A gas-air compound steering gear

By designing the transmission components in the gas-air composite servo, the problem of insufficient stability of the power transmission structure is solved, and higher performance and reliability are achieved.

CN116985990BActive Publication Date: 2025-04-11BEIJING HANGKE JINGGONG TECH CO LTD
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Patent Information

Application Number
CN202310883541.2
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2023-07-18
Publication Date
2025-04-11
Estimated Expiration
2043-07-18

AI Technical Summary

Technical Problem

The power transmission structure of the existing gas-air composite servo is insufficient to support high-strength use, resulting in a degradation of performance.

Method used

A transmission assembly including a first transmission member, a second transmission member and a third transmission member is designed to increase structural strength by sequential transmission arrangements and ensure the reliability of the transmission effect through the limiting member.

Benefits of technology

It improves the transmission reliability of the rudder shaft rotation effect, so that the rudder plate can rotate more reliably according to demand, thereby improving the performance of gas-air composite servo.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present invention discloses a gas-air compound steering gear, comprising a housing, a mounting seat, a rudder wing, a rudder shaft, a transmission assembly and a rudder plate; the mounting seat is arranged in the housing; the rudder wing is arranged on the mounting seat; the rudder shaft is connected to one end of the rudder wing away from the mounting seat; one end of the transmission assembly is connected to the rudder shaft; the rudder plate is connected to the other end of the transmission assembly, and the rudder plate is rotatably arranged in the housing; wherein the transmission assembly comprises a first transmission member, a second transmission member and a third transmission member, one end of the first transmission member is connected to the rudder shaft, the second transmission member is transmission-connected between the first transmission member and the third transmission member, and one end of the third transmission member is connected to the rudder plate. In this way, since the transmission assembly has the first transmission member, the second transmission member and the third transmission member which are sequentially arranged for transmission, the rotation effect of the rudder shaft can be more reliably transmitted to the rudder plate for rotation, so that the gas-air compound steering gear can be rotated as required during use to constitute the use performance of the gas-air compound steering gear.
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Description

Technical Field

[0001] The present invention relates to the technical field of gas-air compound steering gear, and in particular to a gas-air compound steering gear. Background Art

[0002] In the prior art, the steering gear is installed at the rear end of the engine nozzle on the flight, and is an important component for the stable flight and rapid maneuvering of the aircraft by utilizing flight dynamics. Therefore, the power transmission of the steering gear during use is crucial to the control of the steering gear. In the related art, the stability of the power transmission structure in the steering gear is insufficient, and it cannot support the high-intensity use of the steering gear, thereby reducing the performance of the steering gear. Summary of the invention

[0003] The present invention aims to solve at least one of the technical problems existing in the prior art. To this end, one object of the present invention is to provide a gas-air compound steering gear, wherein the transmission assembly provided in the gas-air compound steering gear is relatively stable so that the gas-air compound steering gear has higher performance.

[0004] According to an embodiment of the present invention, the gas-air compound steering gear comprises: a housing, a mounting seat, a rudder wing, a rudder shaft, a transmission assembly and a rudder plate; the mounting seat is arranged in the housing; the rudder wing is arranged on the mounting seat; the rudder shaft is connected to an end of the rudder wing away from the mounting seat; one end of the transmission assembly is connected to the rudder shaft; the rudder plate is connected to the other end of the transmission assembly, and the rudder plate is rotatably arranged on the housing; wherein the transmission assembly comprises a first transmission member, a second transmission member and a third transmission member, one end of the first transmission member is connected to the rudder shaft, the second transmission member is transmission-connected between the first transmission member and the third transmission member, and one end of the third transmission member is connected to the rudder plate.

[0005] According to the gas-air compound steering gear of the embodiment of the present invention, a transmission assembly as shown above is arranged in the gas-air compound steering gear, and the transmission assembly has a first transmission member, a second transmission member and a third transmission member which are arranged in sequence for transmission. The transmission assembly has high structural strength and usability performance, and can make the rotation effect of the rudder shaft be more reliably transmitted to the rudder plate for rotation, so that the gas-air compound steering gear can be rotated as required during use to constitute the usability performance of the gas-air compound steering gear, so that the usability performance of the gas-air compound steering gear is improved.

