ES2102246T3 - Sistema cortador de alambre con carenado aerodinamico que absorbe energia de microondas. - Google Patents
Sistema cortador de alambre con carenado aerodinamico que absorbe energia de microondas.Info
- Publication number
- ES2102246T3 ES2102246T3 ES94926510T ES94926510T ES2102246T3 ES 2102246 T3 ES2102246 T3 ES 2102246T3 ES 94926510 T ES94926510 T ES 94926510T ES 94926510 T ES94926510 T ES 94926510T ES 2102246 T3 ES2102246 T3 ES 2102246T3
- Authority
- ES
- Spain
- Prior art keywords
- wire
- fuseled
- cutter
- cable
- microwave energy
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000010521 absorption reaction Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Elimination Of Static Electricity (AREA)
- Details Of Aerials (AREA)
- Lasers (AREA)
Abstract
SE PROPORCIONA UNA ESTRUCTURA FUSELADA (122) PARA CUBRIR UN GOLPE DE CORTAALAMBRES (120). LA ESTRUCTURA FUSELADA (122) COMPRENDE UN NUCLEO DE ABSORCION DE ENERGIA DE MICROONDAS (150) CUBIERTO POR UNA CAPA DIELECTRICA (160, 161, 165, 166). LA ESTRUCTURA FUSELADA (122) REDUCE LA SEÑAL DE RADAR DEL CORTAALAMBRES Y FRACTURA, EN RESPUESTA A UN GOLPE DE ALAMBRE PARA PERMITIR QUE EL CORTADOR CAPTURE Y CORTE UN ALAMBRE/CABLE. AL MENOS UNA PROYECCION (135) ES FORMADA EN LA ESTRUCTURA FUSELADA (122) PARA COGER UNA FLOJEDAD DEL ALAMBRE/CABLE MIENTRAS DESLIZA LA ESTRUCTURA FUSELADA, LA PROYECCION MANTIENE EL ALAMBRE/CABLE HASTA QUE SE DESARROLLE TENSION PARA FRACTURAR LA ESTRUCTURA FUSELADA, PERMITIENDO ASI QUE EL ALAMBRE/CABLE PASE A TRAVES DEL CORTAALAMBRES DONDE ES POSTERIORMENTE CORTADO. LA ESTRUCTURA FUSELADA (122) REDUCE LA RESISTENCIA AL AVANCE Y MEJORA LAS CARACTERISTICAS AERODINAMICAS DEL AVION DIRIGIENDO EL FLUJO DE AIRE ALREDEDOR DEL CORTAALAMBRES Y DEL EQUIPO JUNTO AL CORTAALAMBRES.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/118,551 US5415364A (en) | 1993-09-09 | 1993-09-09 | Wire cutter system having aerodynamic, microwave energy absorbing fairing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2102246T3 true ES2102246T3 (es) | 1997-07-16 |
Family
ID=22379308
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES94926510T Expired - Lifetime ES2102246T3 (es) | 1993-09-09 | 1994-08-16 | Sistema cortador de alambre con carenado aerodinamico que absorbe energia de microondas. |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US5415364A (es) |
| EP (1) | EP0717697B1 (es) |
| JP (1) | JPH09504492A (es) |
| CN (1) | CN1060731C (es) |
| AU (1) | AU674254B2 (es) |
| CA (1) | CA2168550A1 (es) |
| DE (1) | DE69402328T2 (es) |
| ES (1) | ES2102246T3 (es) |
| IL (1) | IL110741A (es) |
| WO (1) | WO1995007214A1 (es) |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5250950A (en) * | 1979-02-13 | 1993-10-05 | Lockheed Corporation | Vehicle |
| US7284726B2 (en) * | 2004-02-17 | 2007-10-23 | Sikorsky Aircraft Corporation | Self extinguishing composite primary structure |
| NZ537472A (en) * | 2004-12-23 | 2006-07-28 | Arcit Ltd | Wire-strike system |
| US7621480B2 (en) * | 2005-05-26 | 2009-11-24 | Sikorsky Aircraft Corporation | De-rotation system for a counter-rotating, coaxial rotor hub shaft fairing |
| US7607607B2 (en) * | 2005-05-26 | 2009-10-27 | Sikorsky Aircraft Corporation | De-rotation system suitable for use with a shaft fairing system |
| US7229251B2 (en) * | 2005-05-31 | 2007-06-12 | Sikorsky Aircraft Corporation | Rotor hub fairing system for a counter-rotating, coaxial rotor system |
| EP2227641B1 (en) * | 2007-12-03 | 2016-07-20 | Sikorsky Aircraft Corporation | Magnetic de-rotation system for a shaft fairing system |
| EP2238018A2 (en) | 2008-01-02 | 2010-10-13 | Sikorsky Aircraft Corporation | Planetary de-rotation system for a shaft fairing system |
