CN110481763A - Brake machine wheel - Google Patents
Brake machine wheel Download PDFInfo
- Publication number
- CN110481763A CN110481763A CN201910899264.8A CN201910899264A CN110481763A CN 110481763 A CN110481763 A CN 110481763A CN 201910899264 A CN201910899264 A CN 201910899264A CN 110481763 A CN110481763 A CN 110481763A
- Authority
- CN
- China
- Prior art keywords
- brake
- machine wheel
- brake machine
- wheel
- cylinder part
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T5/00—Vehicle modifications to facilitate cooling of brakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
Abstract
The present invention describes a kind of brake machine wheel, it includes wheel hub and supporting structure, the supporting structure has center circle cylinder part and multiple blades, one end of each blade is attached to center circle cylinder part, and its other end radially is attached to the inner wall of wheel hub, wherein, supporting structure is in fan-shaped, and the central longitudinal axis of each blade and center circle cylinder part is tilted a certain angle setting.Brake machine wheel of the invention can be under the premise of not influencing aircraft weight, achieve the effect that actively to cool down to brake heat reservoir, to significantly shorten the cooling time of brake machine wheel, to realize fast cooling, and the normal operation for guaranteeing aircraft under the requirement for meeting turnaround on airport, is conducive to the economic benefit of aircraft.
Description
Technical field
The present invention relates to technical field of aerospace, more particularly to take off landing system, and more particularly, being related to one kind can
The brake machine wheel of autonomous air draught.
Background technique
In technical field of aerospace, wheel brake system is a part the most key during civil aircraft ground is slowed down, certainly
The landing safety of aircraft is determined.The wheel brake system generally includes two parts, and a part is brake machine wheel, another portion
Dividing is then brake control system.Wherein, brake machine wheel generally includes wheel assemblies and brake gear, the wheel brake system of aircraft
Be guarantee aircraft ground taxi, turning, normally landing, take off, landings that overload, suspension take off and ground stop and engine
Brake when test run.
For pilot when manipulating brake system, hydraulic oil enters the braking action cylinder being fixed on wheel shaft, pushes brake block,
Compress movable plate and stationary plate.Due to the rubbing action between rubbing surface, the torque for preventing wheel from rolling is increased, so wheel exists
The frictional ground force being subject in rolling significantly increases, and the running speed of aircraft reduces therewith.Driver's brake is heavier, into brake
Oil liquid pressure in pressurized strut is bigger, also just presses tighter between brake block, and the torque for preventing wheel from rolling is bigger, thus makees
It is also bigger with the frictional ground force on wheel.The kinetic energy that aircraft moves in the horizontal direction mainly passes through brake gear friction
The rubbing action in face is changed into what thermal energy dribbled.
In general, 90% or more kinetic energy is absorbed by brake machine wheel during aircraft landing, so that frictional heat generation leads to machine
Temperature is taken turns to increase.However, excessively high temperature will generate serious damage to the intensity and working performance of wheel and associated components, easily
Cause to brake it is on fire, blow out, or even cause catastrophic failure.
Most kinetic energy of aircraft are converted thermal energy by the stage stopped from aircraft brake to aircraft, friction working.
Frictional force mainly includes the friction etc. between phase mutual friction, tire and the ground braked between Moving plate and quiet disk.In contrast, brake disc
Between frictional force will be main, thus in brake machine wheel formed brake heat reservoir.In the operating of brake machine wheel, due to rubbing
Wiping the heat that power acting generates will lead to the raising of wheel part temperatures, since wheel internal chamber wall is contacted with air, the stream of air
Dynamic, the heat that brake machine wheel generates will be taken away by air.Only when time long enough, the temperature of brake machine wheel entirety just can be with
Air themperature is identical, can just make brake machine wheel revert to take off before state.
As described above, brake heat reservoir absorbs braking ability, and temperature can increase, and only work as during aircraft brake
In the case that brake heat reservoir is again cooled to suitable temperature, aircraft just can be carried out normal operation next time, thus make to stop as soon as possible
The cooling of vehicle heat reservoir is the material particular of a shortening aircraft turnaround on airport.
