CN221766218U - Flight training is with simulation cockpit - Google Patents

Flight training is with simulation cockpit Download PDF

Info

Publication number
CN221766218U
CN221766218U CN202420111643.2U CN202420111643U CN221766218U CN 221766218 U CN221766218 U CN 221766218U CN 202420111643 U CN202420111643 U CN 202420111643U CN 221766218 U CN221766218 U CN 221766218U
Authority
CN
China
Prior art keywords
electric locomotive
simulation cabin
flight training
servo motor
guide rail
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.)
Active
Application number
CN202420111643.2U
Other languages
Chinese (zh)
Inventor
张学
高冰
杨升
李松
巩雨旺
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.)
Avic Tianjin Simulator Engineering Technology Co ltd
Original Assignee
Avic Tianjin Simulator Engineering 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 Avic Tianjin Simulator Engineering Technology Co ltd filed Critical Avic Tianjin Simulator Engineering Technology Co ltd
Priority to CN202420111643.2U priority Critical patent/CN221766218U/en
Application granted granted Critical
Publication of CN221766218U publication Critical patent/CN221766218U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Instructional Devices (AREA)

Abstract

The utility model discloses a simulated cockpit for flight training, and relates to the technical field of flight training equipment. Including the annular guide rail, the annular guide rail top is equipped with the contact net, and the annular guide rail below is equipped with the simulation cabin, is equipped with actuating mechanism on the annular guide rail, and electric locomotive movable mounting is on the annular guide rail, and electric locomotive upper surface fixed mounting has the butt joint base, is equipped with the pantograph on the butt joint base, has seted up the location spout on the electric locomotive, and electric locomotive bottom is equipped with the connection stabilizer blade, is equipped with elevating system between electric locomotive and the simulation cabin. The simulation cabin can be driven to move in the air through the electric locomotive, so that a real flight state is simulated, meanwhile, the servo motor can be started in the use process, the servo motor can drive the driving gear to rotate after being started, the driven gear can be driven to rotate after being driven to rotate, the driven gear can drive the wind-up roller on the driving shaft to rotate after being driven to rotate, and accordingly winding and unwinding of the traction rope are controlled, and lifting of an airplane is simulated.

