CN117048847B - Steering engine rudder shaft position detection device - Google Patents

Steering engine rudder shaft position detection device Download PDF

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Publication number
CN117048847B
CN117048847B CN202311316152.8A CN202311316152A CN117048847B CN 117048847 B CN117048847 B CN 117048847B CN 202311316152 A CN202311316152 A CN 202311316152A CN 117048847 B CN117048847 B CN 117048847B
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China
Prior art keywords
limiting
rod
movable
fixed
groove
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CN202311316152.8A
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CN117048847A (en
Inventor
汪义周
邹泽林
潘秀
刘洪元
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Aerospace Jiangnan Group Co ltd
Guizhou Aerospace Control Technology Co Ltd
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Aerospace Jiangnan Group Co ltd
Guizhou Aerospace Control Technology Co Ltd
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Priority to CN202311316152.8A priority Critical patent/CN117048847B/en
Publication of CN117048847A publication Critical patent/CN117048847A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60Testing or inspecting aircraft components or systems
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Abstract

The application relates to the technical field of steering engine detection, in particular to a steering engine rudder shaft position detection device. The device comprises a base component, a fixed inclined slide block, an adjusting screw component, a movable inclined slide block and a screw limiting component. One end of the fixed slider body is fixedly connected with one side surface of the base portion. A side of the fixed slider body is provided with an inclined fixed bevel. The first rod part and the second rod part of the adjusting screw assembly are sequentially connected. A side of the movable slider body is provided with an inclined movable inclined part. The inclination angle of the movable inclined part is the same as that of the fixed inclined part. At least a portion of the second shank is threadably coupled to the drive screw. The second limiting part is movably connected with the base part. The first limiting part limits the first rod part to move along the axial direction of the first rod part. The second limiting portion provides a lateral thrust to the first lever portion toward the fixed ramp portion. Therefore, the problem of how to conveniently and rapidly detect the position accuracy of the rudder shaft interface groove is solved.

Description

Steering engine rudder shaft position detection device
Technical Field
The application relates to the technical field of steering engine detection, in particular to a steering engine rudder shaft position detection device.
Background
The steering engine of the aircraft is a key actuating mechanism for controlling the steering surface (control surface) of the aircraft to rotate in an autopilot so as to realize posture transformation motions of pitching, yawing, rolling and the like of the posture of the aircraft. The steering engine is a high-precision servo mechanism and mainly comprises a steering body, a steering surface, a driving part, a transmission part, a controller and a sensor. The working principle is that the controller sends out a signal to start the steering engine driving part, the driving part transmits power to the control surface through the transmission part to enable the control surface to rotate, meanwhile, the sensor sends back a signal to the controller to judge whether the control surface reaches a designated position, and the controller further adjusts the position of the control surface based on the signal transmitted back by the sensor, so that the attitude transformation of the aircraft can be realized. The accuracy and the dynamic response quality of the flight track of the aircraft are directly determined by the performance of the steering engine, the transmission part of the steering engine is connected with one end of the control surface through the steering shaft interface groove, and the error between the instruction angle of the controller and the actual deflection angle of the control surface cannot be too large. Before delivery, the steering engine needs to detect whether a steering shaft interface groove of the steering engine accords with technical indexes.
For the detection of the technical indexes of the rudder shaft interface groove, a dial or an angle meter is often adopted for detection. The actual rotation angle of the rudder shaft interface is detected by the detection equipment, so that the problems of inconvenient operation, extremely low detection efficiency, extremely high detection cost and the like exist. In the steering engine, if the position accuracy of the rudder shaft interface groove is detected by using the dial, the dial accuracy is difficult to ensure and the data is difficult to read. If the angle measuring instrument is adopted for detection (namely, the angle of rotation of the rudder shaft interface is transmitted to the angle measuring instrument by the square shaft in clearance fit with the groove), the angle generated by the fit clearance between the interface groove and the transmission shaft is larger because the length of the rudder shaft interface groove is shorter, so that the angle detection error is unstable, and even exceeds the angle error.
Disclosure of Invention
In order to solve the problem of how to conveniently and rapidly detect the position accuracy of a rudder shaft interface groove, the application provides a steering engine rudder shaft position detection device, which comprises:
the base assembly comprises a base part and a screw rod matching hole; the screw fitting hole penetrates from one side of the base portion to the other side of the base portion;
the fixed inclined sliding block comprises a fixed sliding block body and a fixed inclined part; one end of the fixed slider body is fixedly connected with one side surface of the base part; the screw engagement hole penetrates from one side of the fixed slider body to the other side of the fixed slider body; the other end of the fixed slider body extends in a direction away from the base portion; a tilted fixed oblique part is arranged on one side surface of the fixed slider body;
the adjusting screw assembly comprises a first rod part, a second rod part, a first limit groove and a second limit groove; the first rod part and the second rod part are sequentially connected; the first limiting groove is arranged on the outer periphery side adjacent to one end, far away from the second rod part, of the first rod part; the second limiting groove is arranged on the outer peripheral side adjacent to one end, close to the second rod, of the first rod; at least part of the first rod part is in clearance fit with the screw rod matching hole;
the movable inclined slide block comprises a movable slide block body, a movable inclined part and a driving threaded part; a movable inclined part is arranged on one side surface of the movable sliding block body; the inclination angle of the movable inclined part is the same as that of the fixed inclined part; the movable inclined part and the fixed inclined part are mutually matched and abutted; the drive screw penetrates from one end of the movable slider body to the other end of the movable slider body; at least part of the second rod part is in threaded connection with the driving threaded part; the side moving direction of the movable inclined sliding block is perpendicular to the axis of the screw rod matching hole;
the screw limiting assembly comprises a first limiting part and a second limiting part; the first limiting part is movably connected with the base part; the second limiting part is movably connected with the base part; one end of the first limiting part is movably connected with the first limiting groove or the second limiting groove to limit the first rod part to move along the axial direction of the first rod part; the end part of the second limiting part is movably connected with the first limiting groove or the second limiting groove which is not movably connected with the first limiting part, and provides a lateral thrust to the first rod part, wherein the lateral thrust is close to the fixed inclined part;
the base assembly further comprises a planar positioning portion; the plane positioning part is arranged on one side surface of the base part; the steering engine rudder shaft position detection device further comprises an angle measuring instrument; the goniometer is abutted with the plane positioning part; the goniometer is detachably connected with the base portion.