However, major part aircraft use at present is still natural cooling, it is well known that natural cooling generally requires to expend
For quite a long time.Some also can install cooling fan additional on individual types, for giving brake heat reservoir forced ventilation, to shorten
It brakes cooling time.But it installs brake fan additional and undoubtedly will increase the weight of aircraft, and also wanted on the operation panel of cockpit
A brake fan swicth is added, this is because brake fan swicth could be beaten only when main landing gear is grounded and is locked
It opens, and before aircraft standby for takeoff, and have to a brake fan swicth and close.In addition, due to having installed brake fan additional, because
And the software and hardware of brake control unit will be embedded in the operational order of brake fan, display information, warning information etc., and
It also needs to dismantle main gear wheels hub cap to be changed to brake fan, and needs to access power supply for brake fan so that it is transported
Turn.However, once brake fan breaks down, normally sending for aircraft will be caused to severely impact.It is more bad,
During aircraft cruising flight, which is at all inoperative, and can only occupy the efficient loading weight of aircraft,
To increase flight cost and seriously affect economic benefit.
Fig. 1 just shows the structural schematic diagram of such a existing brake machine wheel.As shown in Figure 1, showing machine in figure
Wheel assembly A.Wheel assemblies A includes brake machine wheel 1 and brake heat reservoir 2, wherein brake heat reservoir 2 is mounted in brake machine wheel 1.From
It will be clear that the support construction 3 of brake machine wheel 1 is the planar disc with a centre bore 4 in figure, have more
A vertically hung scroll portion 5, these vertically hung scroll portions 5 are in the same plane and outside radially from centre bore 4.
However, above-mentioned brake machine wheel has the following problems, that is, need to expend just can make brake machine wheel cold for quite a long time
But suitable temperature is arrived, aircraft can just be made to carry out normal operation next time, thus can greatly extend the turnaround on airport of aircraft,
Normally sending for aircraft is affected, to be unfavorable for the economic benefit of aircraft.
Therefore, become brake machine wheel rapid cooling without the weight of increase aircraft urgently to be resolved
The problem of.Based on this, such a demand there is in current technical field, that is, need such a brake machine wheel,
Can be under the premise of not increasing aircraft weight, the significant cooling time for shortening brake machine wheel, thus realize fast cooling, and
Meet and guarantees normally sending for aircraft under the requirement of turnaround on airport.
Summary of the invention
The present invention is precisely in order to solve above-mentioned technical problem and make, the purpose of the present invention is to provide a kind of brake machine wheel,
It can be under the premise of not increasing aircraft weight, the significant cooling time for shortening brake machine wheel, thus realize fast cooling, and
Guarantee normally sending for aircraft under the requirement for meeting turnaround on airport.
In order to achieve the above-mentioned object of the invention, the present invention provides a kind of brake machine wheel, the brake machine wheel includes:
Wheel hub；And
Supporting structure, the supporting structure have center circle cylinder part and multiple blades, and one end of each blade is attached
In the center circle cylinder part, and its other end radially is attached to the inner wall of the wheel hub,
Wherein, the supporting structure is in fan-shaped, the central longitudinal axis of each blade and the center circle cylinder part
It is tilted a certain angle setting.
Preferably, in brake machine wheel of the invention, described one end of each blade and the center circle cylinder part one shape
At.
Preferably, mode is matched by welding, welding or card in described one end of each blade in brake machine wheel of the invention
It is attached to the center circle cylinder part.
Preferably, the other end of each blade passes through welding, welding or card formula in brake machine wheel of the invention
Formula is attached to the inner wall of the wheel hub.
Preferably, in brake machine wheel of the invention, the center longitudinal axis of each blade and the center circle cylinder part
Line angulation is different.
Preferably, in brake machine wheel of the invention, the center longitudinal axis of each blade and the center circle cylinder part
Line angulation be it is identical, to generate more uniform and stable wind regime.
Preferably, in brake machine wheel of the invention, the center longitudinal axis of each blade and the center circle cylinder part
Line is at 30-60 ° of angle.
Preferably, in brake machine wheel of the invention, the center longitudinal axis of each blade and the center circle cylinder part
Line angle at 45 °.