[0006] In some embodiments, a first limiting portion is provided at the end of the rudder shaft, and a second limiting portion is provided at one end of the first transmission member, and the first limiting portion and the second limiting portion are limitedly matched.

[0007] In some embodiments, one of the first limiting portion and the second limiting portion is a limiting protrusion, and the other of the first limiting portion and the second limiting portion is a limiting groove, and the limiting protrusion is limitedly disposed in the limiting groove.

[0008] In some embodiments, a third limiting portion is provided at the other end of the first transmission member, a fourth limiting portion is provided at one end of the second transmission member, a fifth limiting portion is provided at the other end of the second transmission member, and a sixth limiting portion is provided on the third transmission member. The third limiting portion and the fourth limiting portion are arranged via a first limiting member, and the fifth limiting portion and the sixth limiting portion are arranged via a second limiting member.

[0009] In some embodiments, both the first limiting member and the second limiting member are cylindrical limiting members.

[0010] In some embodiments, a seventh limiting portion is provided at one end of the third transmission member, an eighth limiting portion is provided on the rudder plate, and the seventh limiting portion and the eighth limiting portion cooperate with each other in limiting manner.

[0011] In some embodiments, a fourth transmission member is provided at one end of the third transmission member, the fourth transmission member is slidably arranged with the other end of the third transmission member, and the other end of the fourth transmission member is transmission-connected to the sliding member.

[0012] In some embodiments, it also includes: a slide rail, a slide groove is provided on the sliding member, and the slide groove is slidably arranged on the slide rail.

[0013] In some embodiments, the transmission assembly also includes: a connecting shaft, the connecting shaft is connected to the third transmission member, and the extension direction of the connecting shaft is perpendicular to the extension direction of the third transmission member, connecting grooves are provided at both ends of the connecting shaft, and a connecting part is provided on the rudder plate, and the connecting part is connected to the connecting groove.

[0014] In some embodiments, a first transmission groove is provided on the rudder shaft, a second transmission groove is provided on the first transmission member, and the first transmission groove and the second transmission groove are fixedly connected by a screw member.

[0015] Additional aspects and advantages of the present invention will be given in part in the following description and in part will be obvious from the following description, or will be learned through practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] The above and / or additional aspects and advantages of the present invention will become apparent and easily understood from the description of the embodiments in conjunction with the following drawings, in which:

[0017] Figure 1 is a schematic structural diagram of a gas-air compound steering gear according to an embodiment of the present invention;

[0018] Figure 2 is a schematic structural diagram of a gas-air compound steering gear according to an embodiment of the present invention;

[0019] Figure 3 is a schematic structural diagram of a gas-air compound steering gear according to an embodiment of the present invention;

[0020] Figure 4 is a schematic structural diagram of a transmission assembly according to an embodiment of the present invention;

[0021] Figure 5 is an exploded schematic diagram of a transmission assembly according to an embodiment of the present invention;

[0022] Reference numerals:

[0023] Gas-air compound steering gear 10,

[0024] Housing 100,

[0025] Mounting seat 200,

[0026] Rudder Wing 300,

[0027] The rudder shaft 400, the first limiting portion 401, the first transmission groove 402,

[0028] Transmission assembly 500, first transmission member 510, second limiting portion 511, third limiting portion 512, second transmission groove 513,

[0029] The second transmission member 520, the fourth limiting portion 521, the fifth limiting portion 522, the third transmission member 530, the sixth limiting portion 531, the seventh limiting portion 532, the fourth transmission member 540, the sliding member 550, the connecting shaft 560, the connecting groove 561,

[0030] Slide 700,

[0031] Threaded parts 800. DETAILED DESCRIPTION

[0032] Embodiments of the present invention are described in detail below. The embodiments described with reference to the accompanying drawings are exemplary. Embodiments of the present invention are described in detail below.