In some embodiments, the first limiting portion includes a first limiting hole, a first limiting block; the first limiting hole penetrates into the screw rod matching hole from one side of the base part; the axis of the first limiting hole is perpendicular to the lateral movement direction of the movable inclined sliding block; the first limiting block is movably connected with the first limiting hole; one end of the first limiting block is abutted to the first limiting groove to limit the first rod part to move axially.
In some embodiments, the first limiting part comprises two first limiting holes and two first limiting blocks; the two first limiting holes are symmetrically arranged on two sides of the screw matching hole respectively; the two first limiting blocks are respectively and movably connected with the two first limiting holes; one ends of the two first limiting blocks are respectively abutted to the first limiting grooves to limit the first rod part to move along the axial direction of the first rod part.
In some embodiments, the second limiting portion includes a second limiting hole, a second limiting block; the second limiting hole penetrates into the screw rod matching hole from one side of the base part; the axis of the second limiting hole is parallel to the side moving direction of the movable inclined sliding block; the second limiting block is movably connected with the second limiting hole; one end of the second limiting block is abutted to the second limiting groove; the elastic component in the second limiting block provides elastic force to push one end of the second limiting block to provide lateral thrust to the first rod portion, and the lateral thrust is close to the fixed inclined portion.
In some embodiments, the fixed diagonal slider further comprises a flat chute; the smooth groove is arranged on one side of the fixed slider body close to the base part; the extending direction of the smooth groove is parallel to the lateral movement direction of the movable inclined sliding block; the movable inclined slide block further comprises a smooth part; the smooth part is fixedly connected with one end of the movable sliding block body; the smooth part is movably connected with the smooth groove and axially slides along the extending direction of the smooth groove and the second rod part.
In some embodiments, the movable ramp block further comprises a drive aperture; the driving hole penetrates from one side of the smooth part to the other side of the smooth part; the drive bore is concentric with the drive screw; at least a portion of the second stem portion is in clearance fit with the drive bore.
In some embodiments, the first stem portion comprises a first thick stem; the first thick rod is fixedly connected with the first thin rod; the first thick rod is arranged at one end of the first thin rod and one end of the first rod part, which is far away from the second rod part; the first thick rod diameter is greater than the first thin rod diameter; the first limit groove is arranged on the outer peripheral side of the first thick rod; the second limiting groove is arranged on the outer peripheral side adjacent to one end of the first thin rod, which is close to the second rod part; the screw rod matching holes comprise first matching holes and second matching holes; at least part of the first slender rod is arranged in the first matching hole; at least part of the first thick rod is arranged in the second matching hole.
In some embodiments, the second mating hole is elongated in cross-section; the width of the strip is in clearance fit with the outer diameter of the first thick rod; the length direction of the strip is parallel to the side moving direction of the movable inclined sliding block.
In some embodiments, the base assembly further comprises a weight-reducing channel; the weight reduction grooves are formed in two sides, away from the screw matching holes, of the base portion.
In some embodiments, the steering engine rudder shaft position detection device further comprises a platform assembly; the platform assembly is detachably connected with the steering engine to be detected; the movable inclined sliding block and the fixed inclined sliding block are in butt joint with the side wall of the rudder shaft interface groove of the steering engine to be detected; the base part is detachably connected with a rudder shaft of the steering engine to be detected.
In order to solve the problem of how to conveniently and rapidly detect the position accuracy of the rudder shaft interface groove, the application has the following advantages:
1. the square shaft of the rudder shaft position detecting device is arranged in a mode that a movable inclined slide block is combined with a fixed inclined slide block. When the movable inclined sliding block is driven by controlling the adjusting screw rod assembly, the movable inclined sliding block can slide along the inclined direction of the fixed inclined part of the fixed inclined sliding block, so that the width of the square shaft can be changed, and the opposite two side surfaces of the movable inclined sliding block and the fixed inclined sliding block can be clamped with the rudder shaft interface groove. Therefore, the operation is convenient and quick, and the efficiency of detecting the position accuracy of the rudder shaft interface groove is improved.
2. The first limiting part of the screw limiting assembly limits the first rod part of the adjusting screw assembly to axially move along the first rod part, and the second limiting part of the screw limiting assembly provides lateral thrust close to the fixed inclined part for the first rod part of the adjusting screw assembly, so that lateral pretightening force can be provided for the movable inclined sliding block, and the movable inclined sliding block is always attached to the fixed inclined sliding block. Meanwhile, the side movement of the adjusting screw assembly can be smooth, the movable inclined sliding block is driven by the adjusting screw assembly to move smoothly, and the efficiency of detecting the position accuracy of the rudder shaft interface groove is further improved.
Drawings
FIG. 1 shows a schematic diagram of a steering engine rudder shaft position detection device according to an embodiment;
FIG. 2 shows a schematic view of a portion of a steering engine rudder shaft position detection device according to an embodiment;
FIG. 3 shows a schematic view of a portion of a steering engine rudder shaft position detection device according to another embodiment;
FIG. 4 shows a schematic view of a portion of a steering engine rudder shaft position detection device according to another embodiment;
FIG. 5 shows a schematic view of a portion of a steering rudder shaft position detection device according to yet another embodiment;
FIG. 6 illustrates a schematic diagram of the combination of a base assembly, a screw stop assembly, and a fixed diagonal slider of one embodiment;
FIG. 7 shows a schematic diagram of a base assembly, screw stop assembly, fixed diagonal slide joint of another embodiment;
FIG. 8 illustrates a schematic diagram of a movable diagonal slider of an embodiment;
FIG. 9 shows a schematic view of another embodiment of a movable diagonal slider;
FIG. 10 illustrates a schematic view of an adjusting screw assembly of an embodiment;
FIG. 11 illustrates a schematic view of an adjusting screw assembly of another embodiment;
FIG. 12 illustrates a partial schematic view of a base assembly of one embodiment;
FIG. 13 illustrates a partial schematic view of a screw stop assembly of one embodiment.
