| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 341 | 船舶水下应急救援航潜器 | CN201921623800.3 | 2019-09-27 | CN210503132U | 2020-05-12 | 尚雨贤; 张振浩; 范潇然; 马宁婧 |
| 本实用新型公开了船舶水下应急救援航潜器，包括外壳、操纵控制系统、垂直推进系统、动力推进系统、应急修补系统、停靠固定系统、照明灯、耐压罩、摄像头、智能传感系统以及电源、电子调速器，所述停靠固定系统的上端设置有应急修补系统，本实用新型可实现船舶应急观测和船舶破舱应急堵漏，达到了实现智能化、精确化的水下自由移动式下潜无人特种作业，本通过停靠固定系统为微型的水环真空泵吸盘，可使机器人牢固吸附于船壁，利用填补充气囊通过充气方法使其膨胀，当填补充气囊内的气体压力达到规定要求时，填补充气囊填满整个管道断面，利用填补充气囊壁与管道产生的摩擦力堵住漏水，可迅速完成小面积破舱堵漏作业。 | ||||||
| 342 | 一种高压氧舱内呼吸气缓冲雾化加湿装置 | CN202223482229.2 | 2022-12-27 | CN219208589U | 2023-06-20 | 郑衍金; 邵帅; 王有存; 边永辉; 公涛; 孙文红 |
| 本实用新型要解决的问题是提供一种高压氧舱内呼吸气缓冲雾化加湿装置，在对氧气进行雾化加湿的同时，达到了供氧缓冲并降低吸氧阻力的目的，符合相关医疗卫生规范或者相关标准的规定，其包括有耐压密封的缓冲雾化加湿杯，其包括杯体和设在杯体顶端的杯盖，所述杯盖上设有进气管口、出气管口和雾化管口；雾化进气管，其竖直向贯穿并配合安装在所述雾化管口上；虹吸管，其竖直向设置在所述杯体内部，其内部设有贯穿底端的液体流道，其侧壁横向设有连通所述液体流道的出液口，所述出液口靠近所述雾化进气管下端的喷射口并位于所述喷射口正下方。 | ||||||
| 343 | PRESSURE BULKHEAD FOR AN AEROSPACE FUSELAGE | PCT/EP2007/056137 | 2007-06-20 | WO2008000670A2 | 2008-01-03 | BASSO, Pasquale |
The present invention describes a pressure bulkhead (1, 1') for an aerospace fuselage (10) comprising a bulkhead main portion (3) having an approximately flat shape in unloaded state; and a frame (2) supporting and connecting said bulkhead main portion (3) to the fuselage (10); wherein said bulkhead main portion (3) comprises an airtight structure having a reticular component (5, 5', 5" ). |
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| 344 | PRESSURE BULKHEAD FOR AN AEROSPACE FUSELAGE | PCT/EP2007056137 | 2007-06-20 | WO2008000670A3 | 2008-02-21 | BASSO PASQUALE |
| The present invention describes a pressure bulkhead (1, 1') for an aerospace fuselage (10) comprising a bulkhead main portion (3) having an approximately flat shape in unloaded state; and a frame (2) supporting and connecting said bulkhead main portion (3) to the fuselage (10); wherein said bulkhead main portion (3) comprises an airtight structure having a reticular component (5, 5', 5" ). | ||||||
| 345 | УЗЕЛ СТЫКА ОТСЕКОВ ФЮЗЕЛЯЖА САМОЛЕТА И ЕГО ГЕРМОШПАНГОУТ | PCT/RU2012/000715 | 2012-08-30 | WO2013032369A1 | 2013-03-07 | БАРАНОВ, Юрий Александрович; БРЯНЦЕВ, Сергей Федорович |
Технической задачей, решаемой заявляемыми решениями узла стыка отсеков фюзеляжа самолета и гермошпангоута, является разработка конструкций небольшой массы в сочетании с повышенной эксплуатационной живучестью узла стыка и гермошпангоута. Узел стыка отсеков содержит обшивки стыкуемых герметичного и негерметичного отсеков, подкрепленные стрингерами, и гермошпангоут, расположенный в месте стыка герметичного и негерметичного отсеков, фитинги, расположенные по разные стороны гермошпангоута, и стыковую ленту. Гермошпангоут содержит сферическую оболочку с меридиально ориентированными силовыми элементами, внутренний и наружный