Preferably, further including filter screen in brake machine wheel of the invention, aircraft is run when sucking air for preventing
The impurity such as branch, crushed stone on road are drawn into the brake machine wheel.
In view of above content, compared to existing brake machine wheel, brake machine wheel of the invention can not influence aircraft weight
Under the premise of amount, achieve the effect that actively to cool down to brake heat reservoir, to shorten the cooling time of brake machine wheel, significantly so as to reality
Show fast cooling, and guarantee the normal operation of aircraft under the requirement for meeting turnaround on airport, is conducive to the economic benefit of aircraft.
Detailed description of the invention
Fig. 1 shows a kind of structural schematic diagram of existing brake machine wheel component.
Fig. 2 shows the perspective views of the brake machine wheel of a preferred embodiment of the present invention.
Fig. 3 shows the front view of the brake machine wheel of the preferred embodiment of the invention.
List of the appended drawing reference in technical solution and embodiment in figure:
10. brake machine wheel
100. wheel hub
101. inner wall
200. supporting structure
201. center circle cylinder parts
202. blade
Specific embodiment
A specific embodiment of the invention explained below, it should be pointed out that in the specific descriptions of these embodiments
In the process, in order to carry out brief and concise description, this specification can not all features to actual embodiment make in detail
Most description.It is to be understood that during the actual implementation of any one embodiment, as in any one work
During journey project or design object, in order to realize the objectives of developer, in order to meet, system is relevant or quotient
The relevant limitation of industry can usually make various specific decisions, and this can also be implemented from a kind of embodiment to another kind
It changes between mode.Moreover, it is to be understood that although effort made in this development process may be complicated
And it is interminable, however for those skilled in the art relevant to present disclosure, in the disclosure
The changes such as some designs, manufacture or the production carried out on the basis of the technology contents of exposure are conventional technology, no
It should be understood as that content of this disclosure is insufficient.
Unless otherwise defined, technical term or scientific term used in claims and specification should be this hair
The ordinary meaning that personage in bright technical field with general technical ability is understood.The similar word such as "one" or " one " is simultaneously
It does not indicate that quantity limits, but indicates that there are at least one.The similar word such as " comprising " or "comprising" means to appear in " packet
Include " either the element before "comprising" or object cover the element or object for appearing in " comprising " or "comprising" presented hereinafter
Part and its equivalent element, it is not excluded that other elements or object.The similar word such as " connection " or " connected " is simultaneously non-limiting
In physics or mechanical connection, it is also not necessarily limited to direct or indirect connection.
Hereinafter, by brake machine wheel of the invention being specifically described in conjunction with attached drawing.
As shown in Figures 2 and 3, the perspective view and front view of brake machine wheel 10 are shown in figure.The brake machine wheel 10 includes wheel
Hub 100 and supporting structure 200.Wherein, which is generally in fan-shaped, by center circle cylinder part 201 and more
A blade 202 is constituted.One end of these blades 202 is attached to center circle cylinder part 201, and its other end then attaches radially
In the inner wall 101 of wheel hub 100.Herein it is noted that one end of these blades 202 can be with 201 1 bodily form of center circle cylinder part
At, or by welding, welding, card with etc. modes be attached to center circle cylinder part 201.Equally, the other end of blade 202
Can by welding, welding, card with etc. modes be attached to the inner wall 101 of wheel hub 100.
In particular, it will be clear that these blades 202 are not on same plane from Fig. 2 and 3, but as
Fan blade is tilted a certain angle setting with the central longitudinal axis of center circle cylinder part 201 like that.When brake machine wheel 10 rotates
When coming, these inclined blades 202 constantly can be drawn inwardly to air and form wind, to blow brake heat reservoir
Wind.And the heat reservoir that brakes is mounted on the inside of brake machine wheel 10, thus will receive brushing for generated wind, to reach fast quickly cooling
But effect.