Reference numerals: a platform assembly; 11 end face positioning parts; 12 circumferential positioning portions; a base assembly 02; a 21 base portion; 22 plane positioning parts; 23 weight reduction grooves; 24 screw rod matching holes; 241 first mating holes; 242 a second mating aperture; 03 screw limiting components; 31 a first limit part; 311 first limiting holes; 312 a first stopper; 32 second limit parts; 321 second limiting holes; a second limiting block 322; 04 adjusting screw assembly; 41 a first stem portion; 411 first thick bar; 412 a first thin rod; 42 a first limit groove; 43 a second lever portion; 44 a second limiting groove; 05, moving an inclined slide block; 51 a movable slider body; 52 movable ramp; a 53 smoothing section; 54 drive the threaded portion; 55 drive holes; 06 fixing an inclined slide block; 61 securing the slider body; 62 fixing the bevel; 63 a third limiting hole; 64 flat sliding grooves; 07 goniometer; 08 steering engine; 81 rudder shaft interface groove.
Detailed Description
The disclosure will now be discussed with reference to several exemplary embodiments. It should be understood that these embodiments are discussed only to enable those of ordinary skill in the art to better understand and thus practice the present disclosure, and are not meant to imply any limitation on the scope of the present disclosure.
As used herein, the term "comprising" and variants thereof are to be interpreted as meaning "including but not limited to" open-ended terms. The term "based on" is to be interpreted as "based at least in part on". The terms "one embodiment" and "an embodiment" are to be interpreted as "at least one embodiment. The term "another embodiment" is to be interpreted as "at least one other embodiment". The terms "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "vertical", "horizontal", "transverse", "longitudinal", etc. refer to an orientation or positional relationship based on that shown in the drawings. These terms are only used to better describe the present application and its embodiments and are not intended to limit the scope of the indicated devices, elements or components to the particular orientations or to configure and operate in the particular orientations. Also, some of the terms described above may be used to indicate other meanings in addition to orientation or positional relationships, for example, the term "upper" may also be used to indicate some sort of attachment or connection in some cases. The specific meaning of these terms in the present application will be understood by those of ordinary skill in the art according to the specific circumstances. Furthermore, the terms "mounted," "configured," "provided," "connected," and "connected" are to be construed broadly. For example, it may be a fixed connection, a removable connection, or a unitary construction; may be a mechanical connection, or an electrical connection; may be directly connected, or indirectly connected through intervening media, or may be in internal communication between two devices, elements, or components. The specific meaning of the above terms in the present application can be understood by those of ordinary skill in the art according to the specific circumstances. Furthermore, the terms "first," "second," and the like, are used primarily to distinguish between different devices, elements, or components (the particular species and configurations may be the same or different), and are not used to indicate or imply the relative importance and number of devices, elements, or components indicated. Unless otherwise indicated, the meaning of "a plurality" is two or more.
The embodiment discloses a steering engine 08 rudder shaft position detection device, as shown in fig. 3, fig. 4, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, may include:
a base assembly 02, the base assembly 02 comprising a base portion 21, a screw engagement hole 24; the screw engagement hole 24 penetrates from one side of the base portion 21 to the other side of the base portion 21;
a fixed diagonal slider 06, the fixed diagonal slider 06 comprising a fixed slider body 61, a fixed diagonal portion 62; one end of the fixed slider body 61 is fixedly connected to one side surface of the base portion 21; screw engagement holes 24 penetrate from one side of the fixed slider body 61 to the other side of the fixed slider body 61; the other end of the fixed slider body 61 extends in a direction away from the base portion 21; a fixed slider body 61 is provided with a fixed inclined portion 62 on one side surface thereof;
the adjusting screw assembly 04, wherein the adjusting screw assembly 04 comprises a first rod part 41, a second rod part 43, a first limit groove 42 and a second limit groove 44; the first lever portion 41 and the second lever portion 43 are connected in sequence; the first limiting groove 42 is provided on the outer peripheral side adjacent to one end of the first lever portion 41 away from the second lever portion 43; the second limit groove 44 is provided on the outer peripheral side adjacent to one end of the first lever portion 41 near the second lever portion 43; at least a portion of the first stem 41 is clearance fit with the screw engagement hole 24;
the movable inclined slide block 05, the movable inclined slide block 05 comprises a movable slide block body 51, a movable inclined part 52 and a driving threaded part 54; a movable inclined part 52 is provided on one side of the movable slider body 51; the movable inclined part 52 and the fixed inclined part 62 have the same inclination angle; the movable inclined part 52 and the fixed inclined part 62 are mutually matched and abutted; the drive screw 54 penetrates from one end of the movable slider body 51 to the other end of the movable slider body 51; at least part of the second rod portion 43 is threadedly coupled to the drive screw portion 54; the side moving direction of the movable inclined slide block 05 is vertical to the axis of the screw matching hole 24;
the screw limiting assembly 03 comprises a first limiting part 31 and a second limiting part 32; the first limiting part 31 is movably connected with the base part 21; the second limiting part 32 is movably connected with the base part 21; one end of the first limiting part 31 is movably connected with the first limiting groove 42 or the second limiting groove 44 to limit the axial movement of the first rod part 41; the end part of the second limiting part 32 is movably connected with the first limiting groove 42 or the second limiting groove 44 which is not movably connected with the first limiting part 31, and provides a lateral thrust to the first rod part 41, which is close to the fixed inclined part 62;
the base assembly 02 further includes a planar positioning portion 22; the plane positioning portion 22 is provided on one side surface of the base portion 21; the steering engine 08 rudder shaft position detection device also comprises an angle measuring instrument 07; the goniometer 07 abuts against the plane positioning portion 22; the goniometer 07 is detachably connected to the base portion 21.
