首页> 外国专利> PNEUMATIC DEVICE FOR RAPIDLY REACTIVATING A TURBINE ENGINE, ARCHITECTURE FOR A PROPULSION SYSTEM OF A MULTI-ENGINE HELICOPTER PROVIDED WITH SUCH A DEVICE, AND CORRESPONDING HELICOPTER

PNEUMATIC DEVICE FOR RAPIDLY REACTIVATING A TURBINE ENGINE, ARCHITECTURE FOR A PROPULSION SYSTEM OF A MULTI-ENGINE HELICOPTER PROVIDED WITH SUCH A DEVICE, AND CORRESPONDING HELICOPTER

机译：用于快速重新启动涡轮发动机的气动装置，具有这种装置的多引擎直升机推进系统的架构以及相应的直升机

页面导航

摘要
著录项
相似文献

摘要

The invention relates to a device for the rapid reactivation of a helicopter turbine engine (6), characterised in that it comprises a pneumatic turbine (7) mechanically connected to said turbine engine (6) so as to be able to rotate it and ensure reactivation thereof; a pneumatic storage (9) connected to said pneumatic turbine (7) by means of a pneumatic circuit (10) for supplying pressurised gas to said pneumatic turbine (7); a controlled fast-opening pneumatic valve (11) arranged on the pneumatic circuit (10) between said storage (9) and said pneumatic turbine (7) and suitable for being on demand placed at least in an open position in which the gas can supply said pneumatic turbine (7), or in a closed position in which said pneumatic turbine (7) is no longer supplied with pressurised gas.

机译：本发明涉及一种用于快速重启直升机涡轮发动机（ 6 ）的装置，其特征在于，该装置包括机械地连接至所述涡轮发动机的气动涡轮（ 7 ）。（ 6 ）以便能够旋转并确保其重新激活;借助于空气回路（ 10 ）连接到所述气动涡轮（ 7 ）的气动存储器（ 9 ），用于向所述气动涡轮（ 7 ）供应压缩气体气动涡轮（ 7 ）;受控的快开式气动阀（ 11 ）布置在所述存储装置（ 9 ）和所述气动涡轮机（ 9 ）之间的气动回路（ 10 ）上 7 ），并且适合于按需放置在至少一个可以为所述气动涡轮机供气的打开位置（ 7 ），或者在一个需要关闭的位置不再向气动涡轮（ 7 ）提供加压气体。 展开▼

著录项

公开/公告号US2017211483A1

专利类型

公开/公告日2017-07-27

原文格式PDF

申请/专利权人 SAFRAN HELICOPTER ENGINES;
展开▼

申请/专利号US201515327631

发明设计人 ROMAIN THIRIET;CAMEL SERGHINE;FREDERIC MOULON;
展开▼

申请日2015-07-21

分类号F02C7/277;B64C27/06;B64D31/06;B64D35/08;F01D19;B64D27/10;

国家 US

入库时间 2022-08-21 13:51:19

相似文献

专利

外文文献

中文文献

1. 用于涡轮发动机的快速重新运转的气动装置，用于设置有这种装置的多发动机直升机的推进系统的架构，以及相应的直升机 [P] . 中国专利： CN106574515A . 2017-04-19

2. 用于重启涡轮轴发动机的可移除组合件，设有这种组合件的多引擎直升机的推进系统的架构和相应的直升机 [P] . 中国专利： CN107074355B . 2020.09.04

3. PNEUMATIC DEVICE FOR RAPIDLY REACTIVATING A TURBINE ENGINE, ARCHITECTURE FOR A PROPULSION SYSTEM OF A MULTI-ENGINE HELICOPTER PROVIDED WITH SUCH A DEVICE, CORRESPONDING HELICOPTER AND METHOD [P] . PL3175090T3 . 2019-09-30

机译：用于快速重新启动涡轮发动机的气动装置，具有这种装置的多发动机直升机的推进系统的体系结构，相应的直升机和方法

4. PNEUMATIC DEVICE FOR RAPIDLY REACTIVATING A TURBINE ENGINE ARCHITECTURE FOR A PROPULSION SYSTEM OF A MULTI-ENGINE HELICOPTER PROVIDED WITH SUCH A DEVICE AND CORRESPONDING HELICOPTER [P] . 韩国专利： KR20170031703A . 2017-03-21

