-
公开(公告)号：US5195701A
公开(公告)日：1993-03-23
申请号：US830725
申请日：1992-02-04
Applicant: W. Craig Willan
Inventor： W. Craig Willan
CPC classification number: B65D90/325 , B64D45/0015 , B64D9/00 , B65D88/14 , B65D90/36 , B64D2045/005
Abstract: An air cargo container with features for reducing damage caused by a bomb explosion. The container has a venting device which faces a fuselage wall of an airplane when the container is stowed. An explosion propels the venting device to pierce the fuselage wall of the airplane in the event of an explosion. This creates a hole which vents the shock waves and gas from the explosion.
Abstract translation: 一个空运货物集装箱，具有减少炸弹爆炸造成的损坏的特点。 当容器被收起时，容器具有面向飞机的机身壁的排气装置。 发生爆炸时，爆炸会促使通风装置刺穿飞机的机身墙壁。 这产生了一个孔，从爆炸中排出冲击波和气体。
-
公开(公告)号：US5294059A
公开(公告)日：1994-03-15
申请号：US895781
申请日：1992-06-09
Applicant: W. Craig Willan
Inventor： W. Craig Willan
CPC classification number: E21B10/60 , B05B1/00 , B05B3/1028
Abstract: A device for directing the flow of an atomized slurry from the ejection orifice of an atomizer housing which is composed of a cylindrical liner bushing made of a wear-resistant material and a cylindrical sleeve bushing designed to support the liner bushing within the ejection orifice of the atomizer housing. The geometries of the liner and sleeve bushings form an annular, recessed shoulder at the discharge end of the bushings During rotation of the atomizer, turbulent flow eddy currents pack slurry media into this shoulder. The liner bushing is bonded in the sleeve bushing under compression to create a residual preload opposing the centrifugal force generated by rotation of the atomizer housing.
Abstract translation: 用于引导来自雾化器壳体的喷射口的雾化浆料的流动装置，其由由耐磨材料制成的圆柱形衬套和用于将衬套衬套支撑在衬套衬套的喷射孔内的圆柱形衬套 雾化器外壳 衬套和套筒衬套的几何形状在衬套的排放端处形成环形凹入的肩部。在雾化器旋转期间，湍流涡流将浆料介质包装到该肩部中。 衬套衬套在压缩下结合在套管衬套中，以形成与由雾化器壳体旋转产生的离心力相反的残余预压。
-
公开(公告)号：US5370310A
公开(公告)日：1994-12-06
申请号：US196513
申请日：1994-02-14
Applicant: W. Craig Willan
Inventor： W. Craig Willan
CPC classification number: E21B10/60 , B05B1/00 , B05B3/1028
Abstract: A device for directing the flow of an atomized slurry from the ejection orifice of an atomizer housing which is composed of a cylindrical liner bushing made of a wear-resistant material and a cylindrical sleeve bushing designed to support the liner bushing within the ejection orifice of the atomizer housing. The geometries of the liner and sleeve bushings form an annular, recessed shoulder at the discharge end of the bushings. During rotation of the atomizer, turbulent flow eddy currents pack slurry media into this shoulder. The liner bushing is bonded in the sleeve bushing under compression to create a residual preload opposing the centrifugal force generated by rotation of the atomizer housing.
Abstract translation: 用于引导来自雾化器壳体的喷射口的雾化浆料的流动装置，其由由耐磨材料制成的圆柱形衬套和用于将衬套衬套支撑在衬套衬套的喷射孔内的圆柱形衬套 雾化器外壳 衬套和衬套衬套的几何形状在衬套的排放端处形成环形的凹入的肩部。 在雾化器旋转期间，湍流涡流将浆料介质包装到该肩部中。 衬套衬套在压缩下结合在套管衬套中，以形成与由雾化器壳体旋转产生的离心力相反的残余预压。
-
公开(公告)号：US4976136A
公开(公告)日：1990-12-11
申请号：US421402
申请日：1989-10-13
Applicant: W. Craig Willan
Inventor： W. Craig Willan
IPC: G01M3/20
CPC classification number: G01M3/20
Abstract: A method of detecting cracks and structural separations in the fuselage of an aircraft utilizes a highly detectable gas such as chlorofluorocarbon. The gas will be pumped into the interior of the fuselage until the fuselage reaches a pressure that occurs during normal flight operations. A detector will then be moved over the skin of the fuselage. The detector is of a type that will detect minute amounts of any gas escaping through cracks and structural separations in the fuselage. The detector has an entrapment shoe which entraps any gas that might be bleeding off through a tiny crack. The detector has an alarm circuit which provides an alarm to the operator.
Abstract translation: 一种检测飞机机身裂缝和结构分离的方法利用高度可检测的气体如氯氟烃。 气体将被泵送到机身内部，直到机身达到在正常飞行操作期间发生的压力。 然后将检测器移动到机身的皮肤上。 检测器是一种类型，可以检测微小的任何气体通过机身中的裂纹和结构分离而逸出。 检测器具有一个夹带鞋，其夹带任何可能通过微小裂纹渗出的气体。 检测器具有向操作者提供报警的报警电路。
-
-
-
Search Results
4
records
(took 0.01 seconds)
