CN202838724U - Simulated flight management computer FMC - Google Patents

Simulated flight management computer FMC Download PDF

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Publication number
CN202838724U
CN202838724U CN 201220504932 CN201220504932U CN202838724U CN 202838724 U CN202838724 U CN 202838724U CN 201220504932 CN201220504932 CN 201220504932 CN 201220504932 U CN201220504932 U CN 201220504932U CN 202838724 U CN202838724 U CN 202838724U
Authority
CN
China
Prior art keywords
interface
circuit board
simulated flight
fmc
button
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN 201220504932
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Chinese (zh)
Inventor
胡伟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
TIANJIN AOJET AVIATION TECHNOLOGY Co Ltd
Original Assignee
TIANJIN AOJET AVIATION TECHNOLOGY Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by TIANJIN AOJET AVIATION TECHNOLOGY Co Ltd filed Critical TIANJIN AOJET AVIATION TECHNOLOGY Co Ltd
Priority to CN 201220504932 priority Critical patent/CN202838724U/en
Application granted granted Critical
Publication of CN202838724U publication Critical patent/CN202838724U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a simulated flight management computer FMC, including a display, left execution keys, right execution keys, function keys, number input keys, and English letter input keys. All the keys are connected to a key circuit board. A 12V power interface, a USB interface and a VGA interface are provided on the key circuit board. The 12V power interface on the key circuit board is a direct current 12V interface. The USB interface provided on the key circuit board is an interface to realize the communication between the simulated flight management computer FMC with a computer. The simulated flight management computer FMC device in the utility model can make trainees experience the flight simulation flight management computer FMC functions and operation force, has strong sense of reality, and greatly improves the aircraft simulation fidelity.

Description

Simulated flight supervisory computer FMC
Technical field
The utility model relates to a kind of simulated flight supervisory computer FMC, belongs to the virtual emulation field.
Background technology
Simulated flight supervisory computer FMC is the aloft flight management of a kind of simulation present generation aircraft and navigator, is exactly the device by FMC in the Reality simulation aircraft, provides synthetic flight training a real FMC operating environment.The function of simulated flight supervisory computer FMC realizes at present, finishes by software simulation on PC.The weak point of the operation format of this simulation is that the sense of reality is not strong, can't realize the true button operation of FMC, thereby not reach teaching result.
Summary of the invention
For above-mentioned prior art, in order to overcome simulated flight supervisory computer FMC in the prior art, the deficiency of modeling scheme, the utility model provides a kind of simulated flight supervisory computer FMC, button operation wherein and layout are all consistent with the FMC in the true aircraft, the trainee is by simulated flight supervisory computer FMC equipment, can sense of reality to the method for operating of Flight Management Computer FMC.
In order to solve the problems of the technologies described above, the technical scheme that the utility model simulated flight supervisory computer FMC is achieved is: comprise display screen, left execution button, right execution button, function button, digital input key, English alphabet input key; All buttons are connected on the button circuit board, and the 12V power interface is arranged on the button circuit board, USB interface, VGA interface.
Described display screen is 5 inches display screens of liquid crystal.
Described display screen has the VGA interface, and the demonstration output function is provided.
Described left execution button, right execution button, function button, digital input key, English alphabet input key all are connected on the button circuit board.
The 12V power interface is direct current 12V on the described button circuit board, for display screen provides power supply.
Described button circuit board provides USB interface, realizes the interface that is connected by communication between simulated flight supervisory computer FMC and the computing machine.
Compared with prior art, the beneficial effects of the utility model are: by simulated flight supervisory computer FMC equipment, make the trainee personal experiences arrive simulated flight supervisory computer FMC function and operating force, strong sense of reality is significantly promoted the validity of aircraft simulation.
Description of drawings
Fig. 1 is the utility model simulated flight supervisory computer FMC synoptic diagram;
Fig. 2 is back side simulated flight supervisory computer FMC synoptic diagram of the present utility model;
Among Fig. 1: 1-display screen, the left execution button of 2-, the right execution button of 3-, 4-function button, 5-numeral input key, 6-English alphabet input key.
Among Fig. 2: 7-button circuit board, 8-12V power interface, 9-USB interface, 10-VGA interface.
Embodiment
Below in conjunction with embodiment the utility model is described in further detail.
As shown in Figure 1 and Figure 2, this simulated flight supervisory computer FMC comprises display screen (1), left execution button (2), right execution button (3), function button (4), digital input key (5), English alphabet input key (6), button circuit board (7), 12V power interface (8), USB interface (9), VGA interface (10).
Display screen (1) is 5 inches display screens of liquid crystal.Left execution button (2), right execution button (3), function button (4), digital input key (5), English alphabet input key (6) all are connected on the button circuit board (7).
There is VGA interface (10) that the demonstration output function is provided on the button circuit board (7).
12V power interface (8) on the button circuit board (7) is direct current 12V, for display screen provides power supply.
Button circuit board (7) provides the USB interface that links to each other with computing machine (9), realizes the interface that is connected by communication between simulated flight supervisory computer FMC and the computing machine.
Use the utility model simulated flight supervisory computer FMC, make the trainee personal experiences arrive flight simulation Flight Management Computer FMC function and operating force.
Although the above is described the utility model in conjunction with figure; but the utility model is not limited to above-mentioned embodiment; above-mentioned embodiment only is schematic; rather than restrictive; those of ordinary skill in the art is under enlightenment of the present utility model; in the situation that does not break away from the utility model aim, the technical scheme that the equal replacement of all employings or equivalent transformation form, these all belong within the protection domain of the present utility model.

Claims (4)

1. simulated flight supervisory computer FMC, mainly comprise display screen (1), left execution button (2), right execution button (3), function button (4), numeral input key (5), English alphabet input key (6), button circuit board (7), 12V power interface (8), USB interface (9), VGA interface (10), it is characterized in that: display screen (1) is 5 inches display screens of liquid crystal, left execution button (2), right execution button (3), function button (4), numeral input key (5), English alphabet input key (6) all is connected on the button circuit board (7).
2. simulated flight supervisory computer FMC according to claim 1 is characterized in that: have VGA interface (10) that the demonstration output function is provided on the described button circuit board (7).
3. simulated flight supervisory computer FMC according to claim 1, it is characterized in that: the 12V power interface (8) on the described button circuit board (7) is direct current 12V, for display screen provides power supply.
4. simulated flight supervisory computer FMC according to claim 1, it is characterized in that: described button circuit board (7) provides the USB interface that links to each other with computing machine (9), realizes the interface that is connected by communication between simulated flight supervisory computer FMC and the computing machine.
CN 201220504932 2012-09-29 2012-09-29 Simulated flight management computer FMC Expired - Fee Related CN202838724U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220504932 CN202838724U (en) 2012-09-29 2012-09-29 Simulated flight management computer FMC

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220504932 CN202838724U (en) 2012-09-29 2012-09-29 Simulated flight management computer FMC

Publications (1)

Publication Number Publication Date
CN202838724U true CN202838724U (en) 2013-03-27

Family

ID=47950372

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220504932 Expired - Fee Related CN202838724U (en) 2012-09-29 2012-09-29 Simulated flight management computer FMC

Country Status (1)

Country Link
CN (1) CN202838724U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3007154A1 (en) * 2014-10-11 2016-04-13 Air China Limited Simulation device of flight management system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3007154A1 (en) * 2014-10-11 2016-04-13 Air China Limited Simulation device of flight management system
US10607499B2 (en) 2014-10-11 2020-03-31 Air China Limited Simulation device for a flight management system

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130327

Termination date: 20140929

EXPY Termination of patent right or utility model