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 rotor providing for tilting of axis and blade pitch regulation
摘要
申请公布号
US2444070(A)
申请公布日期
1948.06.29
申请号
US19420442911
申请日期
1942.05.14
申请人
AUTOGIRO COMPANY
发明人
STANLEY PAUL H.
分类号
B64C27/30
主分类号
B64C27/30
代理机构
代理人
主权项
地址
您可能感兴趣的专利
CUTTING METHOD OF EXTRUDED ARTICLE
METHOD FOR MANUFACTURING MESOPOROUS STRUCTURE
COATING METHOD
ULTRASONIC CLEANING SYSTEM AND ULTRASONIC CLEANING METHOD
SPRINKLING NOZZLE
MICROSAMPLE RECOVERY MECHANISM AND MICROSAMPLE RECOVERY METHOD
MODE SETTING CONTROL FOR GRAIN PREPARATION FACILITY
PACHINKO GAME MACHINE
FLUIDIZED-BED APPARATUS AND METHOD FOR CLEANING FILTER IN THE SAME
CRUSHING MACHINE
PACHINKO MACHINE
BOARD CASE OF PACHINKO MACHINE
SLOT MACHINE AND ITS PLAY METHOD
TWO FINGER APPROACHABLE CLOTHESPIN
CLIP SENSOR
SLIDE-EXTENSION HANGER FOR FREE SIZE AND STYLE
GAME MACHINE
INFORMATION PROCESSOR AND ITS CONTROL METHOD, INFORMATION DISPLAY DEVICE AND CONTROL METHOD, AND PROGRAM
SHEARING BLADE UNIT
ANTI-SLIP MAT