CN117125251A - Motor Siemens wedge power M9-PD-35 intelligent steering device - Google Patents
Motor Siemens wedge power M9-PD-35 intelligent steering device Download PDFInfo
- Publication number
- CN117125251A CN117125251A CN202311083302.5A CN202311083302A CN117125251A CN 117125251 A CN117125251 A CN 117125251A CN 202311083302 A CN202311083302 A CN 202311083302A CN 117125251 A CN117125251 A CN 117125251A
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- control
- push rod
- console
- aileron
- infrared receivers
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- 230000002457 bidirectional effect Effects 0.000 claims description 2
- 239000000126 substance Substances 0.000 claims description 2
- 230000001276 controlling effect Effects 0.000 description 6
- 238000009434 installation Methods 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/12—Dual control apparatus
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
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- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention relates to the technical field of intelligent steering control of airplanes, in particular to a motor Sizilce power M9-PD-35 intelligent steering device; the intelligent control system comprises an intelligent operation platform, a controller, an elevator control assembly, a right aileron control assembly, a left aileron control assembly, a gesture sensor and a course sensor, wherein the gesture sensor is used for sensing the pitching angle of an aircraft, the course sensor is used for sensing the course angle of the aircraft, the intelligent operation platform is used for outputting a control signal of the aircraft to the controller, the controller controls the lifting of an aircraft tail wing in the elevator control assembly according to the received pitching control signal, and the controller controls the lifting of a right aileron in the right aileron control assembly and the lifting of a left aileron of the left aileron control assembly according to the received course control signal, so that the course control of the aircraft is completed.
Description
Technical Field
The invention relates to the technical field of intelligent steering control of airplanes, in particular to a motor Sizilch power M9-PD-35 intelligent steering device.
Background
The high-thrust aircraft adopting the motor Siemens Chemicals power M9-PD-35 engine is still controlled by adopting a mechanical system during steering control.
The steering system of the high-thrust aircraft adopting mechanical control in the prior art has the defects of complex structure and poor operation stability.
Disclosure of Invention
The invention aims to provide a motor Sizise power M9-PD-35 intelligent steering device, which solves the problems of complex structure and poor operation stability of a steering system of a mechanically controlled high-thrust aircraft in the prior art.
In order to achieve the above purpose, the invention provides a motor Sizithro power M9-PD-35 intelligent steering device, wherein the motor Sizithro power M9-PD-35 intelligent steering device comprises an intelligent operation platform, a controller, an elevator control assembly, a right aileron control assembly, a left aileron control assembly, a gesture sensor and a heading sensor, signal output ends of the gesture sensor and the heading sensor are connected with a signal input end of the controller, the intelligent operation platform is in bidirectional connection with the controller, and input ends of the elevator control assembly, the right aileron control assembly and the left aileron control assembly are connected with an output end of the controller.
The intelligent operation platform comprises a first control unit, a second control unit and a display screen, wherein the display screen is positioned in front of a pilot, the first control unit and the second control unit are respectively positioned on two sides of the pilot, the display screen is used for displaying pitching data and heading data of an airplane, the first control unit is used for outputting pitching control signals of the airplane and controlling lifting of an airplane tail wing in an elevator control assembly through a controller, and the second control unit is used for outputting steering control signals of the airplane and controlling lifting of a right aileron in the right aileron control assembly and lifting of a left aileron of the left aileron control assembly through the controller.
The first control unit comprises a first control console, a first control push rod, a first infrared emitter, a plurality of first infrared receivers and a plurality of second infrared receivers, the first control push rod is rotationally connected to the first control console, a pitching control cavity is formed in the first control console, the inner bottom of the pitching control cavity is in an arc-shaped structure, one end of the first control push rod, which is located in the pitching control cavity, is provided with the first infrared emitter, the inner bottom of the pitching control cavity is provided with a plurality of first infrared receivers and a plurality of second infrared receivers, the first infrared receivers are uniformly distributed at the rear part of the pitching control cavity, the second infrared receivers are uniformly distributed at the front part of the pitching control cavity, and first reset springs are arranged between the two sides of the first control push rod and the surface of the first control console.
