TWI463125B - Membrane Rigidity Testing Platform for Air Floating Plane Bearing and Its Application - Google Patents

Membrane Rigidity Testing Platform for Air Floating Plane Bearing and Its Application Download PDF

Info

Publication number
TWI463125B
TWI463125B TW100148385A TW100148385A TWI463125B TW I463125 B TWI463125 B TW I463125B TW 100148385 A TW100148385 A TW 100148385A TW 100148385 A TW100148385 A TW 100148385A TW I463125 B TWI463125 B TW I463125B
Authority
TW
Taiwan
Prior art keywords
air
platform
pneumatic cylinder
air floating
gas
Prior art date
Application number
TW100148385A
Other languages
Chinese (zh)
Other versions
TW201326779A (en
Original Assignee
Stone & Resource Ind R & D Ct
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 Stone & Resource Ind R & D Ct filed Critical Stone & Resource Ind R & D Ct
Priority to TW100148385A priority Critical patent/TWI463125B/en
Publication of TW201326779A publication Critical patent/TW201326779A/en
Application granted granted Critical
Publication of TWI463125B publication Critical patent/TWI463125B/en

Links

Landscapes

  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Description

氣浮式平面軸承之氣膜剛性檢測平台及其使用方法Air film rigidity detecting platform for air floating plane bearing and using method thereof

本發明是有關於一種氣膜剛性檢測平台,特別是指一種氣浮式平面軸承之氣膜剛性檢測平台及其使用方法。The invention relates to a gas film rigidity detecting platform, in particular to a gas film rigid detecting platform of an air floating plane bearing and a using method thereof.

參閱圖1,以往的一種氣膜剛性檢測平台1,包括一平台11、一置於該平台11上的氣浮載具12、一連接該氣浮載具12的供氣系統13、一架設於該平台11且位於該氣浮載具12上方的千分錶14,及一架設於該平台11且位於該氣浮載具12上方的機械式感測器15,該機械式感測器15可以是荷重感測器。Referring to FIG. 1 , a conventional air film rigidity detecting platform 1 includes a platform 11 , an air floating carrier 12 disposed on the platform 11 , a gas supply system 13 connected to the air floating carrier 12 , and a racking device The platform 11 is located on the dial gauge 14 above the air floating carrier 12, and a mechanical sensor 15 disposed on the platform 11 and above the air floating carrier 12, the mechanical sensor 15 can It is a load sensor.

此處以該氣浮載具12向下噴氣做為說明,也就是該氣浮載具12為待測物,進行檢測時,先將該千分錶14輕觸於該氣浮載具12表面做歸零動作,接著,開啟該供氣系統13使該氣浮載具12浮起,讀取該千分錶14的數據,得到該氣浮載具12的氣膜厚度,而後,啟動該荷重試驗機,使感測頭將逐漸下降至接觸到該氣浮載具12,直至該氣浮載具12底部完全接觸試平台11,所測得的荷重值為承載力,透過下式計算後得氣膜剛性:Here, the air-floating carrier 12 is described as a downward jet, that is, the air-floating carrier 12 is an object to be tested, and when the detection is performed, the dial gauge 14 is first touched on the surface of the air-floating carrier 12 Returning to zero, then opening the air supply system 13 to float the air bearing carrier 12, reading the data of the dial gauge 14, obtaining the film thickness of the air bearing carrier 12, and then starting the load test Therefore, the sensing head will gradually descend to contact the air bearing carrier 12 until the bottom of the air floating carrier 12 completely contacts the test platform 11, and the measured load value is the bearing capacity, and the gas is calculated by the following formula. Film rigidity:

J =W /H J = W / H ,

J為氣膜剛性(單位:N/μm),W為承載力,H為氣膜厚度。J is the film rigidity (unit: N/μm), W is the bearing capacity, and H is the film thickness.

以往的氣膜剛性檢測平台1所使用的機械式感測器15,其啟動後機械式感測器15將開始下降,當機械式感測器15接觸到氣浮載具12表面的同時,機械式感測器15開始對氣浮載具12施加負載,當氣浮載具12受到機械式感測器15所施加的負載,氣浮載具12之氣膜同時會回饋一反作用力予機械式感測器15,此反作用力即為氣膜承載力;當機械式感測器15負載大於氣膜承載力時,感測器15測頭將持續下降,而氣浮載具12之氣膜厚度將逐漸減少;反之當機械式感測器15負載小於氣膜承載力時,機械式感測器15測頭將會上升,而氣浮載具12之氣膜厚度將逐漸增加;而當氣膜承載力等於感測器15負載時,則兩者將保持平衡且靜止不動。In the mechanical sensor 15 used in the conventional air film rigidity detecting platform 1, after the startup, the mechanical sensor 15 will start to descend, and when the mechanical sensor 15 contacts the surface of the air floating carrier 12, the machine The sensor 15 begins to apply a load to the air bearing carrier 12, and when the air bearing carrier 12 is subjected to the load applied by the mechanical sensor 15, the air film of the air bearing carrier 12 simultaneously feeds back a reaction force to the mechanical type. The sensor 15, the reaction force is the gas film bearing capacity; when the mechanical sensor 15 load is greater than the gas film bearing capacity, the sensor 15 probe will continue to decrease, and the air film thickness of the air bearing carrier 12 It will gradually decrease; otherwise, when the load of the mechanical sensor 15 is less than the bearing capacity of the film, the probe of the mechanical sensor 15 will rise, and the film thickness of the air bearing carrier 12 will gradually increase; When the bearing capacity is equal to the load of the sensor 15, the two will remain balanced and stationary.

