CN108074433A - A kind of tiptoe brake weight induction device for flight simulator - Google Patents
A kind of tiptoe brake weight induction device for flight simulator Download PDFInfo
- Publication number
- CN108074433A CN108074433A CN201711474083.8A CN201711474083A CN108074433A CN 108074433 A CN108074433 A CN 108074433A CN 201711474083 A CN201711474083 A CN 201711474083A CN 108074433 A CN108074433 A CN 108074433A
- Authority
- CN
- China
- Prior art keywords
- piston
- housing
- tiptoe
- brake weight
- induction device
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
Abstract
The invention provides a kind of tiptoe brake weight induction device for flight simulator, including sequentially connected push rod 1, piston 5, spring 11, housing 6 and slide-wire rheostat 10, push rod 1 is arranged in the installation sky on 5 top of piston, spring 11 is set in the protrusion of 5 lower part of piston, spring 11 is co-located on piston 5 in the inner cavity of housing 6, piston 5 is fixed on by plug screw 7 on housing 6, slide rheostat 10 is arranged on the lateral wall of housing 6, slide-wire rheostat is equipped with the sliding bar 13 moved up and down, and 13 top of sliding bar passes through the fixation parallel with push rod of connection sheet 2.The invention is simple in structure, of low cost, avoids the manipulation load control system using complex and expensive, while convenient for safeguarding and adjusting, can meet the simulation requirements of the tiptoe brake weight sense of aircraft flight simulator.
Description
Technical field
The invention belongs to aircraft emulator technical field, more particularly, to a kind of foot for flight simulator
Sharp brake weight induction device.
Background technology
On aircraft, with tiptoe brake sensor.Its effect is to control wheel braking and braking strength；But
The tiptoe brake of actual airplane is realized by hydraulic device, by the tiptoe brake sensor being attached to behind foot pedal, is come
Hydraulic system is controlled to carry out brake, while controls the size of brake weight.But on the flight simulator of the type aircraft, very
Real hydraulic system is not present, it is therefore desirable to which this manipulation of cyclic is emulated.
The content of the invention
In view of this, the invention be directed to a kind of easy brand-new framework for aircraft flight simulator
Tiptoe brake weight induction device,.
In order to achieve the above objectives, the technical solution of the invention is realized in：
A kind of tiptoe brake weight induction device for flight simulator, including sequentially connected push rod 1, piston 5, spring
11st, housing 6 and slide-wire rheostat 10, push rod 1 are arranged in the installation sky on 5 top of piston, and spring 11 is set in 5 lower part of piston
In protrusion, spring 11 is co-located on piston 5 in the inner cavity of housing 6, and piston 5 is fixed on by plug screw 7 on housing 6, is slided
Rheostat 10 is arranged on the lateral wall of housing 6, and slide-wire rheostat is equipped with the sliding bar 13 moved up and down, and 13 top of sliding bar leads to
Cross the fixation parallel with push rod of connection sheet 2.
Further, 6 inner cavity of housing includes accommodating the upper chambers of piston 5 and accommodates the lower chamber of spring 11, in upper chambers
Footpath is more than lower chamber, and platform is formed between upper chambers and lower chamber, drain plug gasket 9 is equipped between 7 bottom of plug screw and platform.
Further, connection sheet 2 is fixed on by connection sheet fixing nut 3 on push rod 1.
Further, sliding bar 13 is fixed on by slide-wire rheostat sliding bar fixing nut 4 in connection sheet 2.
Further, slide-wire rheostat 10 is fixed on by slide-wire rheostat fixed plate 12 on housing 6.
Further, the side wall between piston 5 and plug screw 7 is equipped with copper sheathing 8.
Compared with the prior art, a kind of tiptoe brake weight sense for aircraft flight simulator of the present invention fills
It puts and has the advantage that：
(1) the invention is simple in structure, of low cost, avoids the manipulation load control system using complex and expensive,
Simultaneously convenient for maintenance and adjustment.
(2) the invention simulated effect is good, can meet aircraft flight simulator tiptoe brake weight sense it is imitative
True requirement.
Description of the drawings
The attached drawing for forming the part of the invention is used for providing further understanding the invention, present invention wound
The schematic description and description made does not form the improper restriction to the invention for explaining the invention.
In attached drawing：
Fig. 1 is the structure diagram of the embodiment of the present invention；
Fig. 2 is installation site of the embodiment of the present invention in equipment.
Reference sign：
1- push rods；2- connection sheets；3- connection sheet fixing nuts；4- slide-wire rheostat sliding bar fixing nuts；5- pistons；
6- housings；7- plug screws；8- copper sheathings；9- drain plug gaskets；10- slide-wire rheostats；11- springs；12- slide-wire rheostat fixed plates；
13- sliding bars.
Specific embodiment
It should be noted that in the case where there is no conflict, the feature in embodiment and embodiment in the invention can
To be mutually combined.