пояса, стенку и ленту-дублер. Сферическая оболочка оперта на стенку гермошпангоута. Лента-дублер выполнена в форме кругового кольца с профилем, выполненным с перегибом. Внутренняя полка ленты-дублера помещена между стенкой гермошпангоута и сферической оболочкой, а внешняя полка между фитингами, размещенными в герметичном отсеке, и наружным поясом гермошпангоута. Меридиально ориентированные силовые элементы соединены в единый пакет со сферической оболочкой, лентой-дублером и стенкой гермошпангоута. |
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| 346 | PRESSURE FUSELAGE OF AN AIRCRAFT WITH A FUSELAGE SHELL AND A PRESSURE BULKHEAD DISPOSED THEREIN | EP13711334.6 | 2013-03-18 | EP2828146B1 | 2017-05-03 | ZUARDY, Ichwan; GRASE, Karim; ROWEDDER, Carsten; DE JONG, Claas; MUELLER, Markus; JESSRANG, Mathias |
| 347 | 一种带有不锈钢管的橡胶冷却水管总成 | CN202323231844.0 | 2023-11-29 | CN220979655U | 2024-05-17 | 薛建乾; 薛鹏林; 吴朝俊; 葛家伟; 王兆响; 吴军科; 龙俊明 |
| 本实用新型涉及一种带有不锈钢管的橡胶冷却水管总成，包括第一橡胶管和第二橡胶管，第一橡胶管的一端与第二橡胶管的一端之间插接有不锈钢管并通过卡箍卡紧固定，不锈钢管的一端设有旁通管，且不锈钢管的管壁上固定有三个安装支架，三个安装支架上均设有安装孔，通过安装支架将不锈钢管安装在发动机侧壁上，第一橡胶管和/或第二橡胶管上安装有塑料卡夹，通过塑料卡夹将第一橡胶管和/或第二橡胶管卡接在发动机舱内；本实用新型的有益效果为：两根橡胶管之间插接不锈钢管，且不锈钢管安装在发动机侧壁上，使得发动机侧壁上所安装的不锈钢管的耐腐蚀性、耐高温性、耐压性和耐磨性更好，可以在高温、高压和恶劣的环境下长期稳定运行。 | ||||||
| 348 | 滚塑聚乙烯塑钢复合船用储罐 | CN201120111268.4 | 2011-04-15 | CN202022491U | 2011-11-02 | 杭新华 |
| 本实用新型涉及一种滚塑聚乙烯塑钢复合船用储罐。其包括罐体，其特征在于：所述罐体包括罐身、罐底和上封头，所述罐身为圆柱形结构，罐身下沿与罐底边沿采用圆弧过渡连接，罐身上沿与上封头边沿连接；所述上封头的中心部位向上延伸形成有罐颈，罐颈用于伸出船体的甲板，以便于进出料；在罐颈上部的外壁设有连接大法兰，连接大法兰与船体的封舱法兰弹性连接；所述罐颈顶部的周边布置有进出料口，罐颈顶部的中心设置有快速可开式人孔。本实用新型结构简单、巧妙、合理，船用储罐的整体可与船体结构相吻合，可最大限度地利用船上的空间；储罐壁为塑钢复合结构，耐腐蚀性、耐磨性、耐温和耐压性更佳。 | ||||||
| 349 | 一种微型耐压仓动力舱壳体固定电镀装置 | CN202223096857.7 | 2022-11-22 | CN219195185U | 2023-06-16 | 吴斌; 史振平 |
| 本实用新型公开了一种微型耐压仓动力舱壳体固定电镀装置，包括底板，所述底板的上表面通过螺栓固定连接有安装架，所述安装架的一端螺纹连接有螺纹杆，所述螺纹杆的一端安装有顶盖密封装置，所述底板的顶部通过螺栓固定连接有电镀筒，所述顶盖密封装置包括顶盖、夹紧块和夹紧螺栓，所述螺纹杆的一端活动连接有顶盖。本实用新型在使用时，将底盖插入密封件的底部，转动固定螺栓，将移动块向上移动，移动块与转动块接触，推动转动块转动，转动块抵住密封件的内壁，防止底盖脱落，将顶盖卡接在密封件的顶部，转动夹紧螺栓，使得夹紧块将密封件夹紧，形成密封件内部密封的效果，防止电镀液进入内部，只对密封件的外部进行电镀。 | ||||||
| 350 | 水密耐压小舱口盖 | CN202021030462.5 | 2020-06-08 | CN212654491U | 2021-03-05 | 王飞升 |
| 本实用新型公开了一种水密耐压小舱口盖。包括围板、盖板、轮轴、手轮、挡块、锁杆、安全支撑杆、支撑板、铰链、弹簧、支撑轴；轮轴设置在盖板上，轮轴下端延伸至封闭结构内部，轮轴两端分别设置有手轮，轮轴上设置有锁杆，锁杆位于封闭结构内部，锁杆位置对应围板内壁上设置有挡块，挡块底面与锁杆顶面接触；所述盖板一侧与围板通过铰链连接，铰链间设置有支撑轴，支撑轴上套装有弹簧，弹簧顶置在铰链间；所述支撑板一端可转动地设置在围板一侧，所述安全支撑杆一端设置在盖板一侧，安全支撑杆、铰链位于同一侧，安全支撑杆与支撑板相互垂直设置，支撑板上设置有固定槽，固定槽包括横槽、弧形槽，安全支撑杆一端设置在固定槽中。 | ||||||
| 351 | 一种爆破试验机 | CN202020394036.3 | 2020-03-25 | CN211697297U | 2020-10-16 | 陈子山; 付志兴; 付明义 |
| 本实用新型涉及管材耐压试验的技术领域，特别是涉及一种爆破试验机；其可同时进行管材的对比试验，收集不同温度环境下管材的爆破极限温度和压力，便于管材的安装和拆卸，缩短试验时间；包括试验舱本体和加压泵；还包括第一间隔竖板、第二间隔竖板、第三间隔竖板、间隔横板、三组夹持机构、进水管和回水管，三组夹持机构均包括两组支撑柱、第一安装板、第二安装板、两组伸缩杆、气压缸、两组第一连通软管和两组第二连通软管，两组伸缩杆的伸长端均套设有拉簧，气压缸的输出端设置有L型板，第一安装板的后端设置有两组第一密封塞，第二安装板的前端设置有两组第二密封塞，第一腔室、第二腔室和第三腔室内底壁上均设置有电热管。 | ||||||