由於機械式感測器15則為機械式,出力範圍與規格為固定,而無法依待測物性能調整出力範圍,且僅可量測氣膜剛性的最大值。以往在量測氣膜剛性時,機械式感測器15之測頭從伸出至接觸氣浮載具12,最後使氣浮載具12底面完全接觸設備平台11之台面後,機械式感測器15之測頭才完全停止,並開始計算在這施壓過程中感測器15施予氣浮載具12之最大負載值是多少,故以往的檢測方式僅能量測氣浮載具12之氣膜剛性最大值,且由於機械式感測器15是在被測物完全接觸設備平台11之台面時,才開始計算負載值,故以往的量測結果往往高估了氣浮載具12本身之氣膜剛性,其結果是有誤差的。Since the mechanical sensor 15 is mechanical, the output range and the specification are fixed, and the output range cannot be adjusted according to the performance of the object to be tested, and only the maximum value of the film rigidity can be measured. In the past, when the film stiffness was measured, the probe of the mechanical sensor 15 extended from the contact to the air bearing carrier 12, and finally the bottom surface of the air floating carrier 12 completely contacted the table top of the equipment platform 11, mechanical sensing The probe of the device 15 is completely stopped, and it is calculated to calculate the maximum load value of the air-floating carrier 12 that the sensor 15 applies during the pressing process. Therefore, the conventional detection method only measures the air-floating carrier 12 The film has a maximum rigidity, and since the mechanical sensor 15 starts to calculate the load value when the object is completely in contact with the table top of the equipment platform 11, the conventional measurement results tend to overestimate the air bearing carrier 12 The film's own rigidity is rigid and the result is inaccurate.

以往氣膜厚度的大小受到供氣系統13的設定參數所影響,當設定參數調升到某個數值時,氣膜厚度受到被測物規格之限制而將不會再增加,此時氣膜厚度值即為初始氣膜厚度值,初始氣膜厚度值是當被測物尚未承受任何負載的情況下,所達到的氣膜厚度值,故初始氣膜厚度可視為最大氣膜厚度;而當被測物受到負載作用導致氣膜厚度逐漸減少時,當氣膜厚度趨近於零時但不等於零,此氣膜厚度值即為氣膜厚度最小值。In the past, the thickness of the film was affected by the setting parameters of the gas supply system 13. When the set parameter was raised to a certain value, the film thickness was limited by the specification of the sample to be measured, and the film thickness was not increased. The value is the initial film thickness value, and the initial film thickness value is the film thickness value achieved when the measured object has not been subjected to any load, so the initial film thickness can be regarded as the maximum film thickness; When the thickness of the film is gradually reduced by the load, when the film thickness approaches zero but not equal to zero, the film thickness value is the minimum film thickness.

當氣浮載具12受到負載作用導致氣膜厚度逐漸下降的同時,氣膜厚度愈小相對地導致氣膜密度愈大,氣膜密度愈大將造成氣膜承載力愈大;故最大氣膜承載力為最小氣膜厚度所能承受之最大負載值,即為最大氣膜承載力;而最小氣膜承載力則為初始氣膜厚度所能承受之最大負載值,即為最小氣膜負載力。When the air-floating carrier 12 is subjected to load, the thickness of the film gradually decreases. The smaller the film thickness is, the larger the film density is. The larger the film density is, the larger the gas film bearing capacity is. The bearing capacity is the maximum load value that the minimum film thickness can withstand, that is, the maximum film carrying capacity; and the minimum film carrying capacity is the maximum load value that the initial film thickness can withstand, that is, the minimum film loading force. .

值得強調的是,以往的氣浮載具12的供氣系統13與機械式感測器15之能源型態為兩套不同的系統,氣浮載具12固定僅能以氣壓系統的供氣系統13為供應型態,而機械式感測器15可以為機械能轉動能,或電能轉動能...等各種供應形態,故以往僅能針對氣浮載具12之供氣系統13進行調整,而供氣系統13的設定將影響氣浮載具12之負載能力大小;以往的機械式感測器15之規格設計是固定的,當氣浮載具12之負載能力超出量測設備之容許範圍,將會產生機械式感測器15無法測得氣浮載具12之最大負載能力。It is worth emphasizing that the energy type of the gas supply system 13 and the mechanical sensor 15 of the conventional air bearing vehicle 12 are two different systems, and the air floating carrier 12 is fixed only to the air supply system of the air pressure system. 13 is a supply type, and the mechanical sensor 15 can be a variety of supply modes such as mechanical energy rotation energy, or electric energy rotation energy, etc., so in the past, only the air supply system 13 of the air floating carrier 12 can be adjusted. The setting of the air supply system 13 will affect the load capacity of the air floating carrier 12; the conventional mechanical sensor 15 is designed to be fixed, and when the load capacity of the air floating carrier 12 exceeds the allowable range of the measuring device The mechanical sensor 15 will not be able to measure the maximum load capacity of the air bearing carrier 12.

因此,一種可以快速量測的氣膜剛性檢測平台1,為目前相關業者的研發目標之一。Therefore, a gas film rigidity detecting platform 1 that can be quickly measured is one of the research and development targets of current related companies.

