首页
产品
黄页
商标
征信
会员服务
注册
登录
全部
|
企业名
|
法人/股东/高管
|
品牌/产品
|
地址
|
经营范围
发明名称
Aircraft pitch-axis stability and command augmentation system
摘要
申请公布号
EP0743243(B1)
申请公布日期
2000.03.29
申请号
EP19950202999
申请日期
1995.11.06
申请人
THE BOEING COMPANY
发明人
NAJMABADI, KIOUMARS;COLEMAN, EDWARD E.;EVAND, MONTE R.;BLEEG, ROBERT J.;BREUHAUS, RICHARD S.;NELSON, TIMOTHY A.;ANDERSON, DORR MARSHALL
分类号
B64C13/16;G05D1/08;(IPC1-7):B64C13/16
主分类号
B64C13/16
代理机构
代理人
主权项
地址
您可能感兴趣的专利
Constructional element, building system and method of construction
Position sensing device having a movable photosensing element
METHOD AND APPARATUS FOR THE NON-INVASIVE DETERMINATION OF CARDIAC OUTPUT
Voltage clamp circuit
Hip bath
Bill validator having a bill detection device
Well completion methods
Water drain panel for basement
Emergency link
Clip for a gutter guard
Bidirectional temperature and pressure effect compensator for inflatable elements
Imaging member containing heat sensitive hyperbranched polymer and methods of use
Mattress arrangement
Method for X-ray micro-diffraction measurement and X-ray micro-diffraction apparatus
Device for controlling the quality of packets of cigarettes
Method and system for integrating material quality data
Method for actuating electromagnetic actuators
POLYNUCLEOTIDES AND POLYPEPTIDES ENCODED THEREBY
REGULATION OF HUMAN MEMBRANE-TYPE SERINE PROTEASE
18806,TRYPSIN SERINE PROTEASE-LIKE MOLECULE AND USES THEREOF