixed on the speed selection stop component and the lower end is fixed on one small cylinder; the speed-selecting stop assembly limits the flanging to rotate between the maximum speed stop piece and the feathering stop piece; the upper part of the reducing screw shaft is sleeved and connected with a threaded hole formed in a large cylinder at the upper end of the upper shell assembly in a threaded sealing manner, and the thinned part at the middle lower part is assembled in an inner hole of the upper spring seat in an interference manner; the valve core and valve bonnet assembly comprises a valve core and a valve bonnet integrated with the upper end of the valve core, an integrated lower spring seat is arranged on the outer circle of the upper end surface of the valve core, a circle of groove is formed on the inner circle of the lower spring seat, and the inserting piece is arranged in the groove and connected with the inner circle key groove of the lower spring seat; the lower end part of the reducing screw shaft is sleeved in the insert in a micro-clearance manner, the lower end with the thickened diameter is positioned below the insert, and the springs fixed on the upper spring seat and the lower spring seat penetrate through the reducing screw shaft; the valve core of the valve core bonnet assembly is arranged in the valve sleeve, and a bearing with a bottom surface boss is assembled in a gap on the valve core on the lower end surface of the valve bonnet; the centrifugal counterweight component comprising a centrifugal block is positioned in an inner cavity at the upper end of the lower shell component, the lower end of the centrifugal counterweight component is clamped on an excircle at the upper end of the valve sleeve through a spline sleeve, and the hook end of the centrifugal block is abutted on a bottom boss of the bearing; the valve sleeve micro-gap is assembled in the mounting hole of the lower shell component, and the lower end of the valve sleeve micro-gap is provided with a connecting mechanism with an engine; a convex shoulder is arranged on the outer circle of the valve core, and an oil groove I and an oil groove II are arranged on the outer circle of the valve core above and below the convex shoulder; the valve sleeve is provided with a high-pressure oil inlet and a high-pressure oil outlet which are communicated with the oil groove I and an oil return port which is communicated with the oil groove II; when the propeller normally works at the selected balance rotating speed, the convex shoulder blocks the high-pressure oil outlet on the valve sleeve; when the rotating speed of the propeller is smaller than the selected balance rotating speed, the convex shoulder is arranged at the lower end of the high-pressure oil outlet, and the high-pressure oil outlet is communicated with the high-pressure oil inlet; when the rotating speed of the propeller is higher than the selected balance rotating speed, the convex shoulder is arranged at the upper end of the high-pressure oil outlet, and the high-pressure oil outlet is communicated with the oil return opening.

Further preferably, the peripheral wall of one end of the speed selecting handle with the internal spline hole is disconnected, a through hole and a threaded hole are formed in two end walls of the disconnected peripheral wall, and the through hole and the threaded hole are fixed together through a spherical cylindrical head screw I with a hole and a light spring washer I. This structure is easy to mount and dismount.

Further preferably, the peripheral wall of the speed selection stop assembly is broken, a through hole and a threaded hole are formed in two end walls of the broken peripheral wall, and the through hole and the threaded hole are fixed together through a spherical cylindrical head screw II with a hole and a light spring washer II. This structure is easy to mount and dismount.

Further preferably, the centrifugal weight component comprises a support, two centrifugal blocks and a spiral retainer ring which are distributed correspondingly; the lower end of the support is clamped on the excircle of the upper end part of the valve sleeve through a spline sleeve; two centrifugal blocks are assembled on the support through a shaft and a bearing clearance respectively, a circle of spiral retainer ring is clamped and fixed on the outer wall of the upper end of the support, and two ends of the shaft are abutted on the inner end wall of the spiral retainer ring; the hook end which is abutted on the boss at the bottom surface of the bearing is provided with an arc surface. The existence of spiral retaining ring makes the axle be difficult for deviating from, and structural reliability is high, and the circular arc face has reduced the friction of the bottom surface boss of bearing, has increased life.