In this embodiment, steering engine 08 is a device mounted on an aircraft that directs the flight of the aircraft. In the flight process of the aircraft, the control surface of the steering engine 08 rotates to realize the attitude transformation of pitching, yawing, rolling and the like of the aircraft. Because the quality of the performance of the steering engine 08 directly determines the flight track precision and the dynamic response quality of the aircraft, the transmission part of the steering engine 08 is connected with one end of the control surface through the rudder shaft interface groove 81, and the error between the instruction angle of the controller and the actual deflection angle of the control surface cannot be too large. Before delivery, the steering engine 08 needs to detect whether the steering engine 08 rudder shaft interface groove 81 meets technical indexes. As shown in fig. 3, the steering engine 08 rudder shaft position detecting device may include a base component 02, a screw limiting component 03, an adjusting screw component 04, a movable inclined slide block 05 and a fixed inclined slide block 06. As shown in fig. 6 and 7, the base member 02 may include a base portion 21 and a screw engagement hole 24. Screw mating holes 24 may be penetrated from one side of the base portion 21 to the other side of the base portion 21 to facilitate placement of the adjusting screw assembly 04. The fixed ramp block 06 may include a fixed slider body 61, a fixed ramp 62. One end of the fixed slider body 61 may be fixedly coupled to one side of the base portion 21. Screw mating holes 24 may pass through from one side of fixed slider body 61 to the other side of fixed slider body 61. The other end of the fixed slider body 61 may extend in a direction away from the base portion 21, and may have a length that matches the depth of the rudder shaft interface groove 81, so that the outer peripheral side thereof can be easily engaged with the rudder shaft interface groove 81. One side of the fixed slider body 61 may be provided with a slanted fixed slope 62 so that the movable slider can slide in a slanted direction of the fixed slope 62. As shown in fig. 4 and 10, the adjusting screw assembly 04 may include a first lever portion 41, a second lever portion 43, a first limit groove 42, and a second limit groove 44. The first lever portion 41 and the second lever portion 43 may be connected in sequence. The first stopper groove 42 may be provided at an outer peripheral side (i.e., a lower region of the first lever portion 41) adjacent to an end of the first lever portion 41 remote from the second lever portion 43. The second stopper groove 44 may be provided at an outer peripheral side (i.e., an upper region of the first lever portion 41) adjacent to an end of the first lever portion 41 near the second lever portion 43. At least part of the first rod part 41 can be in clearance fit with the screw rod matching hole 24, a certain side movement space can be provided for the adjusting screw rod assembly 04, and the adjusting screw rod assembly 04 can conveniently and smoothly move laterally when driving the movable inclined slide block 05 to move, so that the opposite two side surfaces of the movable inclined slide block 05 and the fixed inclined slide block 06 are clamped with the rudder shaft interface groove 81, and the rudder shaft position accuracy detection efficiency is improved. As shown in fig. 8 and 9, the movable ramp slider 05 may include a movable slider body 51, a movable ramp portion 52, and a driving screw portion 54. The movable slider body 51 may be provided with a sloped movable ramp 52 on a side opposite the fixed ramp 62. The inclination angle of the movable inclined part 52 can be the same as that of the fixed inclined part 62, and the inclination directions are opposite, and the movable inclined part 52 and the fixed inclined part 62 can be mutually matched and abutted, so that the movable inclined slide block 05 can slide smoothly along the inclination direction of the fixed inclined part 62. The side-shifting direction of the movable diagonal slider 05 may be perpendicular to the axis of the screw mating hole 24. The driving threaded portion 54 can penetrate from one end of the movable slider body 51 to the other end of the movable slider body 51, and at least part of the second rod portion 43 is in threaded connection with the driving threaded portion 54, so that the adjusting screw assembly 04 can drive the movable inclined slider 05 to move through threaded rotation and lateral movement, loosening and clamping of the movable inclined slider 05, the fixed inclined slider 06 and the rudder shaft interface groove 81 are achieved, and further efficiency of detecting position accuracy of the rudder shaft interface groove 81 can be improved. As shown in fig. 3 and 4, the screw limit assembly 03 may include a first limit portion 31 and a second limit portion 32. The first limiting portion 31 may be movably connected to the base portion 21, and the second limiting portion 32 may be movably connected to the base portion 21. The first limiting portion 31 may be a bolt or a positioning pin, and the second limiting portion 32 may be a spring or a ball screw.
One end of the first limiting part 31 can be movably connected with the first limiting groove 42, so that two side faces of one end of the first limiting part 31 are abutted against the side wall of the first limiting groove 42, and therefore the first rod part 41 is limited to move along the axial direction of the first rod part, the side movement of the adjusting screw assembly 04 is smooth, and smooth movement of the movable inclined sliding block 05 driven by the adjusting screw assembly 04 is ensured. The tip of second spacing portion 32 can with second spacing groove 44 swing joint, can make second spacing portion 32 one end and second spacing groove 44 butt, thereby can restrict first pole portion 41 and move along its axial while still can provide the side thrust that is close to towards fixed sloping portion 62 for first pole portion 41, and then can provide the side pre-tightening force to movable inclined slider 05, make movable inclined slider 05 and fixed inclined slider 06 laminate all the time, make adjusting screw subassembly 04 side shift more smoothly, the loosening and the block of drive movable inclined slider 05 more fast, fixed inclined slider 06 and rudder shaft interface groove 81, improve the efficiency of detecting rudder shaft interface groove 81 position precision.
One end of the first limiting part 31 can be movably connected with the second limiting groove 44, so that two side faces of one end of the first limiting part 31 are abutted against the side wall of the second limiting groove 44, the first rod part 41 is limited to move along the axial direction of the first rod part, the adjusting screw assembly 04 moves laterally more smoothly, and smooth movement of the movable inclined sliding block 05 driven by the adjusting screw assembly 04 is ensured. The tip of second spacing portion 32 still can with first spacing groove 42 swing joint, can make second spacing portion 32 one end and first spacing groove 42 butt, thereby can restrict first pole portion 41 and move along its axial, can still provide the side thrust that is close to towards fixed sloping portion 62 for first pole portion 41, and then can provide side pretightning force to movable inclined slider 05, make movable inclined slider 05 and fixed inclined slider 06 laminate all the time, make adjusting screw subassembly 04 side shift more smoothly, the loosening and the block of drive movable inclined slider 05 more fast, fixed inclined slider 06 and rudder shaft interface groove 81, improve the efficiency of detecting rudder shaft interface groove 81 position accuracy.
As shown in fig. 2, the base assembly 02 may also include a planar positioning portion 22. The plane positioning portion 22 may be provided at one side surface of the base portion 21. Steering engine 08 rudder shaft position detection device can also include goniometer 07. The goniometer 07 can be abutted with the plane positioning part 22, and the goniometer 07 can be detachably connected with the base part 21, so that the later maintenance and replacement of the goniometer 07 are facilitated. The goniometer 07 is used to detect the actual rotation angle of the rudder shaft interface slot 81.
In some embodiments, as shown in fig. 4 and 5, the first limiting portion 31 includes a first limiting hole 311 and a first limiting block 312; the first stopper hole 311 penetrates into the screw fitting hole 24 from the base portion 21 side; the axis of the first limiting hole 311 is perpendicular to the lateral movement direction of the movable inclined slide block 05; the first limiting block 312 is movably connected with the first limiting hole 311; one end of the first limiting block 312 abuts against the first limiting groove 42 to limit the first rod 41 to move along the axial direction.
