A mechanical electronic attitude indicator used in flight simulators

Abstract

The present invention proposes a mechanical electronic attitude meter used in a flight simulator, which belongs to the field of aircraft instruments. The main board is connected to the second stepper motor through a second copper column, the micro through-hole slip ring is connected to the housing connector, the calibration disk is connected to the second stepper motor, the main board is connected to the housing connector through the second copper column, the calibration circuit board is fixed to the second copper column through a fastener, the mounting plate and the third dial mounting plate are fixedly mounted on the slip ring extension handle, the first stepper motor is fixedly connected to the slip ring extension handle, and the first copper column is respectively mounted on the third dial mounting plate and the mounting plate. The main feature is to simulate the flight speed of a real aircraft, and to be applied to the flight experience and training of a flight simulator, and to have an automatic calibration function, providing accurate data for application in a flight simulator. It is mainly used in the instrument part of a flight trainer.

Description

Technical Field

[0001] The invention belongs to the field of aircraft instruments, and in particular relates to a mechanical electronic attitude instrument used in a flight simulator. Background Art

[0002] At present, the market for simulation simulators is constantly expanding. In such an environment, in order to achieve a higher degree of simulation in simulators, we have conducted research on the functions of real electronic products of aircraft. Most of the existing ground flight simulators use instruments used on real aircraft. Such instruments are difficult to match with flight simulators and are relatively expensive. Summary of the invention

[0003] In order to solve the problems in the prior art, the present invention provides a mechanical electronic attitude indicator used in a flight simulator.

[0004] To achieve the above-mentioned purpose, the present invention adopts the following technical scheme: a mechanical electronic attitude instrument used in a flight simulator, comprising an adjusting knob, a meter head, a rotating electromagnet, a fault pointer, an adjusting pointer pressing sheet, a connecting plate, an electromagnet adjusting handle, a lens, an adjusting pointer, an upper shell, a third dial scale film, a third dial, a third dial mounting plate, a limiting piece, a second dial mounting handle, a second dial mounting handle reinforcing rod, a first dial scale film I, a second dial, a first dial scale film II, a first dial, a first stepping motor, a first copper column, a mounting plate, a slip ring extension handle, a calibration disk, a calibration circuit board, a micro through-hole slip ring, a shell connector, a mainboard, a second copper column, a second stepping motor, a lower shell and a back cover;

[0005] The main board is connected to the second stepper motor through the second copper column, the micro through-hole slip ring is connected to the housing connector, the calibration disk is connected to the second stepper motor, the main board is connected to the housing connector through the second copper column, the calibration circuit board is fixed to the second copper column by a fastener, the mounting plate and the third dial mounting plate are fixedly mounted on the slip ring extension handle, the first stepper motor is fixedly connected to the slip ring extension handle, the first copper column is respectively mounted on the third dial mounting plate and the mounting plate, the limit plate, the second dial mounting handle reinforcement rod and the second dial mounting handle are sequentially connected and then mounted on the first On the stepper motor, the first dial is fixedly connected to the extended handle of the slip ring and then coated with the first dial scale film II, the second dial is fixedly connected to the second dial mounting handle and then coated with the first dial scale film I, the third dial is fixedly connected to the first copper column and then coated with the third dial scale film, the rotating electromagnet is installed and connected to the connecting plate and the fault pointer is fixed on the electromagnet adjustment handle, the adjustment pointer pressing piece is fixedly connected to the adjustment pointer, the lens is embedded in the header slot after the adjustment knob and the header are installed, and the back cover, the lower shell, the shell connector, the upper shell, the connecting plate and the header are connected in sequence.

[0006] Furthermore, a light emitting diode is provided on the connecting plate.

[0007] Furthermore, the specifications of the micro through-hole slip ring are inner hole 5mm, outer diameter 22mm, 6-way, and flange.

[0008] Furthermore, the first copper column is a knurled copper column.

[0009] Furthermore, the lens is made of transparent acrylic material.

[0010] Furthermore, the reduction ratio of the first stepper motor is 30.