Through the propeller shaft manipulation on the aircraft the utility model discloses an on speed selection handle, change reducing screw shaft position and then change the pressure volume of spring, can make the screw select to work under the balanced rotational speed of difference, the speed regulator is driven rotatoryly by the drive mechanism of engine, at this moment, the elasticity of spring and the centrifugal force of the rotatory production of centrifugal piece of centrifugal counterweight assembly exert the axial component on case valve cap subassembly and reach the balance, the shoulder of case just plugs up the lubricating oil circuit that leads to in the screw intracavity, makes it work under a balanced rotational speed. When the speed regulator exceeds the balance rotating speed, the centrifugal block is thrown upwards to overcome the elasticity of the spring to lift the valve core bonnet assembly, the high-pressure oil outlet is communicated with the oil return opening, high-pressure oil in the propeller cavity is divided into the low-pressure oil groove, the propeller pitch is increased, the load is increased, the rotating speed of the propeller is reduced until the valve core bonnet assembly descends, the axial component force of the elasticity of the spring and the centrifugal force is balanced, the rotating speed returns to the selected balance rotating speed, and the shoulder of the valve core blocks the lubricating oil path leading to the propeller cavity again. When the speed regulator is lower than the balance rotating speed, the spring elasticity overcomes the axial component force of the centrifugal block, the valve core bonnet assembly descends, the high-pressure oil outlet is communicated with the high-pressure oil inlet, high-pressure oil enters the propeller cavity, the propeller pitch is reduced, the load is reduced, the rotating speed of the propeller is increased until the valve core bonnet assembly ascends, the spring elasticity and the axial component force of the centrifugal force are balanced, the rotating speed returns to the selected balance rotating speed, and the oil path leading to the propeller cavity is blocked by the convex shoulder of the valve core again.

In a word, the utility model discloses the structure is simple relatively, and the installation is dismantled conveniently, has the optional speed, can realize that balanced rotational speed is adjustable controllable. Use the utility model discloses a screw rotational speed is stepless adjustable in certain extent, can guarantee reliable operation under the selected required screw rotational speed, makes the better safe and reliable of aircraft flight.

Drawings

FIG. 1 is a schematic view of the mounting structure of the present invention when the speed regulator is balancing the rotating speed;

FIG. 2 is a schematic view of the mounting structure of the present invention when the gear pump of the speed governor is not rotating at a high rotational speed;

FIG. 3 is a schematic view of the mounting structure of the present invention when the gear pump of the speed governor is not rotating at a lower rotational speed;

FIG. 4 is a top view of the governor of the present invention installed;

fig. 5 is a top view of the centrifugal weight assembly of the present invention.

Detailed Description

The invention is further described with reference to the accompanying drawings and specific embodiments.