In the present embodiment, as shown in fig. 4 and 5, the first limiting portion 31 may include a first limiting hole 311 and a first limiting block 312. The first stopper hole 311 may be provided from one side (left or right) of the base portion 21 into the screw fitting hole 24. The axis of the first limiting hole 311 (e.g., the left-right direction in fig. 7) may be perpendicular to the side-moving direction (e.g., the front-rear direction in fig. 7) of the movable diagonal slider 05. The side-shifting direction of the movable diagonal slider 05 may be perpendicular to the axis of the screw mating hole 24. The first limiting block 312 may be disposed in the first limiting hole 311 and movably connected to the first limiting hole 311, where the movable connection manner may be threaded connection or sliding connection. The upper and lower sides of one end of the first limiting block 312 can be abutted to the side wall in the first limiting groove 42 to limit the first rod portion 41 to move along the axial direction, so that the adjusting screw assembly 04 can move smoothly, and the adjusting screw assembly 04 is ensured to drive the movable inclined sliding block 05 to move smoothly.
In some embodiments, as shown in fig. 5, the first limiting portion 31 includes two first limiting holes 311 and two first limiting blocks 312; the two first limiting holes 311 are symmetrically arranged at two sides of the screw matching hole 24 respectively; the two first limiting blocks 312 are respectively and movably connected with the two first limiting holes 311; one end of each of the two first limiting blocks 312 is respectively abutted into the first limiting groove 42 to limit the first rod 41 to move along the axial direction.
In this embodiment, as shown in fig. 5, the first limiting portion 31 may include two first limiting holes 311 and two first limiting blocks 312. The two first limiting holes 311 may penetrate into the screw fitting hole 24 from symmetrical both sides of the base portion 21, respectively. The two first limiting blocks 312 may be respectively disposed in the two first limiting holes 311 and movably connected with the two first limiting holes 311, where the movable connection manner may be threaded connection or sliding connection. The upper side and the lower side of one end of the two first limiting blocks 312 can be abutted to the side wall in the first limiting groove 42, so that the first rod portion 41 can be more stably limited to move along the axial direction of the first rod portion, the side movement of the adjusting screw assembly 04 can be smoother, and the smoothness of the moving of the movable inclined slide block 05 driven by the adjusting screw assembly 04 is ensured.
In some embodiments, as shown in fig. 3, the second limiting portion 32 includes a second limiting hole 321 and a second limiting block 322; the second limiting hole 321 penetrates into the screw fitting hole 24 from the base portion 21 side; the axis of the second limiting hole 321 is parallel to the side moving direction of the movable inclined slide block 05; the second limiting block 322 is movably connected with the second limiting hole 321; one end of the second limiting block 322 is abutted into the second limiting groove 44; the elastic member in the second stopper 322 provides an elastic force to push one end of the second stopper 322 to provide a lateral pushing force to the first lever portion 41 toward the fixed inclined portion 62.
In this embodiment, as shown in fig. 3, the second limiting portion 32 may include a second limiting hole 321 and a second limiting block 322. The second limiting hole 321 may penetrate into the screw fitting hole 24 from one side of the base portion 21. The axis of the second limiting hole 321 (left-right direction in fig. 6) may be parallel to the side-moving direction (left-right direction in fig. 6) of the movable diagonal slider 05. The second limiting block 322 may be disposed in the first limiting hole 311 and movably connected to the second limiting hole 321, where the movable connection may be a threaded connection or a sliding connection. The end of one end of the second limiting block 322 may be abutted to the inner wall of the second limiting groove 44. An elastic component can be arranged in the second limiting block 322, the elastic component can provide elastic force to push one end of the second limiting block 322, the structure is simple and easy to realize, the second limiting block 322 can provide lateral thrust close to the fixed inclined part 62 for the first rod part 41, lateral pretightening force can be provided for the movable inclined sliding block 05, the movable inclined sliding block 05 and the fixed inclined sliding block 06 can be always attached, and the fluency of the side movement of the movable inclined sliding block 05 driven by the adjusting screw assembly 04 is ensured.
In other embodiments, as shown in fig. 13, the second limiting portion 32 may include a plurality of second limiting holes 321 and a plurality of second limiting blocks 322. The second limiting holes 321 may be uniformly distributed at one side of the screw engaging hole 24 in the circumferential direction. Each second limiting block 322 may be movably connected with each second limiting hole 321. An end portion of one end of each second limiting block 322 may abut against an inner wall of the second limiting groove 44. A corresponding elastic component may be disposed in each second limiting block 322, where the elastic component may provide an elastic force to push one end of each second limiting block 322. The second limiting blocks 322 can provide acting forces in multiple directions for the first rod portion 41, so that more stable lateral thrust approaching the fixed inclined portion 62 is provided for the first rod portion 41, and further more stable lateral pretightening force can be provided for the movable inclined sliding block 05, so that the movable inclined sliding block 05 and the fixed inclined sliding block 06 can be always attached, and further smoothness of lateral movement of the movable inclined sliding block 05 driven by the adjusting screw assembly 04 is ensured.
In some embodiments, as shown in fig. 7, 8, and 9, the fixed diagonal slider 06 further includes a flat chute 64; the flat chute 64 is provided on the side of the fixed slider body 61 close to the base portion 21; the extending direction of the flat sliding groove 64 is parallel to the side moving direction of the movable inclined sliding block 05; the movable diagonal slider 05 further includes a smoothing portion 53; the smooth part 53 is fixedly connected with one end of the movable slider body 51; the smooth portion 53 is movably connected to the smooth groove 64, and slides axially along the extending direction of the smooth groove 64 and the second lever portion 43.
