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1. 发明授权

US3712063A Cooled pintle assembly 失效
标题翻译：冷却紧固件总成
公开(公告)号：US3712063A
公开(公告)日：1973-01-23
申请号：US3712063D
申请日：1970-03-24
申请人： BELL AEROSPACE CORP
发明人： ANDRYSIAK S , MCKENNA R
IPC分类号： F02K9/52 , F02K9/58 , F02K9/64 , F02K9/86 , F02K9/97 , F02K
CPC分类号： F02K9/86 , F02K9/52 , F02K9/58 , F02K9/64 , F02K9/97
摘要： To maintain a constant pressure in the combustion chamber of a rocket engine, which operates with either liquid and/or metallized propellants, a cooled throat pintle assembly is provided to vary the throat area in an E-D nozzle. The pintle design is a composite structure consisting of a Columbium alloy central rod member having in its cylindrical and injector portions a Grafoil intermediate layer and a Carbitex outer layer. The throat portion of the pintle assembly consists of stacked pyrolytic graphite washers having a spiral formed coolant passages. The throat, cylindrical, and injector portions of the pintle are gas film cooled with fuel-rich gases that are ducted through the center of the pintle from a pressurization system gas generator. The injector or forward end of the pintle is cooled by a gas film exiting from the pintle housing. The throat portion of the pintle is cooled by gases exiting through spiral grooves in the washers.
摘要翻译：为了在与液体和/或金属化的推进剂一起操作的火箭发动机的燃烧室中保持恒定的压力，提供冷却的喉咙组件以改变E-D喷嘴中的喉部区域。枢轴设计是由Columbium合金中心杆构件组成的复合结构，其中其圆柱形和喷射器部分具有Grafoil中间层和Carbitex外层。枢轴组件的喉部由具有螺旋形冷却剂通道的层叠热解石墨垫圈组成。枢轴的喉部，圆柱形和注射器部分是用富含燃料的气体冷却的气膜，其通过来自加压系统气体发生器的枢轴的中心导管。枢轴的注射器或前端由从枢轴外壳排出的气膜冷却。枢轴的喉部由通过垫圈中的螺旋槽排出的气体冷却。

2. 发明授权

US3570807A Electromechanical control valve 失效
标题翻译：机电控制阀
公开(公告)号：US3570807A
公开(公告)日：1971-03-16
申请号：US3570807D
申请日：1969-01-14
申请人： BELL AEROSPACE CORP
发明人： STURMAN ODED E , SCIORTINO SALVATORE A , KASSIR ABDUL R
IPC分类号： F16K31/06 , F16K31/08 , F16K31/10
CPC分类号： F16K31/0682
摘要： An electromechanical control valve in which a poppet is magnetically biased against a valve seat and is mechanically unseated upon decrease of the magnetic moment. A suspension plate carries the poppet on one side thereof and an armature on the other side to constitute an integrated assembly. A permanent magnet attracts the armature to thereby bias the poppet against the seat and deform the suspension plate. A coil is disposed on the armature and, when energized, develops a magnetic potential in opposition to the magnetic potential of the permanent magnet to thereby decrease the permanent magnet attraction whereby the deformed suspension plate, acting as a spring, urges the poppet out of the seat. The coil can be disposed so as to positively attract the armature through the null point to an opposite poll. The suspension plate also serves to isolate the magnetic circuit from the poppet-seat area.

3. 发明授权

US3570806A Balanced electromechanical control valve 失效
标题翻译：平衡电动控制阀
公开(公告)号：US3570806A
公开(公告)日：1971-03-16
申请号：US3570806D
申请日：1969-01-14
申请人： BELL AEROSPACE CORP
发明人： STURMAN ODED E , SCIORTINO SALVATORE A , KASSIR ABDUL R
IPC分类号： F16K31/08
CPC分类号： F16K31/082
摘要： An electromechanical control valve in which a poppet is biased against a seat therefor within an enclosing chamber having inlet and outlet ports and which is balanced against fluid pressure forces. Oppositely disposed walls of the chamber are deformable and a force-transmitting rod carries the poppet between such deformable walls whereby displacement of the poppet causes deformation of the walls to urge the poppet in the opposite direction. A system geometry is utilized which takes into account the effective surfaces of the poppet and the configurations of the walls when deformed. In particular embodiments, bias on the poppet is obtained by the application of the magnetic potential of a permanent magnet operatively associated with an armature extension of the poppet outside the chamber. The permanent magnet biases the poppet to its seat and a coil is disposed on the armature to oppose the permanent magnet potential whereby the deformed chamber walls, acting as springs, urge the poppet to an open position.