| 352 | 一种船舶上层建筑隔音舱板 | CN201821631179.0 | 2018-10-09 | CN209096930U | 2019-07-12 | 朱锦洪; 邹建新 |
| 本实用新型涉及船舶的技术领域,更具体地说，它涉及一种船舶上层建筑隔音舱板，由若干本体拼接组合构成，本体包括依次叠合的上隔板、夹层板及下隔板，夹层板和上隔板之间构成有第一容纳槽，夹层板和下隔板之间构成有第二容纳槽，第一容纳槽和第二容纳槽内均填充有消音块，消音块上开设有若干消音孔，消音孔呈蜂窝状排布，消音孔的内壁上排布有凸粒，所述夹层板包括相互抵触的上夹板及下夹板，上夹板的下端面均布有若干上凸球，相邻两根上凸球之间构成有活动间隙，下夹板的上端面均布有若干下凸球，下凸球伸入活动间隙内和上凸球挤压，本实用新型结构合理简单，实用性强，耐压能力强，抗压、抗扭能力强，隔音效果好。 | ||||||
| 353 | Pressure bulkhead system | US15590699 | 2017-05-09 | US20170327199A1 | 2017-11-16 | Karim GRASE; Marc SCHIMMLER; Wolfgang EILKEN; Memis TIRYAKI |
| A pressure bulkhead system comprises a pressure bulkhead adapted to be connected to a fuselage of a vehicle to separate a pressurized cabin space of the vehicle from an unpressurized cabin space of the vehicle, and a peripheral pressure frame to sealingly connect the pressure bulkhead to the vehicle fuselage. The peripheral pressure frame comprises an attachment section sealingly attached to an outer rim portion of a first surface of the pressure bulkhead. The first surface, when the pressure bulkhead system is installed in the vehicle, faces the unpressurized cabin space of the vehicle. A flange section is adapted to be sealingly attached to an inner surface of the vehicle fuselage and extends in a direction facing away from the first surface of the pressure bulkhead. A flexible section interconnects the attachment section and the flange section and is flexible to accommodate cabin pressure acting on the pressure bulkhead. | ||||||
| 354 | Aircraft rear structure | US14983468 | 2015-12-29 | US09896181B2 | 2018-02-20 | Esteban Martino Gonzalez; Diego Folch Cortes; Pablo Goya Abaurrea; Sandra Linares Mendoza |
| An aircraft rear structure that comprises a rear pressure bulkhead, and a lifting surface located at both sides of the fuselage of the aircraft. The lifting surface comprises spars extending in the longitudinal direction of the lifting surface. The pressure bulkhead is aligned with one of the spars of the lifting surface. | ||||||
| 355 | DOSENVERSCHLUSS, INSBESONDERE FÜR EINE MILCHDOSE | PCT/EP2015/002005 | 2015-10-12 | WO2016119799A1 | 2016-08-04 | ZÖLLER, Rolf |
Die Erfindung betrifft einen Dosenverschluss (1) zum Einsetzen in einen Dosendeckel (2) einer Dose, insbesondere einer Milchdose, die bei einer Sterilisierung des Doseninhalts erwärmt wird, mit einer Ausgießöffnung (10) zum Ausgießen von Flüssigkeit aus der Dose, und einem Originalitätssicherungselement (12), das die Ausgießöffnung (10) im Originalzustand verschließt und zum Ausgießen aufgebrochen werden kann, um die Ausgießöffnung (10) freizugeben. Die Erfindung sieht zusätzlich ein Druckschott (14) vor, das die Ausgießöffnung (10) an der Innenseite des Originalitätssicherungselements (12) verschließt und den Doseninnendruck dadurch von dem Originalitätssicherungselement (12) fernhält, wobei das Druckschott (14) zum Ausgießen aufgebrochen werden kann, um die Ausgießöffnung (10) freizugeben. |
