CN208043053U - A kind of altimeter suitable for flight simulator - Google Patents

Abstract

The utility model relates to the technical field of aircraft flight simulators, in particular to an altimeter suitable for flight simulators. The large gear assembly is clamped between the air pressure dial and the uniform light plate, and the height indicating plate is arranged on the upper end of the air pressure dial. The thin pointer is arranged on the upper end of the height indicating plate, the installation panel is arranged on the upper end of the thin pointer, and a long pointer and a short pointer are respectively arranged between the installation panel and the thin pointer. Beneficial effects of the utility model: the utility model drives a mechanical gear mechanism through a stepping motor or a steering gear, the gear mechanism is connected with the instrument pointer, drives the instrument pointer to rotate through the driving gear mechanism, and finally directly displays the aircraft flight through the installation panel display mechanism The adjustment knob on the instrument panel can adjust the zero point indicated by the altimeter, so as to realize the adjustment of the zero point indicated by the instrument under different conditions.

Description

A kind of altimeter suitable for flight simulator

technical field

The utility model relates to the technical field of aircraft flight simulators, in particular to an altimeter suitable for flight simulators.

Background technique

The altimeter is an instrument that measures and indicates the vertical distance of the aircraft from a selected horizontal datum, and reflects the flight altitude of the aircraft to the flight crew in the form of visual signals. As a professional equipment for flight training, the flight simulator requires that the functions of the flight simulator altimeter during the simulated training flight and the real aircraft altimeter during flight should be as consistent as possible. This helps to increase the sense of reality of training and enhance user experience in flight simulation training.

Therefore, it is necessary to propose an altimeter suitable for flight simulators for the above problems.

Utility model content

Aiming at the deficiencies in the above-mentioned prior art, the purpose of this utility model is to provide an altimeter suitable for flight simulators.

An altimeter suitable for flight simulators, comprising a mounting panel, a thin pointer, an altitude indicator plate, an air pressure dial, a large gear assembly and a dodging plate, the large gear assembly is clamped between the air pressure dial and the dodging plate, The altitude indicating plate is arranged on the upper end of the air pressure dial, the thin pointer is arranged on the upper end of the altitude indicating plate, the installation panel is arranged on the upper end of the thin pointer, and a long pointer is arranged between the installation panel and the thin pointer and short pointers.

Preferably, a backlight panel is provided at the lower end of the dodging plate, a transmission mechanism cover is provided at the lower end of the backlight panel, and a transmission mechanism bottom plate is provided at the lower end of the transmission mechanism cover.

Preferably, a speed change mechanism is provided between the speed change mechanism cover plate and the speed change mechanism bottom plate, and the speed change mechanism is drivingly connected to a stepping motor or a steering gear.

Preferably, one side of the installation panel is provided with an adjustment knob.

Preferably, the adjustment knob is engaged with the bull gear assembly.

Preferably, the upper end of the installation panel is provided with a transparent cover.

Due to the adoption of the above technical scheme, the utility model has beneficial effects: the utility model drives a mechanical gear mechanism through a stepping motor or a steering gear, the gear mechanism is connected with the instrument pointer, and the instrument pointer is driven to rotate through the driving gear mechanism, and finally the panel display mechanism is installed It intuitively shows the flying altitude of the aircraft, and the adjustment knob on the instrument panel can adjust the zero point indicated by the altimeter, so as to realize the adjustment of the zero point indicated by the instrument under different circumstances.

Description of drawings

Fig. 1 is a structural diagram of the utility model;

Fig. 2 is a schematic diagram of the unfolded state of the utility model;

Reference signs in the figure: 1. Transparent watch cover, 2. Adjusting knob, 3. Installation panel, 4. Long pointer, 5. Short pointer, 6. Thin pointer, 7. Altitude indicator plate, 8. Air pressure dial, 9 . Large gear assembly, 10. Uniform light plate, 11. Backlight panel, 12. Cover plate of speed change mechanism, 13. Speed change mechanism, 14. Base plate of speed change mechanism.

Detailed ways

The embodiments of the utility model will be described in detail below in conjunction with the accompanying drawings, but the utility model can be implemented in various ways defined and covered by the claims.