As shown in fig. 1 to 5, the present embodiment includes upper and lower housing assemblies 1, 9, a bottom plate 16, a speed selection handle 3, a speed selection stop assembly 5, a return torsion spring 2, a maximum speed stop member 14, a feathering stop member 15, a variable diameter screw shaft 4 located in the inner cavities of the upper and lower housing assemblies 1, 9, upper and lower spring seats 13, 17, a spring 6, a bearing 7, a centrifugal weight assembly 8, a valve sleeve 10, a valve core bonnet assembly 11 and a tab 12. One end of the speed-selecting handle 3 is provided with a splined hole, and the other end is provided with a connecting structure with the propeller rod. Preferably, the speed-selecting handle 3 has a broken peripheral wall at one end with an internal spline hole, a through hole and a threaded hole are arranged on two end walls of the broken peripheral wall, and the through hole and the threaded hole are fixed together by a spherical cylindrical head screw I28 with a hole and a light spring washer I27. The upper part of the speed-selecting stop component 5 is sleeved between the splined hole of the speed-selecting handle 3 and the upper part of the reducing screw shaft 4, the external spline of the speed-selecting stop component is connected with the internal spline of the speed-selecting handle 5, the internal spline of the speed-selecting stop component is connected with the external spline of the upper part of the reducing screw shaft 4, and the speed-selecting stop component is provided with a limiting flanging. Preferably, the peripheral wall of the speed-selecting stop assembly 5 is broken, and a through hole and a threaded hole are formed in two end walls of the broken peripheral wall, and the two are fixed together by a spherical cap screw II 29 with a hole and a light spring washer II 30. The maximum speed stop piece 14 and the feathering stop piece 15 are respectively fixed on two small cylinders on the upper end surface of the upper shell assembly; the outer end of the big cylinder at the upper end of the upper shell component 1 is sleeved with a reset torsion spring 2, the upper end of which is fixed on the speed-selecting stop component 5, and the lower end of which is fixed on one of the small cylinders. The speed stop assembly 5 limits the turn-up from rotating between the maximum speed stop 14 and the feathering stop 15. The upper part of the reducing screw shaft 4 is sleeved and hermetically connected in a threaded hole formed in a large cylinder at the upper end of the upper shell assembly 1 by adopting a trapezoidal thread, and the thinning part of the middle lower part is in interference fit in an inner hole of the upper spring seat 13. The valve core and bonnet assembly 11 comprises a valve core 19 and a bonnet 18 integrated with the upper end of the valve core 19, an integrated lower spring seat 17 is arranged on the outer circle of the upper end face of the valve core 19, a circle of groove is formed on the inner circle of the lower spring seat 17, and the inserting piece 12 is arranged in the groove and connected with an inner circular key groove of the lower spring seat 17. The lower end of the valve housing 10 is provided with a spline connected with an output shaft of the engine. The lower end part of the reducing screw shaft 4 is sleeved in the insert 12 in a micro-clearance way, and the lower end with the thickened diameter is positioned below the insert 12. The spring 6 fixed on the upper and lower spring seats 13, 17 is threaded on the reducing screw shaft 4. The valve core 19 of the valve core bonnet assembly is arranged in the valve sleeve 10, and the bearing 7 with a bottom surface boss is arranged on the valve core 19 on the lower end surface of the valve bonnet 18 in a clearance mode. The centrifugal counterweight component 8 comprising a centrifugal block is positioned in the inner cavity at the upper end of the lower shell component 9, the lower end of the centrifugal counterweight component is clamped on the excircle at the upper end of the valve sleeve 10 through a spline sleeve, and the hook end of the centrifugal block is abutted on the bottom boss of the bearing 7. Preferably, the centrifugal weight assembly comprises a support 32, two centrifugal blocks 33 and a spiral retainer ring 31 which are distributed correspondingly; the lower end of the support 32 is clamped on the excircle of the upper end part of the valve sleeve 10 through a spline sleeve; two centrifugal blocks 33 are respectively assembled on a support 32 through a shaft 35, a bearing 36 and a gasket 34 in a clearance mode, a circle of spiral retainer ring 31 is fixedly clamped on the outer wall of the upper end of the support 32, and two ends of the shaft 35 are abutted to the inner end wall of the spiral retainer ring 31; the hook end which is abutted on the boss at the bottom surface of the bearing 7 is provided with an arc surface. The valve sleeve 10 is micro-gap fitted in the mounting hole of the lower housing assembly 9, and its lower end is splined to the engine. A convex shoulder 20 is arranged on the outer circle of the valve core 19, and an oil groove I22 and an oil groove II 24 are arranged on the outer circle of the valve core 19 above and below the convex shoulder 20. The valve housing 10 is provided with a high pressure oil inlet 26 communicated with the oil groove I22, a high pressure oil outlet 23 and an oil return 25 communicated with the oil groove II 24. When the propeller normally works at the selected balance rotating speed, the convex shoulder 20 blocks the high-pressure oil outlet 23 on the valve sleeve 10; when the rotating speed of the propeller is smaller than the selected balance rotating speed, the convex shoulder 20 is arranged at the lower end of the high-pressure oil outlet 23, the high-pressure oil outlet 23 is communicated with the high-pressure oil inlet 26, high-pressure oil is fed into the propeller, the rotating speed is increased, and the convex shoulder 20 blocks the high-pressure oil outlet 23 on the valve sleeve 10 until the propeller normally works at the selected balance rotating speed. When the rotating speed of the propeller is higher than the selected balance rotating speed, the convex shoulder 20 is arranged at the upper end of the high-pressure oil outlet 23, the high-pressure oil outlet 23 is communicated with the oil return port 25, the propeller returns oil, the rotating speed is reduced, and the convex shoulder 20 blocks the high-pressure oil outlet 23 on the valve sleeve 10 until the selected balance rotating speed is reached to normally work. And 21 is a high-pressure oil inlet hole in the lower housing assembly 9 communicated with the high-pressure oil inlet 26.

Naturally, the invention also relates to other embodiments, and those skilled in the art can make corresponding changes and modifications according to the invention without departing from the spirit and substance of the invention, and these corresponding changes and modifications should be considered as improvements in the equivalent technology, and fall within the scope of protection of the claims of the invention.

Claims (5)