[0033] Reference below Figure 1-Figure 5 The gas-air compound steering gear 10 according to the embodiment of the present invention includes: a housing 100, a mounting seat 200, a rudder wing 300, a rudder shaft 400, a transmission assembly 500 and a rudder plate.

[0034] Specifically, the mounting seat 200 is arranged in the shell 100; the rudder wing 300 is arranged on the mounting seat 200; the rudder shaft 400 is connected to the end of the rudder wing 300 away from the mounting seat 200; one end of the transmission assembly 500 is connected to the rudder shaft 400; the rudder plate is connected to the other end of the transmission assembly 500, and the rudder plate is rotatably arranged in the shell 100; wherein the transmission assembly 500 includes a first transmission member 510, a second transmission member 520 and a third transmission member 530, one end of the first transmission member 510 is connected to the rudder shaft 400, the second transmission member 520 is transmission-connected between the first transmission member 510 and the third transmission member 530, and one end of the third transmission member 530 is connected to the rudder plate.

[0035] It should be noted that a receiving space for receiving other components is formed in the housing 100, so that other structures are suitable for being constructed in the receiving space, so that the housing 100 is suitable for protecting other structures to improve the performance of the gas-air compound steering gear 10. A mounting seat 200 is provided in the housing 100, and the rudder wing 300 is suitable for being arranged on the mounting seat 200 in a rotating manner to transmit the rotation effect, and a rudder shaft 400 is provided at one end of the rudder wing 300, so that the rudder wing 300 is suitable for driving the rudder shaft 400 to rotate. At the same time, the transmission assembly 500 is connected to the rudder shaft 400, so that the rudder shaft 400 is suitable for driving the transmission assembly 500 to transmit and drive the rudder plate to rotate to form or adjust the performance of the gas-air compound steering gear 10.

[0036] During the use of the transmission assembly 500, the first transmission member 510 is suitable for being connected to the rudder shaft 400 so that the rotation effect of the rudder shaft 400 is suitable for being transmitted to the first transmission member 510, and the second transmission member 520 is transmission-connected to the first transmission member 510, and the third transmission member 530 is transmission-connected to the second transmission member 520 so that the rotation effect is suitable for being transmitted to the rudder plate through the third transmission member 530 to drive the rudder plate to rotate, thereby driving the rotation of the rudder plate to constitute the adjustment of the use performance of the gas-air compound servo 10.

[0037] According to the gas-air compound servo 10 of the embodiment of the present invention, a transmission assembly 500 as shown above is provided in the gas-air compound servo 10, and the transmission assembly 500 has a first transmission member 510, a second transmission member 520 and a third transmission member 530 which are sequentially arranged for transmission. The transmission assembly 500 has high structural strength and performance, and can make the rotation effect of the rudder shaft 400 be more reliably transmitted to the rudder plate for rotation, so that the gas-air compound servo 10 can be rotated as required during use to constitute the performance of the gas-air compound servo 10, so that the performance of the gas-air compound servo 10 is improved.

[0038] In some embodiments, a first limiting portion 401 is provided at the end of the rudder shaft 400, and a second limiting portion 511 is provided at one end of the first transmission member 510, and the first limiting portion 401 is limitedly matched with the second limiting portion 511. In this way, by providing the first limiting portion 401 at the end of the rudder shaft 400, the first limiting portion 401 is suitable for being limitedly matched with the second limiting portion 511 on the first transmission member 510, so that the rotation effect on the rudder shaft 400 can be more reliably transmitted to the transmission assembly 500 to realize the rotation drive of the rudder plate, thereby making the control and use of the gas-air compound steering gear 10 more reliable.

[0039] In some specific embodiments, one of the first limiting portion 401 and the second limiting portion 511 is a limiting protrusion, and the other of the first limiting portion 401 and the second limiting portion 511 is a limiting groove, and the limiting protrusion is limitedly arranged in the limiting groove. It can be understood that by setting the first limiting portion 401 and the second limiting portion 511 as the limiting protrusion and the limiting groove respectively, the limiting connection between the first limiting portion 401 and the second limiting portion 511 is made more reliable, so that the transmission effect between the rudder shaft 400 and the first transmission member 510 is more stable, so that the rudder shaft 400 is suitable for rotation under the control of the transmission assembly 500 to improve the performance of the gas-air compound steering gear 10.