In this embodiment, as shown in fig. 7, the fixed diagonal slider 06 may also include a flat chute 64. The flat sliding groove 64 may be provided on a side of the fixed diagonal slider 06 near the base portion 21, and an extending direction of the flat sliding groove 64 may be parallel to a side moving direction of the movable diagonal slider 05. As shown in fig. 8 and 9, the movable ramp block 05 may further include a smooth portion 53. The smoothing portion 53 may be plate-shaped, and one side of the smoothing portion 53 may be fixedly connected to one end of the movable slider body 51. The smooth portion 53 may be movably connected with the smooth groove 64, and the smooth portion 53 may guide the movable diagonal slider 05 to slide along the extending direction of the smooth groove 64, and may also guide the movable diagonal slider to slide along the axial direction of the second rod portion 43. The sliding direction of the smooth portion 53 is limited by the flat sliding groove 64, and the moving direction of the adjusting screw assembly 04 is limited by the first limiting portion 31 and the second limiting portion 32, so that the movable inclined sliding block 05 can move laterally in a stable and always tightly attached manner with the fixed inclined sliding block 06, and the opposite two side surfaces of the movable inclined sliding block 05 and the fixed inclined sliding block 06 can be clamped with the rudder shaft interface groove 81 better.
In other embodiments, as shown in FIG. 6, fixed diagonal slider 06 may also include a third limiting aperture 63. The third limiting hole 63 may penetrate from one end to the other end of the fixed slider body 61 (penetrating from the upper to the lower direction as shown in fig. 6), and may communicate with the screw engagement hole 24, so that one end of the adjusting screw assembly 04 may be connected with the movable diagonal slider 05 through the third limiting hole 63. Part of the second rod portion 43 can be in clearance fit with the third limiting hole 63, so that a certain avoiding space can be provided, and the side movement of the adjusting screw assembly 04 is smoother.
In some embodiments, as shown in fig. 8 and 9, the movable ramp block 05 further includes a drive hole 55; the drive hole 55 penetrates from one side of the smooth portion 53 to the other side of the smooth portion 53; the drive hole 55 is concentric with the drive screw 54; at least a portion of the second stem 43 is in clearance fit with the drive aperture 55.
In this embodiment, as shown in fig. 8 and 9, the movable ramp block 05 may further include a driving hole 55. The driving hole 55 may penetrate from one side of the smooth portion 53 to the other side of the smooth portion 53. The drive hole 55 can be concentric with the drive screw thread portion 54, at least part of the second rod portion 43 can be in clearance fit with the drive hole 55, one end of the second rod portion 43 can be in threaded connection with the drive screw thread portion 54, stress points between the adjusting screw assembly 04 and the movable inclined sliding block 05 are increased, the force of the adjusting screw assembly 04 acting on the movable inclined sliding block 05 can be more uniform and stable, a certain side moving space can be provided for the adjusting screw assembly 04, accordingly the adjusting screw assembly 04 can drive the movable inclined sliding block 05 to move side smoothly, and further the efficiency of detecting the position accuracy of the rudder shaft interface groove 81 is improved.
In some embodiments, as shown in fig. 5, 6, 7, 11, the first stem 41 comprises a first thick stem 411; the first thick rod 411 and the first thin rod 412 are fixedly connected; the first thick rod 411 is disposed at an end of the first thin rod 412 remote from the second rod portion 43; the first thick rod 411 has a diameter greater than the diameter of the first thin rod 412; the first limiting groove 42 is provided on the outer peripheral side of the first thick lever 411; the second limit groove 44 is provided on the outer peripheral side adjacent to one end of the first thin rod 412 near the second rod portion 43; the screw fitting hole 24 includes a first fitting hole 241, a second fitting hole 242; at least a portion of the first pin 412 is disposed within the first mating hole 241; at least a portion of the first thick rod 411 is disposed within the second mating hole 242.
In the present embodiment, as shown in fig. 5 and 11, the first lever portion 41 may include a first thick lever 411. The first thick rod 411 may be fixedly coupled with the first thin rod 412. The first thick rod 411 may be disposed at an end of the first thin rod 412 remote from the second rod portion 43. The diameter of the first thick rod 411 may be greater than the diameter of the first thin rod 412. In order to stably limit the movement of the adjusting screw assembly 04 along the axial direction thereof, the contact area between the upper and lower sides of one end of the first limiting block 312 and the side wall of the first limiting groove 42 needs to be increased, which results in that the cutting depth of the first limiting groove 42 tends to be larger. In order to improve the strength of the adjusting screw assembly 04, the first limiting groove 42 may be disposed on the outer circumferential side of the large-diameter first thick rod 411, so that the adjusting screw assembly 04 may be prevented from being deformed, and the reliability of the steering engine 08 rudder shaft position detecting device may be ensured. The second stopper groove 44 may be provided at an outer peripheral side adjacent to an end of the first thin rod 412 near the second rod portion 43. As shown in fig. 6 and 7, in order to ensure that the adjusting screw assembly 04 can smoothly laterally move due to the different diameters of the first thin rod 412 and the first thick rod 411, the screw engaging holes 24 may be provided with corresponding first engaging holes 241 and second engaging holes 242 to engage with the adjusting screw assembly 04. At least a portion of the first thin rod 412 may be disposed in the first fitting hole 241 and at least a portion of the first thick rod 411 may be disposed in the second fitting hole 242.
In some embodiments, as shown in fig. 6 and 12, the cross section of the second mating hole 242 is elongated; the width of the long strip is in clearance fit with the outer diameter of the first thick rod 411; the length direction of the long strip is parallel to the side moving direction of the movable inclined slide block 05.
In this embodiment, as shown in fig. 6 and 12, the cross section of the second fitting hole 242 may be elongated. The width of rectangular shape can with the external diameter clearance fit of first thick pole 411, the length direction of rectangular shape can be parallel with the side direction of moving of activity oblique slider 05 to can provide bigger side space for adjusting screw subassembly 04, make adjusting screw subassembly 04 drive activity oblique slider 05 move side more smoothly, the opposite direction both sides face of activity oblique slider 05, fixed oblique slider 06 can be fast with rudder shaft interface groove 81 block, improve the efficiency of detecting rudder shaft position accuracy.
In some embodiments, as shown in fig. 2, the base assembly 02 further includes a weight-reducing channel 23; the weight-reducing grooves 23 are provided on both sides of the base portion 21 away from the screw fitting hole 24.
In this embodiment, as shown in fig. 2, the base assembly 02 may further include a plurality of weight-reducing slots 23. The weight reducing grooves 23 can be symmetrically arranged on two sides of the base part 21 far away from the screw matching holes 24, so that the weight reduction of the steering engine 08 rudder shaft position detection device can be realized, and the manufacturing cost is reduced.
