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DS16F95J/883 PDF预览

DS16F95J/883

更新时间： 2024-01-14 01:07:43
品牌 Logo 应用领域
德州仪器 - TI 驱动接口集成电路总线收发器驱动器
页数 文件大小 规格书
20页 631K
描述
EIA-485/EIA-422A 差分总线收发器 | NAB | 8 | -55 to 125

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DS16F95J/883 技术参数

生命周期：Active零件包装代码：DIP
包装说明：DIP, DIP8,.3针数：8
Reach Compliance Code：not_compliantECCN代码：EAR99
HTS代码：8542.39.00.01风险等级：5.11
Is Samacsys：N其他特性：LG_MAX; SEATED HGT-NOM
差分输出：YES驱动器位数：1
高电平输入电流最大值：0.00002 A输入特性：DIFFERENTIAL SCHMITT TRIGGER
接口集成电路类型：LINE TRANSCEIVER接口标准：EIA-422-A; EIA-485; SCSI-1
JESD-30 代码：R-GDIP-T8JESD-609代码：e0
长度：10.16 mm湿度敏感等级：1
功能数量：1端子数量：8
最高工作温度：125 °C最低工作温度：-55 °C
最小输出摆幅：1.5 V输出特性：3-STATE
最大输出低电流：0.00002 A输出极性：TRUE
封装主体材料：CERAMIC, GLASS-SEALED封装代码：DIP
封装等效代码：DIP8,.3封装形状：RECTANGULAR
封装形式：IN-LINE峰值回流温度（摄氏度）：NOT SPECIFIED
电源：5 V认证状态：Not Qualified
最大接收延迟：38 ns接收器位数：1
筛选级别：MIL-STD-883座面最大高度：5.08 mm
子类别：Line Driver or Receivers最大压摆率：28 mA
最大供电电压：5.5 V最小供电电压：4.5 V
标称供电电压：5 V电源电压1-最大：5.5 V
电源电压1-分钟：4.5 V电源电压1-Nom：5 V
表面贴装：NO技术：BIPOLAR
温度等级：MILITARY端子面层：Tin/Lead (Sn/Pb)
端子形式：THROUGH-HOLE端子节距：2.54 mm
端子位置：DUAL处于峰值回流温度下的最长时间：NOT SPECIFIED
最大传输延迟：25 ns宽度：7.62 mm
Base Number Matches：1