1. A speed selection mechanism of a propeller speed regulator is characterized in that: the variable-diameter screw type speed-changing control device comprises an upper shell assembly, a lower shell assembly, a bottom plate, a speed-selecting handle, a speed-selecting stop assembly, a reset torsion spring, a maximum speed stop piece, a feathering stop piece, variable-diameter screw shafts, an upper spring seat, a lower spring seat, a spring, a bearing, a centrifugal counterweight assembly, a valve sleeve, a valve core bonnet assembly and an inserting piece, wherein the variable-diameter screw shafts, the upper spring seat, the lower spring seat, the spring, the bearing, the centrifugal counterweight assembly, the valve sleeve, the valve core bonnet assembly and the inserting piece are positioned in inner cavities of the upper shell assembly and the lower shell assembly; one end of the speed selection handle is provided with a spline hole, and the other end of the speed selection handle is provided with a connecting structure with the propeller rod; the upper part of the speed selection stop assembly is sleeved between a spline hole of the speed selection handle and the upper part of the reducing screw shaft, an external spline of the speed selection stop assembly is connected with an internal spline of the speed selection handle, an internal spline of the speed selection stop assembly is connected with an external spline of the upper part of the reducing screw shaft, and a limiting flanging is arranged on the internal spline; the maximum speed stop piece and the feathering stop piece are respectively fixed on two small cylinders on the upper end surface of the upper shell assembly; the outer end of the large cylinder at the upper end of the upper shell component is sleeved with a reset torsion spring of which the upper end is fixed on the speed selection stop component and the lower end is fixed on one small cylinder; the speed-selecting stop assembly limits the flanging to rotate between the maximum speed stop piece and the feathering stop piece; the upper part of the reducing screw shaft is sleeved and connected with a threaded hole formed in a large cylinder at the upper end of the upper shell assembly in a threaded sealing manner, and the thinned part at the middle lower part is assembled in an inner hole of the upper spring seat in an interference manner; the valve core and valve bonnet assembly comprises a valve core and a valve bonnet integrated with the upper end of the valve core, an integrated lower spring seat is arranged on the outer circle of the upper end surface of the valve core, a circle of groove is formed on the inner circle of the lower spring seat, and the inserting piece is arranged in the groove and connected with the inner circle key groove of the lower spring seat; the lower end part of the reducing screw shaft is sleeved in the insert in a micro-clearance manner, the lower end with the thickened diameter is positioned below the insert, and the springs fixed on the upper spring seat and the lower spring seat penetrate through the reducing screw shaft; the valve core of the valve core bonnet assembly is arranged in the valve sleeve, and a bearing with a bottom surface boss is assembled in a gap on the valve core on the lower end surface of the valve bonnet; the centrifugal counterweight component comprising a centrifugal block is positioned in an inner cavity at the upper end of the lower shell component, the lower end of the centrifugal counterweight component is clamped on an excircle at the upper end of the valve sleeve through a spline sleeve, and the hook end of the centrifugal block is abutted on a bottom boss of the bearing; the valve sleeve micro-gap is assembled in the mounting hole of the lower shell component, and the lower end of the valve sleeve micro-gap is provided with a connecting mechanism with an engine; a convex shoulder is arranged on the outer circle of the valve core, and an oil groove I and an oil groove II are arranged on the outer circle of the valve core above and below the convex shoulder; the valve sleeve is provided with a high-pressure oil inlet and a high-pressure oil outlet which are communicated with the oil groove I and an oil return port which is communicated with the oil groove II; when the propeller normally works at the selected balance rotating speed, the convex shoulder blocks the high-pressure oil outlet on the valve sleeve; when the rotating speed of the propeller is smaller than the selected balance rotating speed, the convex shoulder is arranged at the lower end of the high-pressure oil outlet, and the high-pressure oil outlet is communicated with the high-pressure oil inlet; when the rotating speed of the propeller is higher than the selected balance rotating speed, the convex shoulder is arranged at the upper end of the high-pressure oil outlet, and the high-pressure oil outlet is communicated with the oil return opening.

2. The propeller governor speed selection mechanism of claim 1, wherein: the peripheral wall of one end of the speed selecting handle with the internal spline hole is disconnected, a through hole and a threaded hole are formed in two end walls of the disconnected peripheral wall, and the through hole and the threaded hole are fixed together through a spherical cylindrical head screw I with a hole and a light spring washer I.

3. A propeller governor speed selection mechanism according to claim 1 or 2, characterized in that: the peripheral wall of the speed-selecting stop assembly is disconnected, a through hole and a threaded hole are formed in two end walls of the disconnected peripheral wall, and the two through holes and the threaded hole are fixed together through a spherical cylindrical head screw II with a hole and a light spring washer II.

4. The propeller governor speed selection mechanism of claim 3, wherein: the centrifugal counterweight component comprises a support, two centrifugal blocks and a spiral retainer ring which are correspondingly distributed; the lower end of the support is clamped on the excircle of the upper end part of the valve sleeve through a spline sleeve; two centrifugal blocks are assembled on the support through a shaft and a bearing clearance respectively, a circle of spiral retainer ring is clamped and fixed on the outer wall of the upper end of the support, and two ends of the shaft are abutted on the inner end wall of the spiral retainer ring; the hook end which is abutted on the boss at the bottom surface of the bearing is provided with an arc surface.

5. A propeller governor speed selection mechanism according to claim 1 or 2, characterized in that: the centrifugal counterweight component comprises a support, two centrifugal blocks and a spiral retainer ring which are correspondingly distributed; the lower end of the support is clamped on the excircle of the upper end part of the valve sleeve through a spline sleeve; two centrifugal blocks are assembled on the support through a shaft and a bearing clearance respectively, a circle of spiral retainer ring is clamped and fixed on the outer wall of the upper end of the support, and two ends of the shaft are abutted on the inner end wall of the spiral retainer ring; the hook end which is abutted on the boss at the bottom surface of the bearing is provided with an arc surface.

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