The second control unit comprises a second control console, a second control push rod, a second infrared emitter, a plurality of third infrared receivers and a plurality of fourth infrared receivers, a course control cavity is formed in the second control console, the inner bottom of the course control cavity is in an arc-shaped structure, one end of the second control push rod, which is located in the course control cavity, is provided with the second infrared emitter, the inner bottom of the course control cavity is provided with the plurality of third infrared receivers and the plurality of fourth infrared receivers, the plurality of third infrared receivers are uniformly distributed at the rear part of the course control cavity, the plurality of fourth infrared receivers are uniformly distributed at the front part of the course control cavity, and second reset springs are arranged between the two sides of the second control push rod and the surface of the second control console.
The first control push rod and the second control push rod are respectively provided with an installation block, and the first return spring and the second return spring are correspondingly installed between the installation blocks and the corresponding first control console and the second control console.
Each first reset spring and each second reset spring comprise a spring body, a first connecting block and a second connecting block, one end of the spring body is provided with the first connecting block, the other end of the spring body is provided with the second connecting block, the first connecting block is connected with the corresponding first control console and the second control console in a disassembling mode, and the second connecting block is connected with the corresponding mounting block in a disassembling mode.
The motor Sizipcia power M9-PD-35 intelligent steering device comprises an intelligent operation platform, a controller, an elevator control assembly, a right aileron control assembly, a left aileron control assembly, a gesture sensor and a heading sensor, wherein the gesture sensor is used for sensing the elevation angle of an aircraft, the heading sensor is used for sensing the heading angle of the aircraft, the intelligent operation platform is used for outputting an aircraft elevation control signal and an aircraft heading control signal to the controller according to flight requirements, the controller is used for controlling the elevation of an aircraft tail wing in the elevator control assembly according to the received elevation control signal, so that the air flow generates counter stress, the elevation of the aircraft tail wing is regulated by pressing down or lifting the aircraft tail wing, and the controller is used for controlling the elevation of the right aileron in the right aileron control assembly and the elevation of the left aileron control assembly according to the received heading control signal.
Drawings
In order to more clearly illustrate the embodiments of the invention or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the invention, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is an operation schematic diagram of the motor Siemens power M9-PD-35 intelligent steering device provided by the invention.
Fig. 2 is a front view of the intelligent operation platform provided by the invention.
Fig. 3 is a cross-sectional view of the internal structure of fig. 2 taken along line A-A provided by the present invention.
Fig. 4 is a cross-sectional view of the internal structure of the line B-B of fig. 2 provided by the present invention.
Fig. 5 is a schematic structural diagram of a first control unit provided by the present invention.
Fig. 6 is a schematic view of a part of the structure of the first control unit provided by the present invention.
Fig. 7 is an enlarged view of a part of the structure at C of fig. 6 provided by the present invention.
The intelligent control platform, 102-controller, 103-elevator control assembly, 104-right aileron control assembly, 105-left aileron control assembly, 106-attitude sensor, 107-heading sensor, 108-first control unit, 109-second control unit, 110-display screen, 111-first console, 112-first control ram, 113-first infrared transmitter, 114-first infrared receiver, 115-second infrared receiver, 116-pitch control chamber, 117-first return spring, 118-second console, 119-second control ram, 120-second infrared transmitter, 121-third infrared receiver, 122-fourth infrared receiver, 123-heading control chamber, 124-second return spring, 125-mounting block, 126-spring body, 127-first connection block, 128-second connection block, 129-telescoping protective sleeve, 130-protective sleeve body, 131-first fixed block, 132-second fixed block.
Detailed Description
Embodiments of the present invention are described in detail below, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to like or similar elements or elements having like or similar functions throughout. The embodiments described below by referring to the drawings are illustrative and intended to explain the present invention and should not be construed as limiting the invention.
Referring to fig. 1 to 7, the present invention provides a motor-zeppy power M9-PD-35 intelligent steering device, where the motor-zeppy power M9-PD-35 intelligent steering device includes an intelligent operation platform 101, a controller 102, an elevator control assembly 103, a right aileron control assembly 104, a left aileron control assembly 105, a gesture sensor 106 and a heading sensor 107, signal output ends of the gesture sensor 106 and the heading sensor 107 are connected to a signal input end of the controller 102, the intelligent operation platform 101 is bidirectionally connected to the controller 102, and input ends of the elevator control assembly 103, the right aileron control assembly 104 and the left aileron control assembly 105 are connected to an output end of the controller 102.
