|
CN110537021A
|
|
Vane pump
|
|
CN1813079A
|
|
Production device and method for multiple-system film and coating tool for multiple-system film
|
|
CN1816643A
|
|
Multinary deposition film production stabilizing device and method, and tool with multinary deposition film
|
|
JP2005106411A
|
|
Pre-filmer type air blast granulating nozzle
|
|
JP2005102405A
|
|
Cable connector
|
|
JP2005088804A
|
|
Variable delta wing airplane and its fuselage attitude controlling method
|
|
JP2005093449A
|
|
Photovoltaic energy utilization system
|
|
JP2005085012A
|
|
Noise reduction method in image processing
|
|
JP2005082018A
|
|
Aircraft staying in high altitude for long time, its flight control system as well as its communication and observation system
|
|
JP2005075923A
|
|
Pressure sensitive coating material using fluorine-based polymer
|
|
JP2005069948A
|
|
Electronic timepiece, its stepping compensation method, and recording time correction method therefor
|
|
JP2004035896A
|
|
Low temperature thermosensitive coating
|
|
JP2005072913A
|
|
Method for accurately forming reflection mirror shape into designated shape
|
|
JP2005062064A
|
|
Noncontact measuring device
|
|
JP2005061330A
|
|
Free piston type stirling engine
|
|
JP2005057649A
|
|
Electromagnetic wave converging device made of shape storage polymeric material,its mirror plane ramification and the profile retain method
|
|
JP2005050016A
|
|
Shape recognition device, method, and program
|
|
US2005016157A1
|
|
Combine engine for single-stage spacecraft
|
|
JP2005033561A
|
|
Antenna element and antenna employing it
|
|
JP2005036717A
|
|
Ion engine having thrust direction control mechanism
|
