OPTIMIZATION OF FAULT DIAGNOSIS IN HELICOPTER HEALTH AND USA(77)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

This mechanism allows an assembly to call the methods of any COM object implementing IDispatch without needing to be compiled to run any
B.2. OBJECT ORIENTED PROGRAMMING
other interface than IDispatch. Consequently, an assembly can generate code "on the .y", and feed it to an object instance through its IDispatch interface. This functionality is deployed by most win32 based script engines, includ-ing Microsoft Internet Explorer and Matlab. COM objects implementing IDispatch are commonly referred to as automation or ActiveX objects.

B.2.4 .net
This technology is developed by Microsoft, and is a continuation of the COM / ActiveX concept. A .net application runs inside a framework, much like a Java application. Consequently, memory deallocation is no longer the re-sponsibility of the object programmer, but is handled by the framework. Framework implementations does however only exist for Microsoft operat-ing systems, making .net applications non-portable to other platforms. This decrease in generality, compared to Java, gives .net applications access to Microsoft speci.c features such as the system registry and the real-time li-brary DirectX. Objects developed in .net are cross compatible with COM, meaning that they can both make use of existing COM objects as well as exposing their own COM interface.
Objects developed in .net are organized in namespaces, which serve the same function as Java packages. A .net application can e.ortlessly load objects at runtime, either from a prede.ned library location, or from an ex-plicitly de.ned source. Thus, machine code can be imported into the running assembly from any source, remote or local, or even from code compiled at runtime.

 

List of Figures

2.1
HUMSOverview
......................... 15

2.2
MechanicalOverview
....................... 21

2.3
Mechanical
overview
for
AS332L2,
part
1.
.
.
.
.
.
.
.
.
.
.
.
22
2.4
Mechanical
overview
for
AS332L2,
part
2.
.
.
.
.
.
.
.
.
.
.
.
23
2.5
AS332L2
left
hand
ancillary
intermediate
gear
acquisition.
. . 24
2.6
AS332L2
left
hand
ancillary
intermediate
gear
acquisition.
. . 24
3.1
DiagnosisOverview........................ 34

3.2
An
indicator
breaching
its
threshold.
. . . . . . . . . . . . . . 44
3.3
Relevant
clusters
for
shaft
fault
detection.
. . . . . . . . . . . 45
3.4
ARMSdata.ow
......................... 50
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：OPTIMIZATION OF FAULT DIAGNOSIS IN HELICOPTER HEALTH AND USA(77)