In the description of the invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ",
The orientation or position relationship of the instructions such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of description the invention and simplifies description rather than instruction
Or imply that signified device or element must have specific orientation, with specific azimuth configuration and operation, therefore be not understood that
For the limitation to the invention.In addition, term " first ", " second " etc. are only used for description purpose, and it is not intended that instruction
Or imply relative importance or the implicit quantity for indicating indicated technical characteristic." first ", " second " etc. are defined as a result,
Feature can express or implicitly include one or more this feature.In the description of the invention, unless separately
It is described, " multiple " are meant that two or more.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in the description of the invention
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integrally
Connection；Can be mechanical connection or electrical connection；It can be directly connected, can also be indirectly connected by intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, on being understood by concrete condition
State concrete meaning of the term in the invention.
The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments creates.
A kind of tiptoe brake weight induction device for aircraft flight simulator, including the push rod being fixed on piston 5
1；Strong sense spring 11 is installed between piston 5 and housing 6；Piston 5 is fixed on by copper sheathing 8 on housing 6 by plug screw 7；Spiral shell
Drain plug gasket 9 is installed between plug 7 and housing 6, for adjustment plug screw height；Connection sheet 2 is connected piece fixing nut and is fixed on
On push rod；And the sliding bar of slide-wire rheostat 10 is then fixed on by slide-wire rheostat sliding bar fixing nut 4 in connection sheet, it is sliding
Line rheostat 10 is fixed on by slide-wire rheostat fixed plate 12 on housing 6.
The operation principle of the present invention：Using piston spring mechanism, installation one is adjustable on the housing of its piston exterior
Connecting rod, a slide-wire rheostat is driven by the connection sheet being fixed on connecting rod, to simulate brake, and according to slip
Voltage caused by rheostat change in resistance or curent change simulate the variation of brake strength size.The spring of piston lower portion plays
Brake pedal resets and provides the effect of brake weight sense.
When brake pedal promotes push rod 1, push rod 1 promotes piston 5 to act on downwards on spring 11, and spring 11 provides brake
Power sense；On the other hand, push rod 1 is then fixed on by using connection sheet fixing nut 3 on push rod 1 connection sheet 2 while promote logical
The slide-wire rheostat 10 that slide-wire rheostat fixed plate is fixed on housing 6 is crossed, at this point, 10 resistance value of slide-wire rheostat changes,
Voltage or electric current is caused to generate variation, voltage or the variable signal generation brake of electric current and the signal of brake weight size.Spring 11
Another effect be reset for brake pedal.
Copper sheathing 8 for ensure piston 5 during exercise will not clamping stagnation, drain plug gasket 9 is used for the position of adjustment plug screw 7, and protects
It is demonstrate,proved reliably to be fastened in housing 6.
The foregoing is merely the preferred embodiments of the invention, are not intended to limit the invention creation, all at this
Within the spirit and principle of innovation and creation, any modifications, equivalent replacements and improvements are made should be included in the invention
Protection domain within.
Claims (6)
1. a kind of tiptoe brake weight induction device for flight simulator, it is characterised in that：Including sequentially connected push rod (1),
Piston (5), spring (11), housing (6) and slide-wire rheostat (10), push rod (1) are arranged in the installation sky on piston (5) top,
Spring (11) is set in the protrusion of piston (5) lower part, and spring (11) is co-located on piston (5) in the inner cavity of housing (6),
Piston (5) is fixed on by plug screw (7) on housing (6), and slide rheostat (10) is arranged on the lateral wall of housing (6), and slip becomes
Resistance device is equipped with the sliding bar (13) moved up and down, and sliding bar (13) top passes through connection sheet (2) fixation parallel with push rod.
2. tiptoe brake weight induction device according to claim 1, it is characterised in that：Housing (6) inner cavity includes accommodating piston
(5) upper chambers and the lower chamber of receiving spring (11), upper chambers internal diameter are more than lower chamber, are formed between upper chambers and lower chamber
Platform, plug screw (7) are equipped with drain plug gasket (9) between bottom and platform.
3. tiptoe brake weight induction device according to claim 1, it is characterised in that：Connection sheet (2) is fixed by connection sheet
Nut (3) is fixed on push rod (1).
4. tiptoe brake weight induction device according to claim 1, it is characterised in that：The sliding bar (13) is become by slip
Resistance device sliding bar fixing nut (4) is fixed in connection sheet (2).
5. tiptoe brake weight induction device according to claim 1, it is characterised in that：The slide-wire rheostat (10) passes through cunning
Line rheostat fixed plate (12) is fixed on housing (6).