因此,本發明之目的,即在提供一種可以快速量測的氣浮式平面軸承之氣膜剛性檢測平台及其使用方法。Accordingly, it is an object of the present invention to provide a gas film rigidity detecting platform for a gas floating planar bearing that can be quickly measured and a method of using the same.

於是,本發明氣浮式平面軸承之氣膜剛性檢測平台包含一精密比測平台單元、一氣浮載具,及一供氣系統,該精密比測平台單元包括一用於提供平坦表面的精密平台、一設置於該精密平台上方的氣壓缸,及一設置於該精密平台上方且連接於該氣壓缸的千分錶,該氣浮載具放置於該精密平台上,該供氣系統連接該氣浮載具與該精密比測平台單元的氣壓缸。Therefore, the gas film rigidity detecting platform of the air floating plane bearing of the present invention comprises a precision ratio measuring platform unit, an air floating carrier, and a gas supply system, and the precision comparison platform unit comprises a precision platform for providing a flat surface. a pneumatic cylinder disposed above the precision platform, and a dial gauge disposed above the precision platform and connected to the pneumatic cylinder, the air float carrier is placed on the precision platform, and the gas supply system is connected to the gas The floating carrier and the pneumatic cylinder of the precision comparison platform unit.

本發明氣浮式平面軸承之氣膜剛性檢測平台的使用方法,包含以下步驟:首先,準備一如前所述之氣浮式平面軸承之氣膜剛性檢測平台,接著,將該千分錶抵於待測物表面,進行該千分錶歸零,而後,啟動該供氣系統使待測物浮起,讀取該千分錶數值,得知氣膜厚度,接續地,啟動該氣壓缸以向下施壓力於待測物,向下施壓力至待測物不浮起,讀取該氣壓缸數值,得知氣膜的承載力。The method for using the gas film rigidity detecting platform of the air floating plane bearing of the present invention comprises the following steps: First, preparing a gas film rigidity detecting platform of an air floating plane bearing as described above, and then, the dial gauge is offset On the surface of the object to be tested, the dial gauge is reset to zero, and then the gas supply system is activated to float the object to be tested, the dial gauge value is read, the film thickness is known, and the pneumatic cylinder is activated. Apply pressure to the object to be tested downward, apply pressure downward until the object to be tested does not float, and read the value of the cylinder to know the bearing capacity of the film.

本發明之功效在於,透過使用氣壓缸,統一由供氣系統供應待測物浮起與檢測承載力,並且可依待測物的性能調整氣壓缸所施加的負載大小,也可迅速更換合適規格的氣壓缸,而透過設定氣壓缸的氣壓系統參數,量測出待測物在不同的供氣條件與承受不同負載能力的情況下氣膜剛性的數值,達到快速量測的目的。The effect of the invention is that, by using the pneumatic cylinder, the air supply system is uniformly supplied with the lifting and detecting bearing capacity of the object to be tested, and the load applied by the pneumatic cylinder can be adjusted according to the performance of the object to be tested, and the appropriate specification can be quickly replaced. The pneumatic cylinder, by setting the air pressure system parameters of the pneumatic cylinder, measures the value of the air film rigidity of the object under different gas supply conditions and with different load capacity, and achieves the purpose of rapid measurement.

有關本發明之前述及其他技術內容、特點與功效,在以下配合參考圖式之數個較佳實施例的詳細說明中,將可清楚的呈現。The above and other technical features, features, and advantages of the present invention will be apparent from the following detailed description of the preferred embodiments.

在本發明被詳細描述之前,要注意的是,在以下的說明內容中,類似的元件是以相同的編號來表示。Before the present invention is described in detail, it is noted that in the following description, similar elements are denoted by the same reference numerals.

參閱圖2與圖3,本發明氣浮式平面軸承之氣膜剛性檢測平台及其使用方法之第一較佳實施例包含一精密比測平台單元2、一氣浮載具3,及一供氣系統4。Referring to FIG. 2 and FIG. 3, a first preferred embodiment of the gas film rigidity detecting platform of the air floating plane bearing of the present invention and a method for using the same comprises a precision ratio measuring platform unit 2, an air floating carrier 3, and a gas supply. System 4.

該精密比測平台單元2包括一用於提供平坦表面的精密平台21、一連接設置於該精密平台21上方的氣壓缸22,及一連接設置於該精密平台21上方且連接於該氣壓缸22的千分錶23,該千分錶23與該氣壓缸22安裝同一水平面上,且可以同時調整該千分錶23與氣壓缸22相對該精密平台21的高度。The precision comparison platform unit 2 includes a precision platform 21 for providing a flat surface, a pneumatic cylinder 22 connected to the precision platform 21, and a connection above the precision platform 21 and connected to the pneumatic cylinder 22 The dial gauge 23 is mounted on the same horizontal surface as the pneumatic cylinder 22, and the height of the dial gauge 23 and the pneumatic cylinder 22 relative to the precision platform 21 can be simultaneously adjusted.

該精密平台21的材質可以是天然花崗岩、人造石、鑄鐵、鋁蜂巢等等。The precision platform 21 may be made of natural granite, artificial stone, cast iron, aluminum honeycomb, and the like.