Description

Flight training is with simulation cockpit
Technical Field
The utility model relates to the technical field of flight training equipment, in particular to a simulated cockpit for flight training.
Background
Along with the development of economy, roads are more and more congested, the traffic and transportation are rapidly expanded to a three-dimensional space, and the number of the demands of the aircrafts is more and more, so that gaps of the number of pilots are also caused, the training bases of the pilots are synchronously built, and the existing training equipment built or already built is mostly behind. The motion simulation only provides shaking, the shaking stroke is short, the real flight cannot be well simulated, the simulated steering centrifugal body feeling is difficult, and the improvement is still needed, so that the simulated cockpit for the flight training is provided.
Disclosure of utility model
The utility model mainly aims to provide a simulated cockpit for flight training, which can effectively solve the problems in the background art.
In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:
The utility model provides a flight training is with simulation cockpit, includes the annular guide rail, the annular guide rail top is equipped with the contact net, the annular guide rail below is equipped with the simulation cabin, be equipped with actuating mechanism on the annular guide rail, actuating mechanism includes pantograph, docking station, electric locomotive, location spout and connection stabilizer blade, electric locomotive movable mounting is on the annular guide rail, fixed surface installs docking station on the electric locomotive, be equipped with the pantograph on the docking station, the location spout has been seted up on the electric locomotive, the electric locomotive bottom is equipped with the connection stabilizer blade, be equipped with elevating system between electric locomotive and the simulation cabin, elevating system includes traction rope, wind-up roll, driven gear, servo motor and drive shaft, wind-up roll movable mounting is in the simulation cabin, fixed mounting has the drive shaft on the wind-up roll, driven gear is fixedly installed to drive shaft one side, be connected with traction rope on the wind-up roll, servo motor's output end is equipped with driving gear.
Furthermore, a movable wheel is arranged in the positioning sliding groove, and the electric locomotive is movably arranged on the annular guide rail through the movable wheel.
Furthermore, the pantograph is fixed on the electric locomotive through the butt joint base, the pantograph is contacted with the contact net, one end of the traction rope is connected to the bottom of the electric locomotive through the connecting support leg, and the other end of the traction rope is fixed on the wind-up roll.
Furthermore, bearings are arranged at two ends of the driving shaft, and the driving shaft is movably installed in the simulation cabin through the bearings.
Furthermore, the wind-up roll is movably arranged in the simulation cabin through a driving shaft, the driving gear is movably arranged on one side of the driven gear through a servo motor, and the driving gear is meshed with the driven gear.
Further, the simulation cabin is installed below the electric locomotive through a lifting mechanism.
Compared with the prior art, the utility model has the following beneficial effects:
During the use, can hang the simulation cabin below electric locomotive through the traction rope, and can drive the simulation cabin through electric locomotive and remove in the air to simulate real flight condition, can start servo motor in the use simultaneously, it can drive driving gear rotation after starting servo motor, and it can drive driven gear rotation after the driving gear rotation, and it can drive the epaxial wind-up roll of drive after the driven gear rotation to control the receive and release of traction rope, simulate the lift of aircraft.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic diagram of a driving mechanism according to the present utility model;
Fig. 3 is a schematic view of a lifting mechanism according to the present utility model.
In the figure: 1. contact net; 2. an annular guide rail; 3. a simulation cabin; 4. a driving mechanism; 401. a pantograph; 402. a butt joint base; 403. an electric locomotive; 404. positioning a chute; 405. a connecting support leg; 5. a lifting mechanism; 501. a traction rope; 502. a wind-up roll; 503. a driven gear; 504. a servo motor; 505. a drive gear; 506. a drive shaft.
Detailed Description
The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.
As shown in fig. 1 to 3, a flight training is with simulation cockpit, including ring rail 2, ring rail 2 top is equipped with contact net 1, ring rail 2 below is equipped with simulation cabin 3, be equipped with actuating mechanism 4 on the ring rail 2, actuating mechanism 4 includes pantograph 401, docking base 402, electric locomotive 403, location spout 404 and connection stabilizer 405, be equipped with elevating system 5 between electric locomotive 403 and the simulation cabin 3, elevating system 5 includes traction rope 501, wind-up roll 502, driven gear 503, servo motor 504 and drive shaft 506, simulation cabin 3 passes through elevating system 5 and installs in electric locomotive 403 below.
Be equipped with actuating mechanism 4 on the annular guide rail 2, actuating mechanism 4 includes pantograph 401, dock base 402, electric locomotive 403, location spout 404 and connection stabilizer blade 405, electric locomotive 403 movable mounting is on annular guide rail 2, fixed surface installs dock base 402 on the electric locomotive 403, be equipped with pantograph 401 on the dock base 402, set up location spout 404 on the electric locomotive 403, electric locomotive 403 bottom is equipped with connection stabilizer blade 405, pantograph 401 can improve power for electric locomotive 403 to make electric locomotive 403 forward motion, thereby drive simulation cabin 3 and remove in the sky, simulate the flight.
The lifting mechanism 5 is arranged between the electric locomotive 403 and the simulation cabin 3, the lifting mechanism 5 comprises a traction rope 501, a winding roller 502, a driven gear 503, a servo motor 504 and a driving shaft 506, the winding roller 502 is movably arranged in the simulation cabin 3, the driving shaft 506 is fixedly arranged on the winding roller 502, the driven gear 503 is fixedly arranged on one side of the driving shaft 506, the traction rope 501 is connected on the winding roller 502, the servo motor 504 is fixedly arranged on one side of the winding roller 502, the driving gear 505 is arranged at the output end of the servo motor 504, the driving gear 505 is driven to rotate after the servo motor 504 is started, the driven gear 503 is driven to rotate after the driving gear 505 rotates, the winding roller 502 on the driving shaft 506 is driven to rotate, and accordingly winding and unwinding of the traction rope 501 are controlled, and lifting of the simulation aircraft is simulated.
In practical use, the simulated cabin 3 is suspended below the electric locomotive 403 through the traction rope 501, the electric locomotive 403 is movably mounted on the annular guide rail 2 through the movable wheel due to the movable wheel arranged in the positioning chute 404, the pantograph 401 is fixed on the electric locomotive 403 through the docking base 402, the pantograph 401 is contacted with the contact net 1, one end of the traction rope 501 is connected to the bottom of the electric locomotive 403 through the connecting support leg 405, the other end of the traction rope 501 is fixed on the winding roller 502, the electric locomotive 403 can drive the simulated cabin 3 to move in the air, so that a real flying state is simulated, meanwhile, the servo motor 504 can be started in the use process, as the bearings are arranged at the two ends of the driving shaft 506, the driving shaft 506 is movably mounted in the simulated cabin 3 through the bearings, the winding roller 502 is movably mounted in the simulated cabin 3 through the driving shaft 506, the driving gear 505 is movably mounted on one side of the driven gear 503, and the driving gear 505 is meshed with the driven gear 503, so that the driving gear 505 can drive the driven gear 503 to rotate after the servo motor 504 is started, the driving gear 505 can drive the driving gear 503 to rotate, the winding roller 503 can be driven by the driving gear 503 to rotate, and then the driving gear 503 can be controlled to rotate, and the winding roller 503 can be controlled to rotate, so that the winding and the winding can be controlled to rotate.
Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims (6)