[0040] In some embodiments, a third limiting portion 512 is provided at the other end of the first transmission member 510, a fourth limiting portion 521 is provided at one end of the second transmission member 520, a fifth limiting portion 522 is provided at the other end of the second transmission member 520, and a sixth limiting portion 531 is provided on the third transmission member 530. The third limiting portion 512 and the fourth limiting portion 521 are arranged through the transmission of the first limiting member, and the fifth limiting portion 522 and the sixth limiting portion 531 are arranged through the transmission of the second limiting member. In this way, since the first limiting member is used for transmission connection between the third limiting portion 512 and the fourth limiting portion 521, the transmission effect between the first transmission member 510 and the second transmission member 520 is more reliable so that the force transmitted to the first transmission member 510 can be transmitted to the second transmission member 520; and the fifth limiting portion 522 and the sixth limiting portion 531 are transmission-connected by using the second limiting member, so that the force acting on the second transmission member 520 can be transmitted to the third transmission member 530 through the second limiting member for power transmission, so as to achieve the power transmission effect of the transmission assembly 500.

[0041] In some specific embodiments, the first stopper and the second stopper are both cylindrical stoppers. Thus, by setting the first stopper and the second stopper as cylindrical bodies, the power transmission effect between the first transmission member 510 and the second transmission member 520 and the second transmission member 520 and the third transmission member 530 is more reliable, and the transmission effect of the transmission assembly 500 is more reliable, thereby improving the performance of the gas-air compound steering gear 10.

[0042] In some embodiments, a seventh limit portion 532 is provided at one end of the third transmission member 530, and an eighth limit portion is provided on the rudder plate, and the seventh limit portion 532 and the eighth limit portion are limitedly matched. Therefore, by providing the seventh limit portion 532 on the third transmission member 530, the seventh limit portion 532 and the eighth limit portion on the rudder plate are limitedly matched, so that the force on the third transmission member 530 can be transmitted to the rudder plate to drive the rudder plate to rotate.

[0043] In some embodiments, a fourth transmission member 540 is provided at one end of the third transmission member 530, the fourth transmission member 540 is rotatably connected to the other end of the third transmission member 530, and the other end of the fourth transmission member 540 is slidably arranged with the sliding member 550. It should be noted that, since the third transmission member 530 is on the side away from the rudder plate, so that the third transmission member 530 is suitable for connecting with the fourth transmission member 540 to drive the fourth transmission member 540 to move, and the fourth transmission member 540 is also suitable for slidably connecting with the sliding member 550, the sliding member 550 is suitable for limiting the moving direction of the fourth transmission member 540, so that the third transmission member 530 can transmit the force to the rudder plate for rotation according to the design.

[0044] In some embodiments, the gas-air hybrid steering gear 10 further includes: a slide rail 700, a slide groove is provided on the slide member 550, and the slide groove is slidably arranged on the slide rail 700. In this way, by sliding the slide rail 700 and the slide groove on the slide member 550, the slide member 550 can move under the guidance of the slide rail 700, so that the force is suitable for being transmitted to the steering plate through the third transmission member 530 to drive the steering plate to move.

[0045] In some embodiments, the transmission assembly 500 further includes: a connecting shaft 560, the connecting shaft 560 is connected to the third transmission member 530, and the extending direction of the connecting shaft 560 is perpendicular to the extending direction of the third transmission member 530, and connecting grooves 561 are provided at both ends of the connecting shaft 560, and a connecting portion is provided on the rudder plate, and the connecting portion is connected to the connecting groove 561. Therefore, by providing the connecting shaft 560 in the connecting direction between the third transmission member 530 and the rudder plate, the connecting groove 561 is provided on the connecting shaft 560, and the connecting groove 561 is connected to the connecting portion on the rudder plate, so that the force on the third transmission member 530 can better act on the rudder plate to drive the rudder plate to rotate as required.