該氣浮載具3放置於該精密平台21上,在本第一較佳實施例中,該氣浮載具3即為待測物A,該氣浮載具3向下朝該精密平台21噴氣,當該氣浮載具3浮起之後,可將欲運送的物品放置於該氣浮載具3上,藉此省力搬運,一般適用於運送負載較大的物品,本第一較佳實施例屬於重負載型氣壓系統。The air bearing carrier 3 is placed on the precision platform 21. In the first preferred embodiment, the air bearing carrier 3 is the object A to be tested, and the air bearing carrier 3 faces downward toward the precision platform 21 After the air-floating carrier 3 is floated, the article to be transported can be placed on the air-floating carrier 3, thereby saving labor, and generally suitable for transporting articles with large loads, the first preferred embodiment The example belongs to a heavy-load type pneumatic system.

該供氣系統4連接該氣浮載具3與該精密比測平台單元2的氣壓缸22,該供氣系統4包括一用於提供氣源的空氣壓縮機41、一連接該空氣壓縮機41的調壓閥42,及複數個分別連接於該氣浮載具3、氣壓缸22與調壓閥42間的流量控制閥43,該調壓閥42用於調整空氣壓力,該等流量控制閥43用於調整氣浮載具3、氣壓缸22所施加的負載大小。The air supply system 4 is connected to the air-floating carrier 3 and the pneumatic cylinder 22 of the precision comparison platform unit 2. The air supply system 4 includes an air compressor 41 for supplying a gas source, and a connection with the air compressor 41. The pressure regulating valve 42 and a plurality of flow control valves 43 respectively connected between the air floating carrier 3, the pneumatic cylinder 22 and the pressure regulating valve 42 for adjusting the air pressure, the flow control valves 43 is used to adjust the load applied by the air bearing carrier 3 and the pneumatic cylinder 22.

更進一步說明的是,該供氣系統4還包括一設置於該空氣壓縮機41與調壓閥42之間的冷凍乾燥機44、一設置於該冷凍乾燥機44與調壓閥42之間的儲氣桶45、一設置於該調壓閥42與該流量控制閥43間的精密過濾器46,及一設置於該精密過濾器46與該流量控制閥43間的方向控制閥47,該冷凍乾燥機44用於降低空氣濕度,該儲氣桶45用於穩定空氣壓力,該精密過濾器46用於過濾空氣雜質,該方向控制閥47用於控制氣壓缸22伸出或縮回出力方向,本第一較佳實施例該方向控制閥47使用曲柄式五口三位方向控制閥,以手動曲柄控制方式,切換該等流量控制閥43,藉此變換管路內氣體流動之方向或使其靜止,來驅動氣壓缸22執行伸出或縮回之動作。It is further illustrated that the air supply system 4 further includes a freeze dryer 44 disposed between the air compressor 41 and the pressure regulating valve 42 , and a refrigeration dryer 44 disposed between the freeze dryer 44 and the pressure regulating valve 42 . a gas storage tank 45, a precision filter 46 disposed between the pressure regulating valve 42 and the flow control valve 43, and a directional control valve 47 disposed between the precision filter 46 and the flow control valve 43, the freezing The dryer 44 is for reducing the air humidity, the air tank 45 is for stabilizing the air pressure, the precision filter 46 is for filtering the air impurities, and the directional control valve 47 is for controlling the air cylinder 22 to extend or retract the output direction. In the first preferred embodiment, the directional control valve 47 uses a crank-type five-position three-position directional control valve to switch the flow control valves 43 in a manual crank control manner, thereby changing the direction of gas flow in the pipeline or making it It is stationary to drive the pneumatic cylinder 22 to perform an action of extending or retracting.

依據待測物A的幾何外形與實際測試情況等不同的條件,可以更換該千分錶23、氣壓缸22、調壓閥42、流量控制閥43等元件,當待測物A之氣膜厚度較微小時,就必須更換高精度千分錶23、低負載氣壓缸22、高精度之調壓閥42與流量控制閥43,方可準確測得較準確之氣膜剛性;當待測物A之負載能力過大時,則必須更換高負載之氣壓缸22、調壓閥42與流量控制閥43,提高最大負載範圍,方可測得待測物A之負載能力。According to different conditions such as the geometric shape of the object A to be tested and the actual test conditions, the components such as the dial gauge 23, the pneumatic cylinder 22, the pressure regulating valve 42, and the flow control valve 43 can be replaced, and the film thickness of the object A to be tested is changed. In a relatively small hour, it is necessary to replace the high-precision dial gauge 23, the low-load pneumatic cylinder 22, the high-precision pressure regulating valve 42 and the flow control valve 43 in order to accurately measure the more accurate film rigidity; When the load capacity is too large, the high-load pneumatic cylinder 22, the pressure regulating valve 42 and the flow control valve 43 must be replaced to increase the maximum load range, and the load capacity of the object A can be measured.

本第一較佳實施例中,氣浮式平面軸承之氣膜剛性檢測平台21的使用方法,包含以下步驟:In the first preferred embodiment, the method for using the air film rigidity detecting platform 21 of the air floating type planar bearing comprises the following steps:

步驟100,首先,準備本發明之氣浮式平面軸承之氣膜剛性檢測平台21,並依待測物A的量測條件,調整該供氣系統4,也就是依待測物A之幾何形狀與氣流模式,初步判斷待測物A是否適合重負載型氣壓系統;在操作時,主要在於調整供氣系統4之調壓閥42與流量控制閥43,來達到氣壓與流量之大小控制,而量測模式為氣壓、流量皆由小到大。Step 100, first, preparing the gas film rigidity detecting platform 21 of the air floating type planar bearing of the present invention, and adjusting the gas supply system 4 according to the measurement condition of the object A to be tested, that is, according to the geometry of the object A to be tested And the airflow mode, initially determining whether the object A is suitable for the heavy-load type air pressure system; in operation, mainly adjusting the pressure regulating valve 42 and the flow control valve 43 of the air supply system 4 to achieve the control of the air pressure and the flow rate, and The measurement mode is air pressure and flow rate from small to large.