机译：快速激活涡轮发动机结构的气动设备，该多引擎直升机具有这样的设备和相应的直升机

5. PNEUMATIC DEVICE FOR RAPIDLY REACTIVATING A TURBINE ENGINE, ARCHITECTURE FOR A PROPULSION SYSTEM OF A MULTI-ENGINE HELICOPTER PROVIDED WITH SUCH A DEVICE, AND CORRESPONDING HELICOPTER [P] . 欧洲知识产权局专利： EP3175090A1 . 2017-06-07

机译：用于快速重新启动涡轮发动机的气动装置，具有这种装置的多引擎直升机推进系统的架构以及相应的直升机

1. A new design of foaming agent mixing device for a pneumatic foaming system used for mine dust suppression [J] . Wang Deming, Lu Xinxiao, Wang Hetang, 矿业科学技术（英文版） . 2016,第002期

2. A new design of foaming agent mixing device for a pneumatic foaming system used for mine dust suppression [J] . Wang, Deming, Lu, 矿业科学技术学报：英文版 . 2016,第002期

3. Features of Load and Wear of Main Propulsion Devices on Sea-Going Ships with Piston Combustion Engines and Their Impact on Changes in Technical States of the Systems [J] . Jerzy GirtlerGda?sk University of Technology 11/12 Narutowicza St. 80 - 233 Gda?sk PolandOther articles by this author:De Gruyter OnlineGoogle Scholar Polish maritime research . 2018,第4期

4. FEATURES OF LOAD AND WEAR OF MAIN PROPULSION DEVICES ON SEAGOING SHIPS WITH PISTON COMBUSTION ENGINES AND THEIR IMPACT ON CHANGES IN TECHNICAL STATES OF THE SYSTEMS [J] . Girtler Jerzy Polish Maritime Research . 2017,第4期

5. Active expert systems at the complex diagnosis and control of hydromechanical devices of gas-turbine engines [J] . Zhernakov S. V. Автоматизация и современные технологии . 2001,第9期

6. Optimization of balanced field length performance of multi-engine helicopters [C] . Visser, H. G. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, Portland, OR, Aug. 9-11, 1999, Collection of Technical Papers (A99-36864 09-08), Reston, VA, American Institute of Aeronautics and Astronautics, 1999 . 1999

7. Semi-active control of helicopter vibration using controllable stiffness and damping devices. [D] . Anusonti-Inthra, Phuriwat. 2002

8. Mechanical chest compression devices in the helicopter emergency medical service in Switzerland [O] . Urs Pietsch, David Reiser, Volker Wenzel, 2020

9. Mechanical Chest Compression Devices in the Helicopter Emergency Medical Service in Switzerland [O] . Urs Pietsch, David Reiser, Volker Wenzel, 2020

1. Smart Service System(SSS)：A Novel Architecture Enabling Coordination of Heterogeneous Networking Technologies and Devices for Internet of Things [J] . yongan guo ,hongbo zhu ,longxiang yang . 中国通信：英文版 . 2017,第3期

2. Gas-Solid Flow Behavior in a Pneumatic Conveying System for Drying Applications: Coarse Particles Feeding with a Venturi Device [J] . Thiago Faggion de Pádua ,Rodrigo Béttega ,José Teixeira Freire . 化学工程与科学期刊（英文） . 2015,第3期

3. Novel concept of endoscopic device delivery station system for rapid and tight attachment of polyglycolic acid sheet [J] . Hirohito Mori ,Hideki Kobara ,Noriko Nishiyama . 世界胃肠病学杂志：英文版 . 2018,第2期

4. 武装直升机武器系统综显模拟训练装置设计与仿真 [C] . 杨乐 ,王天玉 ,任渊博 . 第二十九届全国直升机年会 . 2013

5. 直升机起落装置的快速设计方法研究 [A] . 林辉 . 2013