| CN102390540A (zh) * | 2011-09-08 | 2012-03-28 | 上海航空机械有限公司 | 用于直升机上的防线缆保护装置 |
| FR2981512B1 (fr) | 2011-10-12 | 2013-11-29 | Eurocopter France | Antenne d'aeronef, et aeronef |
| GB2514090A (en) * | 2013-03-18 | 2014-11-19 | Smith Tech Dev H R | Cable cutter antenna for aircraft |
| US20150122941A1 (en) * | 2013-11-06 | 2015-05-07 | Sikorsky Aircraft Corporation | Counter-rotating rotor system with fairing |
| US9725165B2 (en) * | 2014-10-03 | 2017-08-08 | Bell Helicopter Textron Inc. | Cable cutter system |
| US10675026B2 (en) | 2016-12-21 | 2020-06-09 | Ethicon Llc | Methods of stapling tissue |
| CN108724187B (zh) * | 2018-06-13 | 2021-04-23 | 中国科学技术大学 | 一种机器人抓取飞行物体的运动规划方法及系统 |
| CN109204771A (zh) * | 2018-08-06 | 2019-01-15 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机雷达舱设备安装架 |
| EP3677500B1 (en) * | 2019-01-03 | 2025-03-05 | Textron Innovations Inc. | Modular windshield |
| USD896730S1 (en) * | 2019-09-27 | 2020-09-22 | Bell Textron Inc. | Combined aircraft fuselage and empennage |
| USD894814S1 (en) * | 2019-09-27 | 2020-09-01 | Bell Textron Inc. | Aircraft |
| US11234698B2 (en) | 2019-12-19 | 2022-02-01 | Cilag Gmbh International | Stapling system comprising a clamp lockout and a firing lockout |
| TR2022005071A2 (tr) * | 2022-03-31 | 2023-10-23 | Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi | Kablo kesici sistem. |
| USD1082960S1 (en) * | 2022-11-11 | 2025-07-08 | Guangdong Yangbang Science and Technology Industry Co., Ltd. | Shape-transforming toy |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4924228A (en) * | 1963-07-17 | 1990-05-08 | Boeing Company | Aircraft construction |
| CA1079182A (en) * | 1978-12-07 | 1980-06-10 | Nelson Chan | Cable-cutting device |
| GB2075940B (en) * | 1980-04-22 | 1983-11-16 | Secr Defence | Cable cutting device |
| US4407467A (en) * | 1981-08-24 | 1983-10-04 | Hughes Helicopters, Inc. | Tactical wire-cutter system for helicopters |
| US4726980A (en) * | 1986-03-18 | 1988-02-23 | Nippon Carbon Co., Ltd. | Electromagnetic wave absorbers of silicon carbide fibers |
| US4826103A (en) * | 1987-04-28 | 1989-05-02 | Custom Air, Inc. | Active cable-cutting assembly for aircraft |
| US5288036A (en) * | 1992-10-29 | 1994-02-22 | United Technologies Corporation | Pivoting wire deflection and severing system |
-
1993
- 1993-09-09 US US08/118,551 patent/US5415364A/en not_active Expired - Lifetime
-
1994
- 1994-08-16 DE DE69402328T patent/DE69402328T2/de not_active Expired - Fee Related
- 1994-08-16 ES ES94926510T patent/ES2102246T3/es not_active Expired - Lifetime
- 1994-08-16 JP JP7508675A patent/JPH09504492A/ja not_active Ceased
- 1994-08-16 AU AU76325/94A patent/AU674254B2/en not_active Ceased
- 1994-08-16 WO PCT/US1994/009241 patent/WO1995007214A1/en not_active Ceased
- 1994-08-16 CN CN94193311A patent/CN1060731C/zh not_active Expired - Fee Related
- 1994-08-16 EP EP94926510A patent/EP0717697B1/en not_active Expired - Lifetime
- 1994-08-16 CA CA002168550A patent/CA2168550A1/en not_active Abandoned
- 1994-08-22 IL IL110741A patent/IL110741A/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| DE69402328D1 (de) | 1997-04-30 |
| CN1130369A (zh) | 1996-09-04 |
| US5415364A (en) | 1995-05-16 |
| DE69402328T2 (de) | 1997-07-03 |
| AU674254B2 (en) | 1996-12-12 |
| IL110741A (en) | 1998-03-10 |
| AU7632594A (en) | 1995-03-27 |
| CA2168550A1 (en) | 1995-03-16 |
| EP0717697B1 (en) | 1997-03-26 |
| IL110741A0 (en) | 1994-11-11 |
| JPH09504492A (ja) | 1997-05-06 |
| WO1995007214A1 (en) | 1995-03-16 |
| EP0717697A1 (en) | 1996-06-26 |
| CN1060731C (zh) | 2001-01-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
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