步驟200,接著,將該千分錶23輕觸並抵於待測物A表面,進行該千分錶23歸零的動作。Step 200, next, the dial gauge 23 is touched and pressed against the surface of the object A to be subjected to the zeroing operation of the dial gauge 23.

步驟300,啟動該供氣系統4,並開啟位於該調壓閥42與該氣浮載具3間的流量控制閥43,使待測物A浮起,讀取該千分錶23數值,待千分錶23所量測的數值趨於穩定後,得知氣膜厚度。Step 300, the gas supply system 4 is activated, and the flow control valve 43 between the pressure regulating valve 42 and the air floating carrier 3 is opened, the object A is floated, and the value of the dial gauge 23 is read. After the value measured by the dial gauge 23 tends to be stable, the film thickness is known.

步驟400,開啟位於該調壓閥42與該氣壓缸22間的流量控制閥43,啟動該氣壓缸22以向下施壓力於待測物A,向下施壓力至待測物A不浮起,讀取該氣壓缸22數值,得知氣膜的承載力。Step 400, the flow control valve 43 between the pressure regulating valve 42 and the pneumatic cylinder 22 is opened, the pneumatic cylinder 22 is activated to apply pressure to the object A to be pressed downward, and the pressure is applied downward until the object A does not float. The value of the pneumatic cylinder 22 is read to know the bearing capacity of the gas film.

更進一步說明的是,該步驟400中,該氣壓缸22探的測頭伸出至接觸待測物A上方表面,並開始對待測物A施加負載,使待測物A的氣膜厚度開始下降,下降至待測物A底面與精密平台21頂面完全貼合時,此時該千分錶23數值為零,而後開始調整該氣壓缸22所施加的負載大小,調整至該千分錶23數值即將開始產生變化但數值仍為零時,該氣壓缸22所施加的負載大小,即為待測物A氣膜之承載力。Further, in the step 400, the probe probed by the pneumatic cylinder 22 protrudes to contact the upper surface of the object A, and starts to apply a load to the object A, so that the film thickness of the object A starts to decrease. When the bottom surface of the object A is completely attached to the top surface of the precision platform 21, the value of the dial gauge 23 is zero at this time, and then the load applied by the pneumatic cylinder 22 is adjusted to be adjusted to the dial gauge 23 When the value is about to start to change but the value is still zero, the load applied by the pneumatic cylinder 22 is the bearing capacity of the air film of the object A to be tested.

透過下式計算後得氣膜剛性:The film stiffness is calculated by the following formula:

J =W /H J = W / H ,

J為氣膜剛性(單位:N/μm),W為承載力,H為氣膜厚度。J is the film rigidity (unit: N/μm), W is the bearing capacity, and H is the film thickness.

參閱圖4,本發明氣浮式平面軸承之氣膜剛性檢測平台21的第二較佳實施例與該第一較佳實施例構件與組裝方式大致相同,不同處在於該第二較佳實施例中,放置待測物A於該氣浮載具3上,該氣浮載具3向上噴氣使該待測物A浮起,也就是將大面積的板材,例如玻璃基板、電路板、液晶面版等置於該氣浮載具3上方時,該氣浮載具3與待測物A間會形成一層氣膜,使待測物A能夠浮起,藉此達到非接觸輸送的效果,一般是用於面積大且重量較輕的物品,本第二較佳實施例屬於輕負載型氣壓系統。Referring to FIG. 4, the second preferred embodiment of the gas film rigidity detecting platform 21 of the air floating type planar bearing of the present invention is substantially the same as the first preferred embodiment member and the assembling method, and the difference lies in the second preferred embodiment. The object A is placed on the air bearing carrier 3, and the air bearing carrier 3 is ejected upward to float the object A, that is, a large-area board, such as a glass substrate, a circuit board, or a liquid crystal surface. When the plate or the like is placed above the air-floating carrier 3, a gas film is formed between the air-floating carrier 3 and the object A to be tested, so that the object A can be floated, thereby achieving the effect of non-contact transportation. It is used for items with large area and light weight, and the second preferred embodiment belongs to a light load type pneumatic system.

綜上所述,本發明的優點在於:In summary, the advantages of the present invention are:

一、本發明將以往機械式感測器,改以該氣壓缸22的形式來給予待測物A負載,將施力系統與該氣浮載具3整合為一,統一由該供氣系統4供應待測物A浮起,以及供應該氣壓缸22具備負載能力,保留了可對待測物A進行供氣條件與負載能力的調整特性,還衍生出藉由供氣系統4調整氣壓缸22的負載能力,而透過氣壓系統4的調壓閥42與流量控制閥43來調整氣體之壓力與流量,即可達到控制氣壓缸22測頭之移動速度與負載大小,如此待測物A即可承受不同的負載能力。1. The present invention converts the conventional mechanical sensor into the form of the pneumatic cylinder 22 to give the load A to be tested, and integrates the force applying system and the air floating carrier 3 into one, unified by the gas supply system 4 The supply of the object to be tested A is floated, and the supply of the pneumatic cylinder 22 is provided with a load capacity, and the adjustment characteristics of the air supply condition and the load capacity of the object to be tested A are retained, and the pneumatic cylinder 22 is also adjusted by the air supply system 4. The load capacity, and through the pressure regulating valve 42 of the air pressure system 4 and the flow control valve 43 to adjust the pressure and flow of the gas, the moving speed and the load of the probe of the pneumatic cylinder 22 can be controlled, so that the object A can withstand Different load capacities.