In this embodiment, the attitude sensor 106 is used to sense the pitch angle of the aircraft, the heading sensor 107 is used to sense the heading angle of the aircraft, according to the flight requirement, the intelligent operation platform 101 outputs the pitch control signal of the aircraft and the heading control signal of the aircraft to the controller 102, the controller 102 controls the lifting of the tail wing of the aircraft in the elevator control assembly 103 according to the received pitch control signal, so that the air current generates counter stress, the adjustment of the aircraft pitch is completed by pressing down or lifting the tail wing of the aircraft, the controller 102 controls the lifting of the right aileron in the right aileron rudder control assembly 104 and the lifting of the left aileron in the left aileron rudder control assembly 105 according to the received heading control signal, in the same time, the lifting force of the right aileron of the aircraft is reduced, the lifting force of the left aileron of the aircraft is increased, the lifting force of the left aileron is increased, the left aileron of the aircraft is tilted to the right side in the same time through pressure difference, the lifting force of the left aileron of the aircraft is reduced, the right aileron of the aircraft is lowered, the lifting of the left aileron is increased, and the lifting of the aircraft is more stable through the pressure difference, and the steering system is used to control the whole steering structure.
Further, the intelligent operation platform 101 includes a first control unit 108, a second control unit 109 and a display screen 110, the display screen 110 is located in front of the pilot, the first control unit 108 and the second control unit 109 are respectively located at two sides of the pilot, the display screen 110 is used for displaying pitch data and heading data of the aircraft, the first control unit 108 is used for outputting pitch control signals of the aircraft and controlling the elevation of the tail wing of the aircraft in the elevator control assembly 103 through the controller 102, and the second control unit 109 is used for outputting steering control signals of the aircraft and controlling the elevation of the right aileron in the right aileron control assembly 104 and the elevation of the left aileron control assembly 105 through the controller 102.
In this embodiment, the display screen 110 displays pitch data and heading data of the aircraft, the first control unit 108 outputs pitch control signals of the aircraft to the controller 102, the controller 102 controls the lifting of the tail wing of the aircraft in the elevator control assembly 103, the pitch control of the aircraft is completed, the second control unit 109 outputs steering control signals of the aircraft to the controller 102, and the controller 102 controls the lifting of the right aileron in the right aileron control assembly 104 and the lifting of the left aileron in the left aileron control assembly 105, so as to complete heading control of the aircraft.
Further, the first control unit 108 includes a first console 111, a first control push rod 112, a first infrared emitter 113, a plurality of first infrared receivers 114 and a plurality of second infrared receivers 115, the first control push rod 112 is rotatably connected to the first console 111, a pitch control cavity 116 is disposed in the first console 111, an arc structure is disposed at an inner bottom of the pitch control cavity 116, the first infrared emitter 113 is disposed at one end of the first control push rod 112 located in the pitch control cavity 116, a plurality of first infrared receivers 114 and a plurality of second infrared receivers 115 are disposed at an inner bottom of the pitch control cavity 116, a plurality of first infrared receivers 114 are uniformly distributed at a rear portion of the pitch control cavity 116, and a plurality of second infrared receivers 115 are uniformly distributed at a front portion of the pitch control cavity 116, and a first reset spring is disposed between two sides of the first control push rod 112 and a surface of the first console 111.
In this embodiment, the first control push rod 112 is pushed, so that the first infrared transmitter 113 corresponds to the first infrared receiver 114 and the second infrared receiver 115 in the pitch control cavity 116, the first infrared receiver 114 receiving the corresponding signals controls the aircraft tail in the elevator control assembly 103 to lift to a corresponding angle, so that the aircraft nose of the aircraft is pushed down to a corresponding angle, the second infrared receiver 115 receiving the corresponding signals controls the aircraft tail in the elevator control assembly 103 to push down to a corresponding angle, so that the aircraft nose of the aircraft is lifted up to a corresponding angle, so that the pitch control of the aircraft is more stable, and the first control push rod 112 is provided with the first reset spring 117, so that the operability of the first control push rod 112 is stronger.