In some embodiments, as shown in fig. 1, the steering engine 08 rudder shaft position detection device further comprises a platform assembly 01; the platform assembly 01 is detachably connected with the detected steering engine 08; the movable inclined slide block 05 and the fixed inclined slide block 06 are abutted against the side wall of the rudder shaft interface groove 81 of the steering engine 08 to be detected; the base portion 21 is detachably connected to a rudder shaft of the steering engine 08 to be detected.
In this embodiment, as shown in fig. 1, the rudder shaft position detecting device may further include a platform assembly 01. The platform assembly 01 can be detachably connected with the steering engine 08 to be detected, so that the steering engine 08 with different changes can be detected by the steering shaft position detection device. Opposite two side surfaces of the movable inclined slide block 05 and the fixed inclined slide block 06 can be abutted against the side wall of the rudder shaft interface groove 81 of the detected steering engine 08, so that the rotating angles of the movable inclined slide block 05 and the fixed inclined slide block 06 can be driven by detecting the rudder shaft interface groove 81, and the efficiency of detecting the position accuracy of the rudder shaft is improved. The base part 21 can be detachably connected with the rudder shaft of the steering engine 08 to be detected.
In other embodiments, the platform assembly 01 may include an end face positioning portion 11, a circumferential positioning portion 12. The rudder shaft of the detected steering engine 08 can be positioned, installed and fixed to the detection platform through the end face positioning part 11 and the circumferential positioning part 12, so that the opposite two side faces of the movable inclined sliding block 05 and the fixed inclined sliding block 06 of the rudder shaft position detection device can be quickly abutted with the side wall of the rudder shaft interface groove 81, and the efficiency of detecting the position accuracy of the rudder shaft is improved.
It will be understood by those of ordinary skill in the art that the foregoing embodiments are specific examples of implementing the disclosure, and that various changes in form and details may be made therein without departing from the spirit and scope of the disclosure.

Claims (10)

1. Steering wheel rudder shaft position detection device, its characterized in that, steering wheel rudder shaft position detection device includes:
the base assembly comprises a base part and a screw rod matching hole; the screw fitting hole penetrates from one side of the base portion to the other side of the base portion;
the fixed inclined sliding block comprises a fixed sliding block body and a fixed inclined part; one end of the fixed slider body is fixedly connected with one side surface of the base part; the screw engagement hole penetrates from one side of the fixed slider body to the other side of the fixed slider body; the other end of the fixed slider body extends in a direction away from the base portion; a tilted fixed oblique part is arranged on one side surface of the fixed slider body;
the adjusting screw assembly comprises a first rod part, a second rod part, a first limit groove and a second limit groove; the first rod part and the second rod part are sequentially connected; the first limiting groove is arranged on the outer periphery side adjacent to one end, far away from the second rod part, of the first rod part; the second limiting groove is arranged on the outer peripheral side adjacent to one end, close to the second rod, of the first rod; at least part of the first rod part is in clearance fit with the screw rod matching hole;
the movable inclined slide block comprises a movable slide block body, a movable inclined part and a driving threaded part; a movable inclined part is arranged on one side surface of the movable sliding block body; the inclination angle of the movable inclined part is the same as that of the fixed inclined part; the movable inclined part and the fixed inclined part are mutually matched and abutted; the drive screw penetrates from one end of the movable slider body to the other end of the movable slider body; at least part of the second rod part is in threaded connection with the driving threaded part; the side moving direction of the movable inclined sliding block is perpendicular to the axis of the screw rod matching hole;
the screw limiting assembly comprises a first limiting part and a second limiting part; the first limiting part is movably connected with the base part; the second limiting part is movably connected with the base part; one end of the first limiting part is movably connected with the first limiting groove or the second limiting groove to limit the first rod part to move along the axial direction of the first rod part; the end part of the second limiting part is movably connected with the first limiting groove or the second limiting groove which is not movably connected with the first limiting part, and provides a lateral thrust to the first rod part, wherein the lateral thrust is close to the fixed inclined part;
the base assembly further comprises a planar positioning portion; the plane positioning part is arranged on one side surface of the base part; the steering engine rudder shaft position detection device further comprises an angle measuring instrument; the goniometer is abutted with the plane positioning part; the goniometer is detachably connected with the base portion.
2. The steering engine rudder shaft position detection device according to claim 1, wherein,
the first limiting part comprises a first limiting hole and a first limiting block; the first limiting hole penetrates into the screw rod matching hole from one side of the base part; the axis of the first limiting hole is perpendicular to the lateral movement direction of the movable inclined sliding block; the first limiting block is movably connected with the first limiting hole; one end of the first limiting block is abutted to the first limiting groove to limit the first rod part to move axially.
3. The steering engine rudder shaft position detection device according to claim 2, wherein,
the first limiting part comprises two first limiting holes and two first limiting blocks; the two first limiting holes are symmetrically arranged on two sides of the screw matching hole respectively; the two first limiting blocks are respectively and movably connected with the two first limiting holes; one ends of the two first limiting blocks are respectively abutted to the first limiting grooves to limit the first rod part to move along the axial direction of the first rod part.
4. The steering engine rudder shaft position detection device according to claim 2, wherein,
the second limiting part comprises a second limiting hole and a second limiting block; the second limiting hole penetrates into the screw rod matching hole from one side of the base part; the axis of the second limiting hole is parallel to the side moving direction of the movable inclined sliding block; the second limiting block is movably connected with the second limiting hole; one end of the second limiting block is abutted to the second limiting groove; the elastic component in the second limiting block provides elastic force to push one end of the second limiting block to provide lateral thrust to the first rod portion, and the lateral thrust is close to the fixed inclined portion.
5. The steering engine rudder shaft position detection device according to claim 2, wherein,
the fixed inclined sliding block further comprises a flat sliding groove; the smooth groove is arranged on one side of the fixed slider body close to the base part; the extending direction of the smooth groove is parallel to the lateral movement direction of the movable inclined sliding block; the movable inclined slide block further comprises a smooth part; the smooth part is fixedly connected with one end of the movable sliding block body; the smooth part is movably connected with the smooth groove and axially slides along the extending direction of the smooth groove and the second rod part.
6. The steering wheel rudder shaft position detecting device according to claim 5, wherein,
the movable inclined slide block also comprises a driving hole; the driving hole penetrates from one side of the smooth part to the other side of the smooth part; the drive bore is concentric with the drive screw; at least a portion of the second stem portion is in clearance fit with the drive bore.