6. tiptoe brake weight induction device according to claim 1, it is characterised in that：Between the piston (5) and plug screw (7)
Side wall be equipped with copper sheathing (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711474083.8A CN108074433A (en) | 2017-12-29 | 2017-12-29 | A kind of tiptoe brake weight induction device for flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711474083.8A CN108074433A (en) | 2017-12-29 | 2017-12-29 | A kind of tiptoe brake weight induction device for flight simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108074433A true CN108074433A (en) | 2018-05-25 |
Family
ID=62156057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711474083.8A Pending CN108074433A (en) | 2017-12-29 | 2017-12-29 | A kind of tiptoe brake weight induction device for flight simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108074433A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2903660A1 (en) * | 2006-07-12 | 2008-01-18 | Airbus France Sas | Electrical flight control system for aircraft, has handle integrated to armrest of pilot seat and comprising brake lever, and hydraulic jack connected to linkage system and to another hydraulic jack and double effect oleo-pneumatic jack |
| CN201863825U (en) * | 2010-11-14 | 2011-06-15 | 江苏技术师范学院 | Buttoned type operating control device of automobile line control motor system |
| CN203766733U (en) * | 2014-01-28 | 2014-08-13 | 同济大学 | Pedal feeling simulator with combined type springs |
| CN105547668A (en) * | 2015-12-10 | 2016-05-04 | 中国飞机强度研究所 | Device for testing performances of aviation brake apparatus |
| CN205381106U (en) * | 2016-03-04 | 2016-07-13 | 瑞安市蓝星宇汽车科技有限公司 | Car tire pressure monitor |
| CN106969859A (en) * | 2017-05-05 | 2017-07-21 | 中国海洋大学 | The measuring method and device of arthropod foot of a chela strength |
| CN208805944U (en) * | 2017-12-29 | 2019-04-30 | 天津华翼蓝天科技股份有限公司 | A kind of tiptoe brake weight induction device for flight simulator |
-
2017
- 2017-12-29 CN CN201711474083.8A patent/CN108074433A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2903660A1 (en) * | 2006-07-12 | 2008-01-18 | Airbus France Sas | Electrical flight control system for aircraft, has handle integrated to armrest of pilot seat and comprising brake lever, and hydraulic jack connected to linkage system and to another hydraulic jack and double effect oleo-pneumatic jack |
| CN201863825U (en) * | 2010-11-14 | 2011-06-15 | 江苏技术师范学院 | Buttoned type operating control device of automobile line control motor system |
| CN203766733U (en) * | 2014-01-28 | 2014-08-13 | 同济大学 | Pedal feeling simulator with combined type springs |
| CN105547668A (en) * | 2015-12-10 | 2016-05-04 | 中国飞机强度研究所 | Device for testing performances of aviation brake apparatus |
| CN205381106U (en) * | 2016-03-04 | 2016-07-13 | 瑞安市蓝星宇汽车科技有限公司 | Car tire pressure monitor |
| CN106969859A (en) * | 2017-05-05 | 2017-07-21 | 中国海洋大学 | The measuring method and device of arthropod foot of a chela strength |
| CN208805944U (en) * | 2017-12-29 | 2019-04-30 | 天津华翼蓝天科技股份有限公司 | A kind of tiptoe brake weight induction device for flight simulator |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2374189B1 (en) | Electric energy distribution pole with incorporated ground system | |
| CN208805944U (en) | A kind of tiptoe brake weight induction device for flight simulator | |
| CN109187653B (en) | The Horizontal Layer Soil dynamic electric resistor characteristic test method of meter and different temperatures | |
| CN109188090B (en) | The nonlinear test method of different humidity electric resistance of soil in vertical demixing soil | |
| CN204536482U (en) | The horizontal Withstand test device of insulating bar | |
| RU2016112308A (en) | DEVICE AND METHOD FOR MANAGING THE STABILITY OF A LOCAL ELECTRIC NETWORK WITH AN ADJUSTABLE LOCAL ELECTRIC TRANSFORMER | |
| CN105116247B (en) | A kind of electrode system of complex media interface orthogonal electric field measurement | |
| CN108074433A (en) | A kind of tiptoe brake weight induction device for flight simulator | |
| CN104749406B (en) | Electric energy meter attachment structure | |
| CN209570660U (en) | A kind of environmental protection gas-insulated performance test apparatus | |
| CN202133729U (en) | Low pressure verification vehicle | |
| DE102016205179A1 (en) | Device for measuring the electrical energy of an alternating current | |
| CN202544207U (en) | Top equipment integrated space system | |
| CN203055654U (en) | Electronic type current-voltage combination mutual inductor | |
| CN207691341U (en) | A kind of high pressure detection mouth socket harness | |
| CN207779710U (en) | Road surface simulation device | |
| CN209675097U (en) | Voltage transformer is installed to the device and mutual induction of voltage device assembly of high pressure compartment | |
| CN105954631A (en) | Electronic island tester used for detecting grid-connected inverter | |
| CN207215271U (en) | One kind is weighed handle | |
| CN209169865U (en) | A kind of groove mounting | |
| CN206773129U (en) | A kind of Wire bundle testing apparatus | |
| CN205992695U (en) | A kind of integration console model cable distribution box | |
| CN104567983A (en) | Phytotron de-icing test platform for extra-high voltage divided conductors | |
| CN205810222U (en) | A kind of Multifunction electricity demonstration box | |
| CN203800446U (en) | Combined type insulated isolating device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |