WO2011138566A1 - Dispositif de deverrouillage declenche, reliant deux sous-ensembles detachables - Google Patents
Dispositif de deverrouillage declenche, reliant deux sous-ensembles detachables Download PDFInfo
- Publication number
- WO2011138566A1 WO2011138566A1 PCT/FR2011/051026 FR2011051026W WO2011138566A1 WO 2011138566 A1 WO2011138566 A1 WO 2011138566A1 FR 2011051026 W FR2011051026 W FR 2011051026W WO 2011138566 A1 WO2011138566 A1 WO 2011138566A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- chamber
- release sleeve
- bore
- sleeve
- release
- Prior art date
Links
- 238000013016 damping Methods 0.000 claims abstract description 28
- 239000007789 gas Substances 0.000 claims description 29
- 238000006073 displacement reaction Methods 0.000 claims description 6
- 230000009467 reduction Effects 0.000 claims description 3
- 230000009471 action Effects 0.000 abstract description 4
- 238000000926 separation method Methods 0.000 description 5
- 230000035939 shock Effects 0.000 description 5
- 238000000429 assembly Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
- B64G1/6455—Pyrotechnics; Using heat
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B31/00—Screwed connections specially modified in view of tensile load; Break-bolts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B31/00—Screwed connections specially modified in view of tensile load; Break-bolts
- F16B31/005—Breakbolts loosening due to the action of an explosive charge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/08—Quickly-detachable or mountable nuts, e.g. consisting of two or more parts; Nuts movable along the bolt after tilting the nut
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/08—Quickly-detachable or mountable nuts, e.g. consisting of two or more parts; Nuts movable along the bolt after tilting the nut
- F16B37/0807—Nuts engaged from the end of the bolt, e.g. axially slidable nuts
Definitions
- FR 2 807 123 discloses a device of the type indicated above which essentially comprises a gas generator, a body in which is defined an expansion chamber of the gases emitted by the gas generator, a segmented nut arranged at the inside of a movable release sleeve in said body and a connecting screw of which a threaded portion is engaged in the nut.
- the two subassemblies to be separated are assembled between the body and the screw head.
- the release sleeve comprises an extension forming a duct opening into the damping chamber and slidably engaged in a bore of a wall of said body separating said expansion chamber from said drive chamber.
- the pusher comprises a shutter protruding into said damping chamber and shaped and dimensioned to engage and close said conduit of said release sleeve, at the end of the race of the latter.
- This option may apply if the depreciation is too great or the engine power, as defined, would be too low.
- the release sleeve 40 bears on an internal shoulder 56 of the median portion of the body, under the action of the spring 49.
- this drive chamber 64 has an annular portion 72 defined by a shoulder of the body 14, extending by widening the bore of the body in which slides said release sleeve.
- the calibrated passages 70 are spaced along the side wall of this sleeve. These calibrated passages 70, parallel, are spaced in the axial direction of the release sleeve so that they are closed successively as the displacement of the release sleeve, to allow a reduction of the gas passage section between the damping chamber 66 and the driving chamber 64, as and when this displacement.
- the extension forming a duct 75 defined at the end of the release sleeve is engaged in the wall 77 delimiting the gas expansion chamber; This is the situation illustrated in FIG. 2.
- the gases enter the damping chamber 66 and pass through the calibrated orifices 70 in order to act on the end face of the release sleeve 40. gas does not result in a sudden displacement of the release sleeve due to the restrictions of gas flow through the calibrated passages 70.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air Bags (AREA)
- Fluid-Damping Devices (AREA)
- Automotive Seat Belt Assembly (AREA)
- Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
- Safety Valves (AREA)
Abstract
Description
Claims
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2012150162/11A RU2012150162A (ru) | 2010-05-07 | 2011-05-05 | Устройство расцепления, соединяющее два отделяемых сборочных узла |
US13/696,754 US20130101369A1 (en) | 2010-05-07 | 2011-05-05 | Tripped unlocking device, connecting two detachable subassemblies |
BR112012028364A BR112012028364A2 (pt) | 2010-05-07 | 2011-05-05 | dispositivo de desbloqueio acionado. |
EP11723577.0A EP2566758B1 (fr) | 2010-05-07 | 2011-05-05 | Dispositif de deverrouillage declenche, reliant deux sous-ensembles detachables |
KR1020127032048A KR20140016134A (ko) | 2010-05-07 | 2011-05-05 | 2개의 분리가능한 하위조립체를 연결하는 방아쇠식 잠금해제 장치 |
CA2798037A CA2798037A1 (fr) | 2010-05-07 | 2011-05-05 | Tripped unlocking device, connecting two detachable subassemblies |