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| 356 | PRESSURIZED BULKHEAD | US15185159 | 2016-06-17 | US20170361915A1 | 2017-12-21 | Kyle L. McNamara; Edward Frederick Lauser, JR.; David William Bowen; Kevin Andrew Crow; Michael Stephen Niezgoda |
| A pressure bulkhead for an aircraft includes a wall assembly. The wall assembly includes a first wall section which extends in a direction nonparallel to a length of the aircraft. The wall assembly further includes a second wall section secured to the first wall section wherein the second wall section includes a curved shape. The curved shape includes a convex portion which extends further along the length of the aircraft in a direction toward the aft end of the aircraft than the first wall section. A method for assembling a pressure bulkhead is also provided. | ||||||
| 357 | INTEGRALLY STIFFENED AXIAL LOAD CARRYING SKIN PANELS FOR PRIMARY AIRCRAFT STRUCTURE AND CLOSED LOOP MANUFACTURING METHODS FOR MAKING THE SAME | PCT/US2003/021865 | 2003-07-09 | WO2004039670A2 | 2004-05-13 | McCOSKEY, William, R.; HARTSOCK, Kenneth, A.; NYKREIM, Theodore, P. |
A skin panel is provided that includes an axial load carrying skin and at least one stiffener integrally engaged with the axial load carrying skin. The stiffener includes at least one of a stringer, a frame outer chord, and a flange disposed at about an edge of the skin panel. The skin and the at least one stiffener are integrally formed as a single component structure. Accordingly, the invention provides integrally stiffened axial load carrying skin panels suitable for use in any of a wide range of aircraft structures that employ axial load carrying skins, such as fuselages, wings, empennages, pressure bulkheads, wing carry through sections, escape hatches, passenger doors, cargo doors, and access hatches and panels, among others. |
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| 358 | PRESSURE BULKHEAD | US15381747 | 2016-12-16 | US20170174308A1 | 2017-06-22 | Carlos GARCÍA NIETO; Francisco José CRUZ DOMÍNGUEZ; Juan Pablo JUSTE MENCÍA; Nuria COLMENAREJO MATELLANO; Alejandro MARTÍNEZ CAÑIZARES |
| A pressure bulkhead for an aircraft comprising a pressurized zone, the pressure bulkhead made of a composite material and comprising a front panel intended to be faced towards the pressurized zone; and a rear panel, substantially parallel to the front panel and intended to be located farther from the pressurized zone than the front panel. The pressure bulkhead further comprises a plurality of longerons located between the front panel and the rear panel, each one of them being attached to the front panel and to the rear panel; and a plurality of stiffeners, some of them being attached to the front panel and a remainder of them being attached to the rear panel. | ||||||