1. The utility model provides a flight training is with simulation cockpit which characterized in that: including ring rail (2), ring rail (2) top is equipped with contact net (1), ring rail (2) below is equipped with simulation cabin (3), be equipped with actuating mechanism (4) on ring rail (2), actuating mechanism (4) are including pantograph (401), docking station (402), electric locomotive (403), location spout (404) and connection stabilizer blade (405), electric locomotive (403) movable mounting is on ring rail (2), electric locomotive (403) upper surface fixed mounting has docking station (402), be equipped with pantograph (401) on docking station (402), location spout (404) have been seted up on electric locomotive (403), electric locomotive (403) bottom is equipped with connection stabilizer blade (405), be equipped with elevating system (5) between electric locomotive (403) and the simulation cabin (3), elevating system (5) are including traction rope (501), wind-up roll (502), driven gear (503), servo motor (504) and drive shaft (506), wind-up roll (502) movable mounting is in simulation cabin (3), wind-up roll (502) is equipped with location spout (404), drive shaft (506) fixed mounting, the winding roller (502) is connected with a traction rope (501), a servo motor (504) is fixedly arranged on one side of the winding roller (502), and a driving gear (505) is arranged at the output end of the servo motor (504).
2. A simulated cockpit for flight training as claimed in claim 1 wherein: the positioning chute (404) is internally provided with a movable wheel, and the electric locomotive (403) is movably arranged on the annular guide rail (2) through the movable wheel.
3. A simulated cockpit for flight training as claimed in claim 2 wherein: the pantograph (401) is fixed on the electric locomotive (403) through the butt joint base (402), and the pantograph (401) contacts with the contact net (1), traction rope (501) one end is connected in electric locomotive (403) bottom through connecting stabilizer blade (405), traction rope (501) other end is fixed on wind-up roll (502).
4. A simulated cockpit for flight training as claimed in claim 3 wherein: bearings are arranged at two ends of the driving shaft (506), and the driving shaft (506) is movably arranged in the simulation cabin (3) through the bearings.
5. A simulated cockpit for flight training as claimed in claim 4 wherein: the wind-up roll (502) is movably mounted in the simulation cabin (3) through a driving shaft (506), the driving gear (505) is movably mounted on one side of the driven gear (503) through a servo motor (504), and the driving gear (505) is meshed with the driven gear (503).
6. A simulated cockpit for flight training as claimed in claim 5 wherein: the simulation cabin (3) is arranged below the electric locomotive (403) through the lifting mechanism (5).
CN202420111643.2U 2024-01-16 2024-01-16 Flight training is with simulation cockpit Active CN221766218U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202420111643.2U CN221766218U (en) 2024-01-16 2024-01-16 Flight training is with simulation cockpit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202420111643.2U CN221766218U (en) 2024-01-16 2024-01-16 Flight training is with simulation cockpit

Publications (1)

Publication Number Publication Date
CN221766218U true CN221766218U (en) 2024-09-24

Family

ID=92791611

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202420111643.2U Active CN221766218U (en) 2024-01-16 2024-01-16 Flight training is with simulation cockpit

Country Status (1)

Country Link
CN (1) CN221766218U (en)

Similar Documents

Publication Publication Date Title
CN102133926B (en) Tailstock type vertical take-off and landing unmanned aerial vehicle
CN108312795B (en) Aerial-underwater paleocinetic amphibious aircraft and sailing method can be achieved in one kind
CN203528804U (en) Large-size rescue amphibious aircraft
CN201494622U (en) Wired electric flying and floating aircraft
CN206218213U (en) A kind of culvert type bionic Aircraft
CN101367436B (en) Miniature hybrid power flying platform and implementing method thereof
CN111959822A (en) Can demonstrate iron bird test bench of unmanned aerial vehicle take off and land power
CN105523182A (en) Vertaplane with front tilting rotor wing and rear tilting rotor wing
CN102975722A (en) Fast carrying structure used for transportation and uses thereof
US1825363A (en) Water plane
CN221766218U (en) Flight training is with simulation cockpit
CN212290389U (en) Can demonstrate iron bird test bench of unmanned aerial vehicle take off and land power
CN111137083B (en) Flying automobile
CN213168519U (en) Air-ground dual-purpose unmanned aerial vehicle
CN112373718A (en) Dual-purpose iron bird test bench of function is verified in area flight
CN109592072B (en) Water test flight method for large-scale amphibious aircraft
CN103847964B (en) A kind of can the arc shaped wing aircraft of vrille
CN106005412A (en) Flying saucer type vertical take-off and landing high-speed electromagnetic airplane
CN103646602B (en) Simulated ship-bone aircraft take-off and landing training platform
CN107284658B (en) Composite vertical/short-distance take-off and landing aircraft
CN206691363U (en) A kind of delta-wing aircraft of energy VTOL
CN205524948U (en) Unmanned autogyro
CN212891006U (en) Dual-purpose iron bird test bench of function is verified in area flight
CN2585812Y (en) Personal aerobat
CN106427435A (en) Triphibian flying vehicle

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant