CN105654809A

CN105654809A - Full-angle aviation simulation equipment

Info

Publication number: CN105654809A
Application number: CN201610028962.7A
Authority: CN
Inventors: 王建雄
Original assignee: Individual
Current assignee: Individual
Priority date: 2016-01-10
Filing date: 2016-01-10
Publication date: 2016-06-08

Abstract

The invention aims to provide an aviation analog platform capable of performing full-angle flight simulation. The platform comprises a cylinder base, a "concave" type support with an internal tooth convolution bearing, an annular frame, an inner projection ball screen, an aviation simulation seat, a power supply system, a motion system and a control system. The aviation simulation platform capable of performing full-angle flight simulation is characterized in that an aviator can carry out control on the simulation seat in the ball screen, so that the whole ball screen including the aviator is enabled to realize the flight simulation at any angle. The aviation analog platform is a professional aviation simulation equipment platform.

Description

A kind of full angle flight simulation equipment

Technical field

The present invention provides a kind of flight simulation platform that can realize full angle flight simulation and omnidirectional's simulation visual angle, the rotational angle of drive system is controlled by controller, realize platform and carry out arbitrarily angled control on X Y Z axis, intend true degree so as to improving flight. It it is the flight-simulation equipment platform of a kind of specialty. Belong to novel mechanical, virtual technology, technical field of flight control.

Background technology

For flight simulation equipment (or claiming aviation simulator), current technology background is that most flight simulation platform are built upon on Stewart platform both at home and abroad, although Stewart platform can do six-freedom motion, but its shortcoming is cannot truly to simulate rolling and the At High Angle of Attack action that pilot makes with aircraft, meanwhile, all of flight simulation equipment including the U.S. also fails to provide omnidirectional's simulation visual angle. As for eased flight simulation equipment, only simulator fixed on the ground, carry out solid-state operation by a flat liquid crystal display screen. In a word, conventional flight simulation equipment all greatly reduces the true degree of plan of flight, and meanwhile, low substitution feels the practice ability that also limit pilot.

Summary of the invention

It is an object of the invention to provide a kind of flight simulation platform that can carry out full angle flight simulation. Including cylindrical seat, with " recessed " type support of internal tooth convolution supporting, annular framework, interior pitching curtain, flight simulation seat, power-supply system, action system, control system, it is characterized in can passing through pilot's simulation seat in ball curtain manipulate so that include the flight simulation that the whole ball curtain of pilot realizes on arbitrarily angled.

Accompanying drawing explanation

Fig. 1 is the front view of this invention. Wherein cylindrical seat 1, with " recessed " type support 2 of internal tooth convolution supporting, annular framework 3, interior pitching curtain 4, flight simulation seat 5, power-supply system 6, drive system 7.1, drive system 7.2

Fig. 2 is the side view of this invention. Wherein cylindrical seat 1, " recessed " the type support 2 of supporting of circling round with internal tooth, annular framework 3, interior pitching curtain, 4, flight simulation seat 5, power-supply system 6, drive system 7.1

Fig. 3 is the top view of this invention. Wherein with " recessed " type support 2 of internal tooth convolution supporting, annular framework 3, interior pitching curtain 4, flight simulation seat 5, power-supply system 6, drive system 7.1, drive system 7.2

Detailed description of the invention

Specific embodiment, an operation principle of this patent are expanded on further below in conjunction with accompanying drawing.

Such as Fig. 1, flight simulation seat 5 is supplied electricity to by power-supply system 6, interior pitching curtain 4 is driven to do "Left"-deviationist, Right deviation action around annular framework 3 by drive system 7.2, simultaneously, flight simulation seat 5 makes annular framework 3 carry out pitching motion around " recessed " the type support 2 with internal tooth convolution supporting also by drive system 7.1, finally, the flight simulation seat 5 drive system by hiding in cylindrical seat, make to make left-right rotation action with " recessed " type support 2 of internal tooth convolution supporting.

Fig. 2 side view and Fig. 3 top view principle are with described in Fig. 1.

Such as Fig. 1, operation principle is as follows:

When pilot manipulation simulates seat time, include the interior pitching curtain 4 of pilot, flight simulation seat 5,360 degree of rotations that drive system 7.1 realizes carrying out around X-axis can be passed through respectively, realized the 360 degree of rotations carried out around Y-axis by drive system 7.2, realized the 360 degree of rotations carried out around Z axis by cylindrical seat 1. By the control realization full angle flight simulation to all drive system.

Claims

1. a full angle flight simulation equipment, including cylindrical seat, with " recessed " type support (hereinafter referred to as " ' recessed ' type support ") of internal tooth convolution supporting, annular framework, interior pitching curtain, flight simulation seat, power-supply system, drive system, control system, it is characterized in that: by pilot's simulation seat in ball curtain manipulates, it is possible to make the whole ball curtain including pilot realize the flight simulation on arbitrarily angled.

2. flight simulation equipment according to claim 1, it is characterised in that: in cylindrical seat, it is provided with one group of drive system, and this drive system is controlled by the side-to-side movement of gear mesh " recessed " type support.

3. flight simulation equipment according to claim 1, it is characterised in that: annular framework is located on two end points of " recessed " type support by pedestal, and has drive system that the elevating movement of annular framework is controlled in end points.

4. flight simulation equipment according to claim 1, it is characterised in that: interior pitching curtain is included among annular framework, and is docked with annular framework by two axles, and drive system is controlled by the rotation of wherein internal pitching curtain of axle.

5. flight simulation equipment according to claim 1, it is characterised in that: flight simulation seat and power-supply system are built-in and be fixed among interior pitching curtain, and the space of interior pitching curtain is enough to make flight simulation seat therein sit into 1 to 2 pilot.