二、以往的量測方式之出力範圍與規格多為固定,而本發明則可依待測物A的量測條件,調整該氣壓缸22所施加的負載大小範圍,以及可迅速更換合適規格的氣壓缸22,例如,當待測物A的負載能力較小時,則必須將針對氣壓缸22之負載規格,由大到小依序更換,直至可準確測得待測物A之負載能力;反之,當待測物A之負載能力較大時,則必須將氣壓缸22之負載規格,由小至大依序更換,直至可準確測得待測物A之最大負載能力。2. The range and specifications of the previous measurement methods are mostly fixed, and the present invention can adjust the range of load applied by the pneumatic cylinder 22 according to the measurement condition of the object A, and can quickly replace the appropriate specifications. The pneumatic cylinder 22, for example, when the load capacity of the object A to be tested is small, the load specifications for the pneumatic cylinder 22 must be sequentially changed from large to small until the load capacity of the object A can be accurately measured; On the other hand, when the load capacity of the object A is large, the load specifications of the pneumatic cylinder 22 must be sequentially changed from small to large until the maximum load capacity of the object A can be accurately measured.

三、本發明可藉由設定該氣壓缸22的氣壓系統參數,量測出待測物A在不同的供氣條件與承受不同負載能力的情況下,氣膜剛性的數值,達到快速量測的目的,其中,不同負載能力由氣壓缸22、調壓閥42、流量控制閥43所控制,調壓閥42與流量控制閥43分別調整氣壓缸22之移動速度與負載能力,以往的量測模式僅可量測最大氣膜承載力,其量測模式無彈性調整之空間;而本發明可控制氣壓缸22之負載大小,可以由小至大或由大至小的量測方式進行量測,並可任意設定氣壓缸22之負載大小,以測得在某一氣壓缸22之負載值下,待測物A之氣膜厚度。3. The present invention can determine the value of the air film rigidity of the object A under different gas supply conditions and with different load capacities by setting the air pressure system parameters of the pneumatic cylinder 22, and achieving rapid measurement. The purpose is that the different load capacities are controlled by the pneumatic cylinder 22, the pressure regulating valve 42, and the flow control valve 43, and the pressure regulating valve 42 and the flow control valve 43 respectively adjust the moving speed and load capacity of the pneumatic cylinder 22, and the previous measuring mode. Only the maximum gas film bearing capacity can be measured, and the measuring mode has no space for elastic adjustment; and the present invention can control the load of the pneumatic cylinder 22, and can be measured by small to large or large to small measuring methods. The load of the pneumatic cylinder 22 can be arbitrarily set to measure the film thickness of the object A under the load value of a certain pneumatic cylinder 22.

四、以往因機械式感測器所施加的負載大小多為固定,若待測物A的承載力超出機械式感測器所施加的負載大小範圍,則機械式感測器無法精準量測出待測物A的承載力,本發明以該氣壓缸22來量測待測物A的承載力,因此可依據量測情況,調整該氣壓缸22的壓力與流量,甚至更換成不同規格的氣壓缸22,以獲得較精確的承載力量測值,使得本發明具備彈性調整量測範圍的特點。4. In the past, the load applied by the mechanical sensor was mostly fixed. If the bearing capacity of the object A exceeds the load range applied by the mechanical sensor, the mechanical sensor cannot accurately measure the load. The bearing capacity of the object A to be tested, the present invention uses the pneumatic cylinder 22 to measure the bearing capacity of the object A, so that the pressure and flow rate of the pneumatic cylinder 22 can be adjusted according to the measurement condition, and even the air pressure of different specifications can be replaced. The cylinder 22 is used to obtain a more accurate bearing force measurement, so that the present invention has the feature of elastically adjusting the measurement range.

惟以上所述者,僅為本發明之較佳實施例而已,當不能以此限定本發明實施之範圍,即大凡依本發明申請專利範圍及發明說明內容所作之簡單的等效變化與修飾,皆仍屬本發明專利涵蓋之範圍內。The above is only the preferred embodiment of the present invention, and the scope of the invention is not limited thereto, that is, the simple equivalent changes and modifications made by the scope of the invention and the description of the invention are All remain within the scope of the invention patent.