[0046] In some embodiments, the rudder shaft 400 is provided with a first transmission groove 402, the first transmission member 510 is provided with a second transmission groove 513, and the first transmission groove 402 and the second transmission groove 513 are fixedly connected by a screw member 800. In this way, by fixing the first transmission groove 402 on the rudder shaft 400 and the second transmission groove 513 on the first transmission member 510 with the screw member 800, the transmission effect between the rudder shaft 400 and the first transmission member 510 is made more reliable, so that the rudder plate can be rotated according to the design requirements.

[0047] Other structures and operations of the gas-air compound steering gear 10 according to the embodiment of the present invention are well known to those skilled in the art and will not be described in detail here.

[0048] In the description of this specification, the description with reference to the terms "one embodiment", "some embodiments", "illustrative embodiments", "examples", "specific examples", or "some examples" means that the specific features, structures, materials, or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present invention. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example.

[0049] Although the embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the claims and their equivalents.

Claims

1. A gas-air compound steering gear, characterized in that: include: case; A mounting seat, the mounting seat being arranged in the housing; A rudder wing, wherein the rudder wing is arranged on the mounting seat; A rudder shaft connected to an end of the rudder wing away from the mounting seat; A transmission assembly, one end of which is connected to the rudder shaft; A rudder plate, the rudder plate is connected to the other end of the transmission assembly and the rudder plate is rotatably disposed on the housing; Wherein, the transmission assembly includes a first transmission member, a second transmission member and a third transmission member, one end of the first transmission member is connected to the rudder shaft, the second transmission member is transmission-connected between the first transmission member and the third transmission member, one end of the third transmission member is connected to the rudder plate, one end of the third transmission member is provided with a fourth transmission member, the fourth transmission member is rotationally connected to the other end of the third transmission member, and the other end of the fourth transmission member is slidably arranged with a sliding member.

2. The gas-air compound steering gear according to claim 1, characterized in that: A first limiting portion is provided at the end of the rudder shaft, and a second limiting portion is provided at one end of the first transmission member, and the first limiting portion is matched with the second limiting portion.

3. The gas-air compound steering gear according to claim 2, characterized in that: One of the first limiting portion and the second limiting portion is a limiting protrusion, and the other of the first limiting portion and the second limiting portion is a limiting groove, and the limiting protrusion is limitedly disposed in the limiting groove.

4. The gas-air compound steering gear according to claim 2, characterized in that: A third limiting part is provided at the other end of the first transmission member, a fourth limiting part is provided at one end of the second transmission member, a fifth limiting part is provided at the other end of the second transmission member, and a sixth limiting part is provided on the third transmission member. The third limiting part and the fourth limiting part are arranged through transmission by the first limiting member, and the fifth limiting part and the sixth limiting part are arranged through transmission by the second limiting member.

5. The gas-air compound steering gear according to claim 4, characterized in that: The first limiting member and the second limiting member are both cylindrical limiting members.

6. The gas-air compound steering gear according to claim 4, characterized in that: A seventh limiting portion is disposed at one end of the third transmission member, an eighth limiting portion is disposed on the rudder plate, and the seventh limiting portion and the eighth limiting portion cooperate in limiting manner.

7. The gas-air compound steering gear according to claim 1, characterized in that: Also includes: A slide rail, wherein the slide member is provided with a slide groove, and the slide groove is slidably arranged on the slide rail.

8. The gas-air compound steering gear according to claim 1, characterized in that: The transmission assembly also includes: a connecting shaft, which is connected to the third transmission member, and the extension direction of the connecting shaft is perpendicular to the extension direction of the third transmission member, connecting grooves are provided at both ends of the connecting shaft, and a connecting part is provided on the rudder plate, and the connecting part is connected to the connecting groove.

9. The gas-air compound steering gear according to claim 1, characterized in that: The rudder shaft is provided with a first transmission groove, the first transmission member is provided with a second transmission groove, and the first transmission groove and the second transmission groove are fixedly connected by a screw member.

Citation Information

Patent Citations

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