| 359 | METHOD FOR INSTALLING A DOME-SHAPED PRESSURE BULKHEAD IN A REAR SECTION OF AN AIRCRAFT, AND DEVICE FOR CARRYING OUT THE METHOD | PCT/EP2009057812 | 2009-06-23 | WO2010003818A3 | 2010-05-14 | WEBER FRANK; SCHOENFELDT OLAF |
| The invention relates to a method for installing an especially dome-shaped pressure bulkhead 5,25 on a one-piece, substantially conical rear section 1,13,18 of an aircraft, wherein said rear section comprises a connection area 3,35 and an end area 9, comprising the steps: a) horizontally accommodating a prefabricated rear section 1,13,18 in a horizontal support 12, b) inserting the rear section 1,13,18 into a pivoting frame 17, c) pivoting the rear section 1,13,18 into a vertical position using the pivoting frame 17, wherein the connection area 3,35 of the rear section 1,13,18 points upward, d) horizontally placing and centering the pressure bulkhead 5,25 on the connection area 3,35, and e) joining of the pressure bulkhead 5,25 with the rear section 1,13,18 in the area of the connection area 3,35. Because the rear section 1,13,18 is in a vertical position during the installation of the pressure bulkhead, the pressure bulkhead 5,25 to be integrated can be oriented in a horizontal position in relation to a connection area 3,35 of the rear section 1,13,18, positioned, and joined with the connection area 3,35 using a preferably combined drilling and riveting device 19 with a gantry design. The invention further relates to an apparatus 10 for carrying out the method using a pivoting frame 17 for tilting the rear section 1,13,18 into a vertical position for installing the pressure bulkhead 5,25. | ||||||
| 360 | PRESSURIZED BULKHEAD | EP17159578.8 | 2017-03-07 | EP3257742A1 | 2017-12-20 | McNamara, Kyle L.; LAUSER, Edward Frederick; BOWEN, David William; CROW, Kevin Andrew; NIEZGODA, Michael Stephen |
A pressure bulkhead for an aircraft includes a wall assembly 22. The wall assembly includes a first wall section 24 which extends in a direction nonparallel to a length of the aircraft. The wall assembly further includes a second wall section 26 secured to the first wall section wherein the second wall section includes a curved shape 32. The curved shape includes a convex portion 34 which extends further along the length of the aircraft in a direction toward the aft end of the aircraft than the first wall section. A method for assembling a pressure bulkhead is also provided.
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