7. The steering engine rudder shaft position detection device according to claim 1, wherein,
the first rod part comprises a first thick rod and a first thin rod; the first thick rod is fixedly connected with the first thin rod; the first thick rod is arranged at one end of the first thin rod, which is far away from the second rod part; the first thick rod diameter is greater than the first thin rod diameter; the first limit groove is arranged on the outer peripheral side of the first thick rod; the second limiting groove is arranged on the outer peripheral side adjacent to one end of the first thin rod, which is close to the second rod part; the screw rod matching holes comprise first matching holes and second matching holes; at least part of the first slender rod is arranged in the first matching hole; at least part of the first thick rod is arranged in the second matching hole.
8. The steering wheel rudder shaft position detecting device according to claim 7, wherein,
the cross section of the second matching hole is long-strip-shaped; the width of the strip is in clearance fit with the outer diameter of the first thick rod; the length direction of the strip is parallel to the side moving direction of the movable inclined sliding block.
9. The steering wheel rudder shaft position detecting device according to claim 8, wherein,
the base assembly further includes a weight reduction channel; the weight reduction grooves are formed in two sides, away from the screw matching holes, of the base portion.
10. The steering engine rudder shaft position detection device according to claim 1, wherein,
the steering engine rudder shaft position detection device further comprises a platform assembly; the platform assembly is detachably connected with the steering engine to be detected; the movable inclined sliding block and the fixed inclined sliding block are in butt joint with the side wall of the rudder shaft interface groove of the steering engine to be detected; the base part is detachably connected with a rudder shaft of the steering engine to be detected.
CN202311316152.8A 2023-10-12 2023-10-12 Steering engine rudder shaft position detection device Active CN117048847B (en)

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Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002046691A (en) * 2000-08-08 2002-02-12 Japan Hamuwaaji Kk Steering engine installation method and rotary vane type steering engine
CA3063392A1 (en) * 2014-10-31 2016-04-30 The Boeing Company Method for changing stiffness of a stiffness path in an aircraft structure
CN206113834U (en) * 2016-08-19 2017-04-19 湖北三江航天红峰控制有限公司 Steering wheel corner measuring device
CN106610255A (en) * 2015-10-27 2017-05-03 哈尔滨建成集团有限公司 Adjustment detection device for initial position of small-stress-plane output shaft of steering engine
CN107884216A (en) * 2017-10-17 2018-04-06 兰州飞行控制有限责任公司 A kind of bullet steering wheel simulation test equipment
CN207311867U (en) * 2017-09-04 2018-05-04 江西洪都航空工业集团有限责任公司 A kind of steering engine tests mounting structure
EP3404395A1 (en) * 2017-05-19 2018-11-21 Goodrich Actuation Systems SAS Test apparatus for flight actuator check device
CN110077577A (en) * 2019-03-20 2019-08-02 北京瑞极通达科技有限公司 A kind of electric operator based on high speed rotation aircraft
CN111232240A (en) * 2020-01-17 2020-06-05 湖北三江航天红峰控制有限公司 Mechanical deflection angle testing device of steering engine
CN111252265A (en) * 2018-12-03 2020-06-09 江西洪都航空工业集团有限责任公司 Control surface clearance test equipment
CN112537439A (en) * 2020-12-17 2021-03-23 贵州航天控制技术有限公司 Connecting structure for connecting shaft and hole, control surface and steering engine
CN212891008U (en) * 2020-09-16 2021-04-06 绵阳市平政电子科技有限公司 Steering wheel test mounting structure
CN215984962U (en) * 2021-09-06 2022-03-08 成都志力科技发展有限责任公司 Steering wheel detects frock
CN218850480U (en) * 2022-10-31 2023-04-11 贵州航天控制技术有限公司 Brushless motor and steering engine mechanism with same
CN219284632U (en) * 2022-11-30 2023-06-30 中国航天空气动力技术研究院 Steering engine module for wind tunnel test model

Patent Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002046691A (en) * 2000-08-08 2002-02-12 Japan Hamuwaaji Kk Steering engine installation method and rotary vane type steering engine
CA3063392A1 (en) * 2014-10-31 2016-04-30 The Boeing Company Method for changing stiffness of a stiffness path in an aircraft structure
CN106610255A (en) * 2015-10-27 2017-05-03 哈尔滨建成集团有限公司 Adjustment detection device for initial position of small-stress-plane output shaft of steering engine
CN206113834U (en) * 2016-08-19 2017-04-19 湖北三江航天红峰控制有限公司 Steering wheel corner measuring device
EP3404395A1 (en) * 2017-05-19 2018-11-21 Goodrich Actuation Systems SAS Test apparatus for flight actuator check device
CN207311867U (en) * 2017-09-04 2018-05-04 江西洪都航空工业集团有限责任公司 A kind of steering engine tests mounting structure
CN107884216A (en) * 2017-10-17 2018-04-06 兰州飞行控制有限责任公司 A kind of bullet steering wheel simulation test equipment
CN111252265A (en) * 2018-12-03 2020-06-09 江西洪都航空工业集团有限责任公司 Control surface clearance test equipment
CN110077577A (en) * 2019-03-20 2019-08-02 北京瑞极通达科技有限公司 A kind of electric operator based on high speed rotation aircraft
CN111232240A (en) * 2020-01-17 2020-06-05 湖北三江航天红峰控制有限公司 Mechanical deflection angle testing device of steering engine
CN212891008U (en) * 2020-09-16 2021-04-06 绵阳市平政电子科技有限公司 Steering wheel test mounting structure
CN112537439A (en) * 2020-12-17 2021-03-23 贵州航天控制技术有限公司 Connecting structure for connecting shaft and hole, control surface and steering engine
CN215984962U (en) * 2021-09-06 2022-03-08 成都志力科技发展有限责任公司 Steering wheel detects frock
CN218850480U (en) * 2022-10-31 2023-04-11 贵州航天控制技术有限公司 Brushless motor and steering engine mechanism with same
CN219284632U (en) * 2022-11-30 2023-06-30 中国航天空气动力技术研究院 Steering engine module for wind tunnel test model

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
弹性负载力矩下舵偏转角度的测量方法;郭倩;;航天制造技术(第06期);第64-67页 *

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