2...精密比測平台單元2. . . Precision ratio platform unit

21...精密平台twenty one. . . Precision platform

22...氣壓缸twenty two. . . Pneumatic cylinder

23...千分錶twenty three. . . Dial indicator

3...氣浮載具3. . . Air bearing vehicle

4...供氣系統4. . . Gas supply system

41...空氣壓縮機41. . . Air compressor

42...調壓閥42. . . Pressure regulating valve

43...流量控制閥43. . . Flow control valve

44...冷凍乾燥機44. . . Freeze dryer

45...儲氣桶45. . . Gas storage bucket

46...精密過濾器46. . . Precision filter

47...方向控制閥47. . . Directional control valve

100...步驟100. . . step

200...步驟200. . . step

300...步驟300. . . step

400...步驟400. . . step

A...待測物A. . . Analyte

圖1是示意圖,說明以往的一種利用荷重試驗機的氣膜剛性檢測平台;Figure 1 is a schematic view showing a conventional gas film rigidity detecting platform using a load tester;

圖2是示意圖,說明本發明氣浮式平面軸承之氣膜剛性檢測平台的第一較佳實施例;Figure 2 is a schematic view showing a first preferred embodiment of the gas film rigidity detecting platform of the air floating type planar bearing of the present invention;

圖3是流程圖,說明本發明第一較佳實施例的使用方法;及Figure 3 is a flow chart illustrating the method of use of the first preferred embodiment of the present invention;

圖4是示意圖,說明本發明氣浮式平面軸承之氣膜剛性檢測平台的第二較佳實施例。Figure 4 is a schematic view showing a second preferred embodiment of the gas film rigidity detecting platform of the air floating type planar bearing of the present invention.

2...精密比測平台單元2. . . Precision ratio platform unit

21...精密平台twenty one. . . Precision platform

22...氣壓缸twenty two. . . Pneumatic cylinder

23...千分錶twenty three. . . Dial indicator

3...氣浮載具3. . . Air bearing vehicle

4...供氣系統4. . . Gas supply system

41...空氣壓縮機41. . . Air compressor

42...調壓閥42. . . Pressure regulating valve

43...流量控制閥43. . . Flow control valve

44...冷凍乾燥機44. . . Freeze dryer

45...儲氣桶45. . . Gas storage bucket

46...精密過濾器46. . . Precision filter

47...方向控制閥47. . . Directional control valve

A...待測物A. . . Analyte

Claims (5)

一種氣浮式平面軸承之氣膜剛性檢測平台,包含:一精密比測平台單元,包括一用於提供平坦表面的精密平台、一設置於該精密平台上方的氣壓缸,及一設置於該精密平台上方且連接於該氣壓缸的千分錶;一氣浮載具,放置於該精密平台上;及一供氣系統,連接該氣浮載具與該精密比測平台單元的氣壓缸。A gas film rigidity detecting platform for an air floating plane bearing comprises: a precision measuring platform unit, comprising a precision platform for providing a flat surface, a pneumatic cylinder disposed above the precision platform, and a precision setting a dial gauge connected to the pneumatic cylinder above the platform; an air floating carrier placed on the precision platform; and a gas supply system connecting the air bearing carrier and the pneumatic cylinder of the precision comparison platform unit. 根據申請專利範圍第1項所述之氣浮式平面軸承之氣膜剛性檢測平台,其中,該供氣系統包括一用於提供氣源的空氣壓縮機、一連接該空氣壓縮機的調壓閥,及複數個分別連接於該氣浮載具、氣壓缸與調壓閥間的流量控制閥。The air film rigidity detecting platform of the air floating type planar bearing according to claim 1, wherein the air supply system includes an air compressor for supplying a gas source, and a pressure regulating valve connected to the air compressor. And a plurality of flow control valves respectively connected between the air floating carrier, the pneumatic cylinder and the pressure regulating valve. 一種氣浮式平面軸承之氣膜剛性檢測平台的使用方法,包含以下步驟:(A)準備一如申請專利範圍第1項所述之氣浮式平面軸承之氣膜剛性檢測平台;(B)將該千分錶抵於待測物表面,進行該千分錶歸零;(C)啟動該供氣系統使待測物浮起,讀取該千分錶數值,得知氣膜厚度;及(D)啟動該氣壓缸以向下施壓力於待測物,向下施壓力至待測物不浮起,讀取該氣壓缸數值,得知氣膜的承載力。A method for using a gas film rigidity detecting platform for an air floating plane bearing comprises the following steps: (A) preparing a film rigidity detecting platform of an air floating plane bearing as described in claim 1; (B) The dial gauge is pressed against the surface of the object to be tested, and the dial gauge is reset to zero; (C) the gas supply system is activated to float the object to be tested, and the dial gauge value is read to obtain the film thickness; (D) The pneumatic cylinder is started to apply pressure to the object to be tested downward, and the pressure is applied downward until the object to be tested does not float, and the value of the pneumatic cylinder is read to know the bearing capacity of the gas film. 根據申請專利範圍第3項所述之氣浮式平面軸承之氣膜剛性檢測平台的使用方法,該步驟(A)中,該供氣系統包括一用於提供氣源的空氣壓縮機、一連接該空氣壓縮機的調壓閥,及複數個分別連接於該氣浮載具、氣壓缸與調壓閥間的流量控制閥,該步驟(C)中,開啟位於該調壓閥與該氣浮載具間的流量控制閥,該步驟(D)中,開啟位於該調壓閥與該氣壓缸間的流量控制閥。The method for using a gas film rigidity detecting platform of an air floating type planar bearing according to claim 3, wherein in the step (A), the gas supply system comprises an air compressor for providing a gas source, and a connection a pressure regulating valve of the air compressor, and a plurality of flow control valves respectively connected between the air floating carrier, the pneumatic cylinder and the pressure regulating valve, in the step (C), opening the pressure regulating valve and the air floating valve In the flow control valve between the vehicles, in the step (D), the flow control valve between the pressure regulating valve and the pneumatic cylinder is opened. 根據申請專利範圍第3項所述之氣浮式平面軸承之氣膜剛性檢測平台的使用方法,該步驟(B)中,待測物為氣浮載具。According to the method for using the gas film rigidity detecting platform of the air floating type planar bearing described in claim 3, in the step (B), the object to be tested is an air floating carrier.
TW100148385A 2011-12-23 2011-12-23 Membrane Rigidity Testing Platform for Air Floating Plane Bearing and Its Application TWI463125B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW100148385A TWI463125B (en) 2011-12-23 2011-12-23 Membrane Rigidity Testing Platform for Air Floating Plane Bearing and Its Application