As shown in Fig. 1 and in conjunction with Fig. 2, a kind of altimeter suitable for a flight simulator includes a mounting panel 3, a thin pointer 6, an altitude indicator plate 7, an air pressure dial 8, a large gear assembly 9 and a dodging plate 10. The large gear assembly 9 is clamped between the air pressure dial 8 and the dodging plate 10, the height indicating plate 7 is arranged on the upper end of the air pressure dial 8, the thin pointer 6 is arranged on the upper end of the height indicating plate 7, and the The installation panel 3 is arranged on the upper end of the thin pointer 6 , and the long pointer 4 and the short pointer 5 are respectively arranged between the installation panel 3 and the thin pointer 6 .

Wherein, the lower end of the uniform light plate 10 is provided with a backlight panel 11 , the lower end of the backlight panel 11 is provided with a transmission mechanism cover 12 , and the lower end of the transmission mechanism cover 12 is provided with a transmission mechanism bottom plate 14 .

In addition, a speed change mechanism 13 is arranged between the speed change mechanism cover plate 12 and the speed change mechanism bottom plate 14, and the speed change mechanism 13 is drivingly connected with a stepping motor or a steering gear, and one side of the installation panel 3 is provided with an adjustment knob 2.

Wherein, the adjustment knob 2 is engaged with the large gear assembly 9 , and the upper end of the installation panel 3 is provided with a transparent cover 1 .

The utility model drives a mechanical gear mechanism through a stepping motor or a steering gear, the gear mechanism is connected with the instrument pointer, drives the instrument pointer to rotate through the driving gear mechanism, and finally directly displays the flying height of the aircraft through the installation panel display mechanism. The adjustment knob can adjust the zero position indicated by the altimeter, so as to realize the adjustment of the zero point indicated by the instrument under different circumstances.

The utility model enables the simulated aircraft to have the same flight height display as that of the real aircraft during training, allowing users to have the feeling of real flight during operation, and redesigns the structure according to the existing technical conditions to instruct the training of the flight simulator altitude of the aircraft.

The actuator selected by the flight simulator altimeter is a stepping motor or a steering gear, which drives the corresponding mechanical gear mechanism through the stepping motor or steering gear, so that the altimeter indicates the flight altitude in the flight simulation training. In this way, the altimeter of the flight simulator can visually display the flight altitude

The mechanical gear mechanism is driven by a stepping motor or a steering gear, and the gear mechanism is connected with the instrument pointer, and the instrument pointer is driven to rotate through the driving gear mechanism, and finally the flight height of the aircraft is intuitively displayed through the installation panel display mechanism.

The adjustment knob on the instrument panel can adjust the zero position indicated by the altimeter, so as to realize the adjustment of the zero point indicated by the instrument under different conditions.

The above descriptions are only preferred embodiments of the present utility model, and are not therefore limiting the patent scope of the present utility model. Any equivalent structure or equivalent process transformation made by using the specification of the utility model and the contents of the accompanying drawings may be directly or indirectly used in Other relevant technical fields are all included in the patent protection scope of the present utility model in the same way.

Claims (6)

1. A kind of altimeter that is applicable to flight simulator is characterized in that: comprise mounting panel, thin pointer, altitude indicator plate, air pressure dial, large gear assembly and dodging plate, described large gear assembly is clamped on the air pressure dial Between the dodging plate, the height indicator plate is set on the upper end of the air pressure dial, the thin pointer is set on the upper end of the height indicator plate, the installation panel is set on the upper end of the thin pointer, and the distance between the installation panel and the thin pointer is There are long pointers and short pointers respectively. 2. A kind of altimeter suitable for flight simulator as claimed in claim 1, characterized in that: the lower end of the uniform light plate is provided with a backlight panel, and the lower end of the backlight panel is provided with a speed change mechanism cover plate, the The lower end of the speed change mechanism cover plate is provided with a speed change mechanism bottom plate. 3. A kind of altimeter suitable for flight simulator as claimed in claim 2, characterized in that: a speed change mechanism is arranged between the cover plate of the speed change mechanism and the bottom plate of the speed change mechanism, and the speed change mechanism is connected with a stepping motor or Servo drive connection. 4. The altimeter suitable for flight simulators according to claim 1, wherein an adjustment knob is provided on one side of the installation panel. 5. The altimeter suitable for flight simulators according to claim 4, wherein the adjustment knob is engaged with the large gear assembly. 6 . The altimeter suitable for flight simulators according to claim 1 , wherein a transparent cover is provided on the upper end of the installation panel. 7 .