[0011] Compared with the prior art, the invention has the following beneficial effects: the main feature of the invention is to simulate the flight speed of a real aircraft and apply it to the flight experience and training of a flight simulator, and it has an automatic calibration function to provide accurate data for application in a flight simulator. It can better output accurate data, making flight training more realistic and accurate. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 The present invention is a schematic structural diagram of a mechanical electronic attitude indicator used in a flight simulator.

[0013] 1-adjusting knob, 2-meter head, 3-rotating electromagnet, 4-fault pointer, 5-adjusting pointer pressure piece, 6-connecting plate, 7-electromagnet adjustment handle, 8-lens, 11-adjusting pointer, 12-light-emitting diode, 13-upper shell, 14-third dial scale film, 15-third dial, 17-third dial mounting plate, 19-limiting piece, 21-second dial mounting handle, 22-second dial mounting handle reinforcement rod, 25-first dial scale film I, 26-second dial, 27-first dial scale film II, 28-first dial, 29-first stepper motor, 30-first copper column, 31-mounting plate, 32-slip ring extension handle, 33-calibration disk, 34-calibration circuit board, 35-micro through-hole slip ring, 38-shell connector, 39-main board, 40-second copper column, 42-second stepper motor, 43-lower shell, 44-back cover. DETAILED DESCRIPTION

[0014] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0015] See also Figure 1The present embodiment is described, a mechanical electronic attitude meter used in a flight simulator, comprising an adjusting knob 1, a meter head 2, a rotating electromagnet 3, a fault pointer 4, an adjusting pointer pressing piece 5, a connecting plate 6, an electromagnet adjusting handle 7, a lens 8, an adjusting pointer 11, an upper housing 13, a third dial scale film 14, a third dial 15, a third dial mounting plate 17, a stopper 19, a second dial mounting handle 21, a second dial mounting handle reinforcing rod 22, a first dial scale film I 25, a second dial 26, a first dial scale film II 27, a first dial 28, a first stepping motor 29, a first copper column 30, a mounting plate 31, a slip ring extension handle 32, a calibration disk 33, a calibration circuit board 34, a micro through-hole slip ring 35, a housing connector 38, a main board 39, a second copper column 40, a second stepping motor 42, a lower housing 43 and a back cover 44;

[0016] The main board 39 is connected to the second stepper motor 42 through the second copper column 40, the micro through-hole slip ring 35 is connected to the housing connector 38, the calibration disk 33 is connected to the second stepper motor 42, the main board 39 is connected to the housing connector 38 through the second copper column 40, the calibration circuit board 34 is fixed to the second copper column 40 by a fastener, the mounting plate 31 and the third dial mounting plate 17 are fixedly mounted on the slip ring extension handle 32, the first stepper motor 29 is fixedly connected to the slip ring extension handle 32, the first copper column 30 is respectively mounted on the third dial mounting plate 17 and the mounting plate 31, the limit plate 19, the second dial mounting handle reinforcement rod 22 and the second dial mounting handle 21 are sequentially connected and then mounted on On the first stepper motor 29, the first dial 28 is fixedly connected to the slip ring extension handle 32 and then coated with the first dial scale film II 27, the second dial 26 is fixedly connected to the second dial mounting handle 21 and then coated with the first dial scale film I 25, the third dial 15 is fixedly connected to the first copper column 30 and then coated with the third dial scale film 14, the rotating electromagnet 3 is installed and connected to the connecting plate 6 and then the fault pointer 4 is fixed on the electromagnet adjustment handle 7, the adjustment pointer pressing piece 5 and the adjustment pointer 11 are fixedly connected, the adjustment knob 1 and the header 2 are installed and then the lens 8 is embedded in the header 2 groove, the back cover 44, the lower shell 43, the shell connector 38, the upper shell 13, the connecting plate 6 and the header 2 are connected in sequence.