Here, it is noted that the central longitudinal axis of blade 202 and center circle cylinder part 201 is at 30-60 ° of angle.Especially
It, when the central longitudinal axis of blade 202 and center circle cylinder part 201 angle at 45 °, the wind-force of formation is maximum.In addition, also referring to
One is mentioned that, these blades 202 can be identical with the central longitudinal axis angulation of center circle cylinder part 201, can also not
Together.Certainly, if if angle is identical, then more uniform and stable wind regime can preferably be generated.
In addition, in the biggish situation in gap between blade 202, it may be necessary in the supporting structure of brake machine wheel 10
200 outside installs a filter screen (not shown) additional, when for preventing brake machine wheel 10 from sucking air because of rotation, it is not intended to middle to incite somebody to action
The impurity such as branch, crushed stone on runway are drawn into brake machine wheel 10, and cause the structure or brake heat of brake machine wheel
The damage in library, therefore the filter screen can play certain protective action.
To sum up, core of the invention technology is: it is fan-shaped by the support structure designs of brake machine wheel, so as to
Form a kind of brake machine wheel that can independently suck outside air.When aircraft brake, with the rotation of airplane wheel, this shape
The brake machine wheel of shape will independently suck air, and the air is blown to brake heat reservoir up, and thus, it is possible to not influence aircraft
Under the premise of weight, achieve the effect that actively to cool down to brake heat reservoir, thus significantly shorten the cooling time of brake machine wheel, so as to
It realizes fast cooling, and guarantees the normal operation of aircraft under the requirement for meeting turnaround on airport, be conducive to the economic effect of aircraft
Benefit.
In conclusion in terms of wider range of, the invention is not limited to shown and described herein specific
Details and representative embodiment.Therefore, those skilled in the art can reasonably be combined the element of above embodiment
Or change, not depart from the essence such as the total concept of the invention of the present invention defined by the appended claims and its equivalent
Various modification can be adapted under the premise of mind or range.
Claims (9)
1. a kind of brake machine wheel, the brake machine wheel include:
Wheel hub；And
Supporting structure, the supporting structure have center circle cylinder part and multiple blades, and one end of each blade is attached to institute
Center circle cylinder part is stated, and its other end radially is attached to the inner wall of the wheel hub,
It is characterized in that, the supporting structure is in fan-shaped, wherein the center of each blade and the center circle cylinder part is vertical
Setting is tilted a certain angle to axis.
2. brake machine wheel as described in claim 1, which is characterized in that described one end of each blade and the center circle cylinder part
It is integrally formed.
3. brake machine wheel as described in claim 1, which is characterized in that described one end of each blade by welding, welding or
Card is attached to the center circle cylinder part with mode.
4. brake machine wheel as described in claim 1, which is characterized in that the other end of each blade passes through welding, welding
Or card is attached to the inner wall of the wheel hub with mode.
5. brake machine wheel as described in claim 1, which is characterized in that the center of each blade and the center circle cylinder part
Longitudinal axis angulation is different.
6. brake machine wheel as described in claim 1, which is characterized in that the center of each blade and the center circle cylinder part
Longitudinal axis angulation be it is identical, to generate more uniform and stable wind regime.
7. brake machine wheel as claimed in claim 6, which is characterized in that the center of each blade and the center circle cylinder part
Longitudinal axis is at 30-60 ° of angle.
8. brake machine wheel as claimed in claim 7, which is characterized in that the center of each blade and the center circle cylinder part
Longitudinal axis angle at 45 °.