Further, the second control unit 109 includes a second console 118, a second control push rod 119, a second infrared emitter 120, a plurality of third infrared receivers 121 and a plurality of fourth infrared receivers 122, a heading control cavity 123 is disposed in the second console 118, an inner bottom of the heading control cavity 123 is disposed in an arc structure, one end of the second control push rod 119 located in the heading control cavity 123 is provided with the second infrared emitter 120, a plurality of third infrared receivers 121 and a plurality of fourth infrared receivers 122 are disposed in an inner bottom of the heading control cavity 123, the third infrared receivers 121 are uniformly distributed in a rear portion of the heading control cavity 123, and a plurality of fourth infrared receivers 122 are uniformly distributed in a front portion of the heading control cavity 123, and a second reset spring 124 is disposed between two sides of the second control push rod 119 and a surface of the second console 118.
In this embodiment, the second control push rod 119 is pushed, so that the second infrared transmitter 120 corresponds to the third infrared receiver 121 and the fourth infrared receiver 122 in the heading control cavity 123, the third infrared receiver 121 that receives the corresponding signals controls the aircraft tail in the elevator control assembly 103 to lift to the corresponding angle, so that the aircraft nose of the aircraft is pushed down at the corresponding angle, the third infrared receiver 121 that receives the corresponding signals controls the right aileron in the right aileron control assembly 104 to lift to the corresponding angle, and controls the left aileron of the left aileron control assembly 105 to push down to the corresponding angle, so that the aircraft is tilted to the right side, the fourth infrared receiver 122 that receives the corresponding signals controls the right aileron in the right aileron control assembly 104 to push down to the corresponding angle, and controls the left aileron of the left aileron control assembly 105 to lift to the corresponding angle, so that the second aircraft is tilted to the left side, so that the second push rod 119 is more stable, and the heading is controlled by the second push rod is set.
Further, the first control push rod 112 and the second control push rod 119 are respectively provided with a mounting block 125, and the first return spring 117 and the second return spring 124 are respectively mounted between the mounting blocks 125 and the corresponding first control console 111 and second control console 118.
In this embodiment, the mounting block 125 is provided to facilitate the mounting of the first return spring 117 and the second return spring 124.
Further, each of the first return springs 117 and each of the second return springs 124 includes a spring body 126, a first connection block 127 and a second connection block 128, one end of the spring body 126 is provided with the first connection block 127, the other end of the spring body 126 is provided with the second connection block 128, the first connection block 127 is detachably connected with the corresponding first console 111 and second console 118, and the second connection block 128 is detachably connected with the corresponding mounting block 125.
In the present embodiment, the first connection block 127 is fixed to the corresponding first and second consoles 111 and 118 by using screws, and the second connection block 128 is fixed to the corresponding second connection block 128 by using screws, thereby completing the installation of the first and second return springs 117 and 124.
Further, a telescopic protection sleeve 129 is disposed outside each of the first return springs 117 and each of the second return springs 124, one end of the telescopic protection sleeve 129 is detachably connected to the corresponding first console 111 and second console 118, and the other end of the telescopic protection sleeve 129 is detachably connected to the corresponding mounting block 125.
In this embodiment, through the setting of the telescopic protection sleeve 129, the first return spring 117 and the second return spring 124 are protected, so that the influence of the external environment on the first return spring 117 and the second return spring 124 is avoided, and the overall structure of the intelligent operation platform 101 is more attractive.
Further, each telescopic protection sleeve 129 includes a protection sleeve body 130, a first fixing block 131 and a second fixing block 132, the protection sleeve body 130 is sleeved outside the corresponding spring body 126, one end of the protection sleeve body 130 is provided with the first fixing block 131, the other end of the protection sleeve body 130 is provided with the second fixing block 132, the first fixing block 131 is detached from and connected with the corresponding first console 111 and second console 118, and the second fixing block 132 is detached from and connected with the corresponding mounting block 125.
In the present embodiment, after the protective case body 130 is sleeved outside the corresponding spring body 126, the first fixing block 131 is mounted on the corresponding first console 111 and second console 118 by using screws, and the second fixing block 132 is mounted on the corresponding mounting block 125 by using screws, thereby completing the mounting of the telescopic protective case 129.
The above disclosure is only a preferred embodiment of the present invention, and it should be understood that the scope of the invention is not limited thereto, and those skilled in the art will appreciate that all or part of the procedures described above can be performed according to the equivalent changes of the claims, and still fall within the scope of the present invention.