4. 发明授权

US3570373A Valve operator and method of making the same 失效
标题翻译：阀操作器及其制作方法
公开(公告)号：US3570373A
公开(公告)日：1971-03-16
申请号：US3570373D
申请日：1969-04-25
申请人： BELL AEROSPACE CORP
发明人： TUPKER WILLEM E
IPC分类号： F16K27/00 , F15B15/06 , F15B15/08 , F16K1/22 , F16K31/163 , F01B9/00
CPC分类号： F15B15/066 , F16K1/221 , F16K31/1635
摘要： The valve operator disclosed includes a housing constructed of substantially identical housing halves joined together at mating surfaces. Cylinder means is secured to the housing and bridges the housing halves.

5. 发明授权

US3554094A Piston rod locking mechanism 失效
标题翻译：活塞杆锁定机构
公开(公告)号：US3554094A
公开(公告)日：1971-01-12
申请号：US3554094D
申请日：1969-02-20
申请人： BELL AEROSPACE CORP
发明人： GROSS GEORGE
IPC分类号： B23Q1/28 , F15B15/26
CPC分类号： F15B15/262 , B23Q1/28
摘要： A piston rod locking mechanism in which a locking ring is formed with an eccentric bore for the rod. Means are provided for rotating the locking ring eccentrically with respect to the bore to thereby bind the rod against axial movement.

6. 发明授权

US3521534A Hydraulic link in a control system 失效
标题翻译：控制系统中的液压连杆
公开(公告)号：US3521534A
公开(公告)日：1970-07-21
申请号：US3521534D
申请日：1968-07-18
申请人： BELL AEROSPACE CORP
发明人： CASTERLINE LESLEY C , PAUW FRANCIS E DE
IPC分类号： F15B11/048 , F15B13/16 , F01B15/02
CPC分类号： F15B11/048 , F15B2211/30525 , F15B2211/3144 , F15B2211/32 , F15B2211/325 , F15B2211/329 , F15B2211/755

7. 发明授权

US3500380A Binary input torque motor 失效
标题翻译：二进制扭矩电机
公开(公告)号：US3500380A
公开(公告)日：1970-03-10
申请号：US3500380D
申请日：1965-10-22
申请人： BELL AEROSPACE CORP
发明人： JESSEE JAMES M
IPC分类号： F15B9/17 , H03M1/00 , H03K13/00 , H04L3/00
CPC分类号： F15B9/17 , H03M1/00 , H03M1/22

8. 发明授权

US3496561A Parallel binary signal digital to analog converter having magnetically saturated armature 失效
标题翻译：并行二进制信号数字到具有静态饱和度的模拟转换器
公开(公告)号：US3496561A
公开(公告)日：1970-02-17
申请号：US3496561D
申请日：1965-12-20
申请人： BELL AEROSPACE CORP
发明人： SEIDEL DAVID S
IPC分类号： F15B13/043 , H03M1/00 , H04L3/00 , H03K13/00
CPC分类号： F15B13/0438 , H03M1/00 , H03M1/124

9. 发明授权

US3494513A Positive expulsion tank 失效
标题翻译：积极展示罐
公开(公告)号：US3494513A
公开(公告)日：1970-02-10
申请号：US3494513D
申请日：1966-08-11
申请人： BELL AEROSPACE CORP
发明人： BAUER WILLIAM H
IPC分类号： B64G1/40 , F02K9/60 , B67D5/40
CPC分类号： B64G1/402 , F02K9/605

10. 发明授权

US3488029A Return pressure compensated hydraeric signal comparator 失效
标题翻译：返回压力补偿液压信号比较器
公开(公告)号：US3488029A
公开(公告)日：1970-01-06
申请号：US3488029D
申请日：1968-04-11
申请人： BELL AEROSPACE CORP
发明人： DURBIN JAMES L
IPC分类号： B64C13/42 , F16K31/12 , F15B11/08 , F15B13/04
CPC分类号： B64C13/42

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