[0017] The main operation logic of this embodiment is to form a data link according to the flight software data of the simulator after power-on to drive the motor to control the rotation of the pointer to reach the corresponding data scale. Preferably, the connecting plate 6 is provided with a light-emitting diode 12, the specifications of the micro through-hole slip ring 35 are 5mm inner hole, 22mm outer diameter, 6-way, with flange, the first copper column 30 is a knurled copper column, the lens 8 is made of transparent acrylic material, and the first stepper motor 29 has a reduction ratio of 30. The position, accuracy and speed of the motor are controlled by computer data, so as to provide a better flight training environment.

[0018] The mechanical electronic attitude indicator used in a flight simulator provided by the present invention is introduced in detail above. Specific examples are used in this article to illustrate the principle and implementation mode of the present invention. The description of the above embodiments is only used to help understand the method of the present invention and its core idea. At the same time, for those skilled in the art, according to the idea of ​​the present invention, there will be changes in the specific implementation mode and application scope. In summary, the content of this specification should not be understood as limiting the present invention.

Claims

1. A mechanical electronic attitude indicator for a flight simulator, characterized in that: It comprises an adjusting knob (1), a meter head (2), a rotating electromagnet (3), a fault pointer (4), an adjusting pointer pressing piece (5), a connecting plate (6), an electromagnet adjusting handle (7), a lens (8), an adjusting pointer (11), an upper shell (13), a third dial scale film (14), a third dial (15), a third dial mounting plate (17), a limiting plate (19), a second dial mounting handle (21), a second dial mounting handle reinforcing rod (22), a first dial scale film I (25), a second dial (26), a first dial scale film II (27), a first dial (28), a first stepping motor (29), a first copper column (30), a mounting plate (31), a slip ring extension handle (32), a calibration disk (33), a calibration circuit board (34), a micro through-hole slip ring (35), a shell connecting piece (38), a main board (39), a second copper column (40), a second stepping motor (42), a lower shell (43) and a back cover (44); The main board (39) is connected to the second stepper motor (42) via the second copper column (40), the micro through-hole slip ring (35) is connected to the housing connector (38), the calibration disk (33) is connected to the second stepper motor (42), the main board (39) is connected to the housing connector (38) via the second copper column (40), the calibration circuit board (34) is fixed to the second copper column (40) via a fastener, the mounting plate (31) and the third dial mounting plate (17) are fixedly mounted on the slip ring extension handle (32), the first stepper motor (29) is fixedly connected to the slip ring extension handle (32), the first copper column (30) is respectively mounted on the third dial mounting plate (17) and the mounting plate (31), the limiting plate (19), the second dial mounting handle reinforcing rod (22) and the second dial mounting handle (21) are sequentially connected and then mounted on the first stepper motor (29). On the motor (29), the first dial (28) is fixedly connected to the slip ring extension handle (32) and then coated with the first dial scale film II (27); the second dial (26) is fixedly connected to the second dial installation handle (21) and then coated with the first dial scale film I (25); the third dial (15) is fixedly connected to the first copper column (30) and then coated with the third dial scale film (14); the rotating electromagnet (3) is connected to the connecting plate (6) and then the fault pointer (4) is fixed on the electromagnet adjustment handle (7); the adjusting pointer pressing piece (5) and the adjusting pointer (11) are fixedly connected; after the adjusting knob (1) and the meter head (2) are installed, the lens (8) is embedded in the meter head (2) groove; the back cover (44), the lower shell (43), the shell connector (38), the upper shell (13), the connecting plate (6) and the meter head (2) are connected in sequence.

2. The mechanical electronic attitude indicator used in a flight simulator according to claim 1, characterized in that: The connecting plate (6) is provided with a light emitting diode (12).

3. The mechanical electronic attitude indicator used in a flight simulator according to claim 1, characterized in that: The specifications of the miniature through-hole slip ring (35) are: inner hole 5mm, outer diameter 22mm, 6-way, and flange.

4. The mechanical electronic attitude indicator used in a flight simulator according to claim 1, characterized in that: The first copper column (30) is a knurled copper column.

5. The mechanical electronic attitude indicator used in a flight simulator according to claim 1, characterized in that: The lens (8) is made of transparent acrylic material.

6. The mechanical electronic attitude indicator used in a flight simulator according to claim 1, characterized in that: The first stepper motor (29) has a reduction ratio of 30.

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