DS16F95J/883 数据手册

 浏览型号DS16F95J/883的Datasheet PDF文件第4页浏览型号DS16F95J/883的Datasheet PDF文件第5页浏览型号DS16F95J/883的Datasheet PDF文件第6页浏览型号DS16F95J/883的Datasheet PDF文件第8页浏览型号DS16F95J/883的Datasheet PDF文件第9页浏览型号DS16F95J/883的Datasheet PDF文件第10页 
DS16F95QML  
www.ti.com  
SNOSAN0B –SEPTEMBER 2005–REVISED APRIL 2013  
DC - Receiver Electrical Characteristics(1) (continued)  
The following conditions apply to all parameters, unless otherwise specified. VCC = 5.5V  
Symbol  
IOS  
Parameter  
Conditions  
VIN = 1V, VOUT = 0V  
Notes  
Min Max  
Unit  
Sub-group  
Output Short Circuit  
-85  
-15  
mA  
1, 2, 3  
VCC = 4.5V, VO = 2.5V,  
VCM = 12V & 0V & -7V, IO = -.4mA  
.2  
V
V
V
V
1, 2, 3  
1, 2, 3  
1, 2, 3  
1, 2, 3  
Differential Input High  
Threshold  
VTH  
VCC = 5.5V, Vo = 2.5V,  
VCM = 12V & 0V & -7V, IO = -.4mA  
.2  
VCC = 4.5V, VO = .5V,  
VCM = 12V & 0V & -7V, IO = 8mA  
-.2  
-.2  
Differential Input Low  
Threshold  
VT1  
VTH  
VCC = 5.5V, VO = .5V,  
VCM = 12V & 0V & -7V, IO = 8mA  
+
VCC = 4.5V, VCM = 0V  
VCC = 5.5V, VCM = 0V  
35  
35  
mV  
mV  
1, 2, 3  
1, 2, 3  
Hyteresis  
- (VTH-)  
DC - Both Driver and Receiver Electrical Characteristics(1)  
The following conditions apply to all parameters, unless otherwise specified. VCC = 5.5V  
Symbol  
ICC  
Parameter  
Conditions  
RE = 2V, DE = .8V  
Notes  
Min Max  
Unit  
mA  
mA  
V
Sub-group  
1, 2, 3  
1, 2, 3  
1, 2, 3  
1, 2, 3  
1, 2, 3  
1, 2, 3  
1, 2, 3  
1, 2, 3  
Supply Current ICC Both Disable  
Supply Current ICC Both Enable  
Input Clamp Volt  
25  
ICC  
VIC  
VIH  
VIL  
VIH  
VIL  
I IL  
RE =.8V, DE = 2V  
II = -18mA  
28  
-1.3  
2
Logical "1" Input Voltage  
Logical "0" Input Voltage  
Logical "1" Enable Input Voltage  
Logical "0" Enable Input Voltage  
Logical "0" Input Current  
V
.8  
V
2
V
.8  
V
VI = 0.4V  
See(2)  
-50  
uA  
(1) Pre and post irradiation limits are identical to those listed under A C and DC electrical characteristics. These parts may be dose rate  
sensitive in a space environment and demonstrate enhanced low dose rate effect. Radiation end point limits for the noted parameters  
are ensured only for the conditions as specified in MIL-STD 883, Method 1019, condition A.  
(2) Negative sign of the limits indicates the direction of the current flow only.  
AC - Driver Electrical Characteristics(1)  
The following conditions apply to all parameters, unless otherwise specified.  
VCC = 5V, PRR = 1MHZ, TR ≤ TF ≤ 6nS, 50% duty cycle, AMP = 3V, VLO, ZOUT = 50Ω  
Symbol  
tDD  
Parameter  
Conditions  
Notes  
Min  
8
Max  
25  
30  
25  
30  
18  
25  
18  
25  
35  
45  
40  
50  
Unit  
nS  
nS  
nS  
nS  
nS  
nS  
nS  
nS  
nS  
nS  
nS  
nS  
Sub-group  
Differential Output Delay Time  
(See Figure 6)  
9
10, 11  
9
RL = 60Ω  
RL = 60Ω  
RL = 27Ω  
RL = 27Ω  
See(2)  
8
Differential Output Transition  
Time (See Figure 6)  
8
tTD  
See(2)(3)  
8
10, 11  
9
Propagation Delay Time Low to  
High (See Figure 7)  
6
tPLH  
tPHL  
tPZH  
tPZL  
6
10, 11  
9
Propagation Delay Time high to  
Low (See Figure 7)  
6
6
10, 11  
9
Output Enable Time to H  
(See Figure 8)  
RL = 110Ω  
RL = 110Ω  
10, 11  
9
Output Enable Time to L  
(See Figure 9)  
10, 11  
(1) Pre and post irradiation limits are identical to those listed under A C and DC electrical characteristics. These parts may be dose rate  
sensitive in a space environment and demonstrate enhanced low dose rate effect. Radiation end point limits for the noted parameters  
are ensured only for the conditions as specified in MIL-STD 883, Method 1019, condition A.  
(2) Rise time 20% to 80%, Fall time 80% to 20%.  
(3) tTD = Non-inverting output rise time + inverting output fall time / 2, Non-inverting output fall time + inverting output rise time / 2.  
Copyright © 2005–2013, Texas Instruments Incorporated  
Submit Documentation Feedback  
7
Product Folder Links: DS16F95QML  
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