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW100148385A TWI463125B (en) 2011-12-23 2011-12-23 Membrane Rigidity Testing Platform for Air Floating Plane Bearing and Its Application

Publications (2)

Publication Number Publication Date
TW201326779A TW201326779A (en) 2013-07-01
TWI463125B true TWI463125B (en) 2014-12-01

Family

ID=49224944

Family Applications (1)

Application Number Title Priority Date Filing Date
TW100148385A TWI463125B (en) 2011-12-23 2011-12-23 Membrane Rigidity Testing Platform for Air Floating Plane Bearing and Its Application

Country Status (1)

Country Link
TW (1) TWI463125B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114441330B (en) * 2022-02-07 2023-09-22 北京半导体专用设备研究所(中国电子科技集团公司第四十五研究所) Air floatation stiffness loading device, air floatation stiffness testing equipment and air floatation stiffness testing method
CN115962938B (en) * 2023-01-05 2023-06-27 西安航天精密机电研究所 Non-contact testing method for air film rigidity of H-shaped dynamic pressure bearing gyro motor of gyroscope

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04285809A (en) * 1991-03-14 1992-10-09 Tokyo Seimitsu Co Ltd Apparatus and method for measuring roughness
EP1235115A2 (en) * 2001-02-27 2002-08-28 Canon Kabushiki Kaisha Stage device and movement guidance method
JP2004011686A (en) * 2002-06-04 2004-01-15 Mitsutoyo Corp Air bearing
TW200724294A (en) * 2005-12-22 2007-07-01 Ushio Electric Inc Planar carrying stage device
TW201020076A (en) * 2008-11-17 2010-06-01 Stone & Resource Ind R & D Ct Compound type platform having bidirectional functions of air-floating and sucking
CN101852684A (en) * 2010-05-24 2010-10-06 中国计量学院 Performance testing device of static-pressure air bearing
TWM418018U (en) * 2011-05-20 2011-12-11 C Jac Ind Co Ltd Device capable of providing instantaneous pressure and impact velocity

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04285809A (en) * 1991-03-14 1992-10-09 Tokyo Seimitsu Co Ltd Apparatus and method for measuring roughness
EP1235115A2 (en) * 2001-02-27 2002-08-28 Canon Kabushiki Kaisha Stage device and movement guidance method
JP2004011686A (en) * 2002-06-04 2004-01-15 Mitsutoyo Corp Air bearing
TW200724294A (en) * 2005-12-22 2007-07-01 Ushio Electric Inc Planar carrying stage device
TW201020076A (en) * 2008-11-17 2010-06-01 Stone & Resource Ind R & D Ct Compound type platform having bidirectional functions of air-floating and sucking
CN101852684A (en) * 2010-05-24 2010-10-06 中国计量学院 Performance testing device of static-pressure air bearing
TWM418018U (en) * 2011-05-20 2011-12-11 C Jac Ind Co Ltd Device capable of providing instantaneous pressure and impact velocity

Also Published As

Publication number Publication date
TW201326779A (en) 2013-07-01

Similar Documents

Publication Publication Date Title
CN201166564Y (en) Non-contact test system for solar wafer
CN204495658U (en) The adjustable amount of deflection of complex condition and modulus tester
TWI463125B (en) Membrane Rigidity Testing Platform for Air Floating Plane Bearing and Its Application
CN106644692A (en) Test device for determining creep of concrete
CN104501899A (en) Device and method for precise measurement of volume and density of object
CN209085485U (en) A kind of measuring device of automobile air valve tappet inner convex platform height
CN101806569A (en) Tool for measuring thickness of lamination part of solar cell
CN102103063A (en) Stress corrosion test method and device for metal sheet pre-cracked sample
CN107941279B (en) For measuring the measuring device of air film various parameters in air-flotation system
CN204301670U (en) Adjustable air throttle board plane degree measuring instrument
CN109282778A (en) A kind of novel power battery thickness of the shell detection fixture
CN201016701Y (en) Apparatus for measuring thickness of battery
CN102128579B (en) Detecting device for measuring appearance with compound angle length
CN206832619U (en) One kind automation density measurement equipment
CN207019917U (en) A kind of tire vertical stiffness testing experiment stand of structure optimization
CN214149185U (en) Flatness detection structure and detection system
CN103185683B (en) The air film rigidity detection platform of air-flotation type plane bearing and using method thereof
CN201748898U (en) Thermal deformation detecting instrument
CN202024708U (en) Device for detecting recess and bump defects on surface of battery laminate
CN206037985U (en) Measuring device and system of cold heat exchanger plane degree of new energy automobile battery
CN208952929U (en) A kind of novel power battery thickness of the shell detection fixture
CN109341645B (en) Flatness measurement jig and pressing equipment
CN201885971U (en) Sample table for testing crystalline silicon solar cell in ellipsometer
CN206847851U (en) A kind of pressure sensor metrology and measurement fixture
CN208780578U (en) Carbon dioxide eliminating measuring device