Claims (6)
1. An intelligent steering device of motor Siemens Chemicals power M9-PD-35 is characterized in that,
the intelligent control system comprises an intelligent operation platform, a controller, an elevator control assembly, a right aileron control assembly, a left aileron control assembly, a gesture sensor and a course sensor, wherein the gesture sensor and the signal output end of the course sensor are connected with the signal input end of the controller, the intelligent operation platform is in bidirectional connection with the controller, and the input ends of the elevator control assembly, the right aileron control assembly and the left aileron control assembly are connected with the output end of the controller.
2. The Ma Daxi Qiche power M9-PD-35 intelligent steering device of claim 1,
the intelligent operation platform comprises a first control unit, a second control unit and a display screen, wherein the display screen is positioned in front of a pilot, the first control unit and the second control unit are respectively positioned on two sides of the pilot, the display screen is used for displaying pitching data and heading data of an airplane, the first control unit is used for outputting pitching control signals of the airplane and controlling lifting of an airplane tail wing in an elevator control assembly through a controller, the second control unit is used for outputting steering control signals of the airplane and controlling lifting of a right aileron in the right aileron control assembly and lifting of a left aileron of the left aileron control assembly through the controller.
3. The Ma Daxi Qiche power M9-PD-35 intelligent steering device of claim 2,
the first control unit comprises a first control console, a first control push rod, a first infrared emitter, a plurality of first infrared receivers and a plurality of second infrared receivers, the first control push rod is rotationally connected to the first control console, a pitching control cavity is formed in the first control console, the inner bottom of the pitching control cavity is in an arc-shaped structure, one end of the first control push rod, which is located in the pitching control cavity, is provided with the first infrared emitter, the inner bottom of the pitching control cavity is provided with a plurality of first infrared receivers and a plurality of second infrared receivers, the first infrared receivers are uniformly distributed at the rear part of the pitching control cavity, the second infrared receivers are uniformly distributed at the front part of the pitching control cavity, and first reset springs are arranged between the two sides of the first control push rod and the surface of the first control console.
4. The motor Sihci power M9-PD-35 intelligent steering apparatus of claim 3 wherein,
the second control unit comprises a second control console, a second control push rod, a second infrared emitter, a plurality of third infrared receivers and a plurality of fourth infrared receivers, a course control cavity is formed in the second control console, the inner bottom of the course control cavity is in an arc-shaped structure, one end of the second control push rod, which is located in the course control cavity, is provided with the second infrared emitter, the inner bottom of the course control cavity is provided with the plurality of third infrared receivers and the plurality of fourth infrared receivers, the plurality of third infrared receivers are uniformly distributed at the rear part of the course control cavity, the plurality of fourth infrared receivers are uniformly distributed at the front part of the course control cavity, and second reset springs are arranged between the two sides of the second control push rod and the surface of the second control console.
5. The Ma Daxi Qiche power M9-PD-35 intelligent steering device of claim 4,
the first control push rod and the second control push rod are respectively provided with a mounting block, and a first reset spring and a second reset spring which correspond to each other are mounted between the mounting blocks and the corresponding first control console and the corresponding second control console.
6. The Ma Daxi Qiche power M9-PD-35 intelligent steering device of claim 5,
each first reset spring and each second reset spring comprise a spring body, a first connecting block and a second connecting block, one end of the spring body is provided with the first connecting block, the other end of the spring body is provided with the second connecting block, the first connecting block is connected with the corresponding first control console and the second control console in a disassembling mode, and the second connecting block is connected with the corresponding mounting block in a disassembling mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311083302.5A CN117125251A (en) | 2023-08-24 | 2023-08-24 | Motor Siemens wedge power M9-PD-35 intelligent steering device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311083302.5A CN117125251A (en) | 2023-08-24 | 2023-08-24 | Motor Siemens wedge power M9-PD-35 intelligent steering device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117125251A true CN117125251A (en) | 2023-11-28 |
Family
ID=88862300
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202311083302.5A Pending CN117125251A (en) | 2023-08-24 | 2023-08-24 | Motor Siemens wedge power M9-PD-35 intelligent steering device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN117125251A (en) |
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2023
- 2023-08-24 CN CN202311083302.5A patent/CN117125251A/en active Pending
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