9. brake machine wheel as described in claim 1, which is characterized in that further include filter screen, for preventing when sucking air
The impurity such as branch, crushed stone on runway are drawn into the brake machine wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910899264.8A CN110481763A (en) | 2019-09-23 | 2019-09-23 | Brake machine wheel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910899264.8A CN110481763A (en) | 2019-09-23 | 2019-09-23 | Brake machine wheel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110481763A true CN110481763A (en) | 2019-11-22 |
Family
ID=68559066
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910899264.8A Pending CN110481763A (en) | 2019-09-23 | 2019-09-23 | Brake machine wheel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110481763A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111907697A (en) * | 2020-08-17 | 2020-11-10 | 中国商用飞机有限责任公司 | Brake cooling fan device |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1669951A (en) * | 1926-01-07 | 1928-05-15 | Stitt Refrigeration Company | Flywheel and fan construction |
| US1730490A (en) * | 1926-08-05 | 1929-10-08 | Steel Wheel Corp | Air-cooled-wheel construction |
| US2432385A (en) * | 1946-03-09 | 1947-12-09 | Deere & Co | Wheel with axially adjustable rim |
| GB654499A (en) * | 1948-09-28 | 1951-06-20 | Dunlop Rubber Co | Improvements in cooling systems for vehicle wheel brakes |
| US2762469A (en) * | 1953-09-25 | 1956-09-11 | Lyon George Albert | Wheel cover |
| DE2109563A1 (en) * | 1971-03-01 | 1972-09-14 | Waisen, Jürgen, Dipl.-Ing., 4100 Duisburg | Drive for an aircraft landing gear wheel |
| US4135764A (en) * | 1977-01-24 | 1979-01-23 | Johnson R W | Wheel assembly with air cooling means |
| AU2006337903A1 (en) * | 2006-02-07 | 2007-08-16 | William Edward Fenna | Braking systems with cooling |
| US20090152055A1 (en) * | 2007-12-18 | 2009-06-18 | Isaiah Watas Cox | Wheel motor cooling |
| US20120175203A1 (en) * | 2011-01-07 | 2012-07-12 | Jerry Robertson | Brake Cooling Fan and Method of Use |
| US9114874B1 (en) * | 2012-02-29 | 2015-08-25 | Peter Danto | Aircraft hubcap structure |
| CN109305338A (en) * | 2018-09-30 | 2019-02-05 | 西安航空制动科技有限公司 | A kind of wind-collecting cover component for Inspection Aircraft Wheels cooling system |
| CN110171561A (en) * | 2019-06-24 | 2019-08-27 | 焦佳敏 | A kind of unmanned plane pushing stable landing based on reversed air pressure |
-
2019
- 2019-09-23 CN CN201910899264.8A patent/CN110481763A/en active Pending
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1669951A (en) * | 1926-01-07 | 1928-05-15 | Stitt Refrigeration Company | Flywheel and fan construction |
| US1730490A (en) * | 1926-08-05 | 1929-10-08 | Steel Wheel Corp | Air-cooled-wheel construction |
| US2432385A (en) * | 1946-03-09 | 1947-12-09 | Deere & Co | Wheel with axially adjustable rim |
| GB654499A (en) * | 1948-09-28 | 1951-06-20 | Dunlop Rubber Co | Improvements in cooling systems for vehicle wheel brakes |
| US2762469A (en) * | 1953-09-25 | 1956-09-11 | Lyon George Albert | Wheel cover |
| DE2109563A1 (en) * | 1971-03-01 | 1972-09-14 | Waisen, Jürgen, Dipl.-Ing., 4100 Duisburg | Drive for an aircraft landing gear wheel |
| US4135764A (en) * | 1977-01-24 | 1979-01-23 | Johnson R W | Wheel assembly with air cooling means |
| AU2006337903A1 (en) * | 2006-02-07 | 2007-08-16 | William Edward Fenna | Braking systems with cooling |
| US20090152055A1 (en) * | 2007-12-18 | 2009-06-18 | Isaiah Watas Cox | Wheel motor cooling |
| US20120175203A1 (en) * | 2011-01-07 | 2012-07-12 | Jerry Robertson | Brake Cooling Fan and Method of Use |
| US9114874B1 (en) * | 2012-02-29 | 2015-08-25 | Peter Danto | Aircraft hubcap structure |
| CN109305338A (en) * | 2018-09-30 | 2019-02-05 | 西安航空制动科技有限公司 | A kind of wind-collecting cover component for Inspection Aircraft Wheels cooling system |
| CN110171561A (en) * | 2019-06-24 | 2019-08-27 | 焦佳敏 | A kind of unmanned plane pushing stable landing based on reversed air pressure |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111907697A (en) * | 2020-08-17 | 2020-11-10 | 中国商用飞机有限责任公司 | Brake cooling fan device |
| WO2022036985A1 (en) * | 2020-08-17 | 2022-02-24 | 中国商用飞机有限责任公司 | Brake cooling fan device |
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