ES11723577.0T ES2472460T3 (es) | 2010-05-07 | 2011-05-05 | Dispositivo de conexión separable, que conecta dos subconjuntos ensamblados |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1053609A FR2959787B1 (fr) | 2010-05-07 | 2010-05-07 | Dispositif de deverrouillage declenche, reliant deux sous-ensembles detachables |
FR1053609 | 2010-05-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2011138566A1 true WO2011138566A1 (fr) | 2011-11-10 |
Family
ID=43334603
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2011/051026 WO2011138566A1 (fr) | 2010-05-07 | 2011-05-05 | Dispositif de deverrouillage declenche, reliant deux sous-ensembles detachables |
Country Status (9)
Country | Link |
---|---|
US (1) | US20130101369A1 (fr) |
EP (1) | EP2566758B1 (fr) |
KR (1) | KR20140016134A (fr) |
BR (1) | BR112012028364A2 (fr) |
CA (1) | CA2798037A1 (fr) |
ES (1) | ES2472460T3 (fr) |
FR (1) | FR2959787B1 (fr) |
RU (1) | RU2012150162A (fr) |
WO (1) | WO2011138566A1 (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012018600A1 (de) * | 2012-09-20 | 2014-03-20 | Audi Ag | Drehgelenk für eine Fahrzeugtür und korrespondierende Fahrzeugtür |
CN104781564A (zh) * | 2012-11-13 | 2015-07-15 | 奥托立夫开发公司 | 主动式螺栓松脱装置 |
CN105416615A (zh) * | 2015-11-12 | 2016-03-23 | 哈尔滨工业大学 | 一种微小卫星分离装置 |
GB2587360A (en) * | 2019-09-24 | 2021-03-31 | Martin Baker Aircraft Co Ltd | A linkage |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101583660B1 (ko) * | 2014-05-27 | 2016-01-19 | 한국항공우주연구원 | 파이로 고정분리장치 |
CN104859870B (zh) * | 2014-10-09 | 2017-02-08 | 航天东方红卫星有限公司 | 一种一体化设计的星箭分离机构 |
CN105253331B (zh) * | 2015-09-10 | 2017-07-07 | 北京空间飞行器总体设计部 | 一种力限式压紧释放机构 |
CN106184826B (zh) * | 2016-07-11 | 2018-10-23 | 上海宇航系统工程研究所 | 星箭弹簧分离装置 |
FR3056967B1 (fr) | 2016-10-03 | 2019-06-14 | Arianegroup Sas | Dispositif de liaison ponctuelle provisoire |
EP3676180B1 (fr) * | 2017-09-01 | 2022-11-02 | RUAG Space AB | Dispositif de séparation pour engin spatial et procédé de séparation |
EP3728045B1 (fr) | 2017-12-21 | 2024-04-17 | Beyond Gravity Sweden AB | Dispositif de séparation |
FR3081945B1 (fr) * | 2018-05-31 | 2020-09-18 | Arianegroup Sas | Systeme de separation¨ponctuel electromecanique |
CN109050988A (zh) * | 2018-08-29 | 2018-12-21 | 上海宇航系统工程研究所 | 一种分离螺母连接解锁装置 |
CN110949693B (zh) * | 2019-12-13 | 2021-07-30 | 航天科工火箭技术有限公司 | 一种气动式连接解锁装置 |
US11964781B2 (en) * | 2020-01-15 | 2024-04-23 | Aerospace Propulsion Products B.V. | Coupling unit for detachable coupling parts of a spacecraft |
KR102619334B1 (ko) | 2021-09-17 | 2024-01-02 | 국방과학연구소 | 파이로 분리장치의 볼트 분리유닛 |
CN114046286B (zh) * | 2021-11-10 | 2023-10-20 | 湖北三江航天红阳机电有限公司 | 一种冷气解锁作动器及其使用方法 |
CN114056606A (zh) * | 2021-12-01 | 2022-02-18 | 沈阳航天新光集团有限公司 | 非火工熔断式双向连接分离装置 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4187759A (en) * | 1977-09-16 | 1980-02-12 | The United States Of America As Represented By The Secretary Of The Navy | Separation nut system |
EP0296936A1 (fr) * | 1987-06-16 | 1988-12-28 | AEROSPATIALE Société Nationale Industrielle | Mécanisme de commande d'écartement rapide et contrôle de deux pièces en contact |
FR2807123A1 (fr) | 2000-03-29 | 2001-10-05 | Pyroalliance | Ecrou de separation rearmable a faible niveau de choc induit |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3071404A (en) * | 1960-12-08 | 1963-01-01 | Austin G Van Hove | Explosively releasable fastener |
FR2637252B1 (fr) * | 1988-10-05 | 1990-12-28 | Aerospatiale | Dispositif de solidarisation/desolidarisation provisoire de deux elements l'un a l'autre, et de separation ulterieure |
US5160233A (en) * | 1992-05-13 | 1992-11-03 | The United State Of America As Representd By The Administrator Of The National Aeronautics And Space Administration | Fastening apparatus having shape memory alloy actuator |
FR2728230A1 (fr) * | 1994-12-19 | 1996-06-21 | Aerospatiale | Dispositif de liaison deverouillable entre deux objets, utilisable notamment dans l'espace |
FR2736615B1 (fr) * | 1995-07-13 | 1997-09-19 | Aerospatiale | Deverouilleur a ecrou fendu pour microsatellite, a redondance mecanique et pyrotechnique complete |
US6352397B1 (en) * | 2000-05-31 | 2002-03-05 | Hi-Shear Technology Corporation | Reduced shock separation fastener |
WO2004046568A1 (fr) * | 2002-11-19 | 2004-06-03 | Telezygology Inc | Ensemble boulon, procede et dispositif de liberation et systeme informatique |
US6939073B1 (en) * | 2003-08-26 | 2005-09-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Releasable locking mechanisms |
US20100021265A1 (en) * | 2008-07-24 | 2010-01-28 | Brent Parks | Separation fastener with frangible nut |
-
2010
- 2010-05-07 FR FR1053609A patent/FR2959787B1/fr not_active Expired - Fee Related
-
2011
- 2011-05-05 CA CA2798037A patent/CA2798037A1/fr not_active Abandoned
- 2011-05-05 BR BR112012028364A patent/BR112012028364A2/pt not_active IP Right Cessation
- 2011-05-05 ES ES11723577.0T patent/ES2472460T3/es active Active
- 2011-05-05 EP EP11723577.0A patent/EP2566758B1/fr active Active
- 2011-05-05 KR KR1020127032048A patent/KR20140016134A/ko not_active Application Discontinuation
- 2011-05-05 US US13/696,754 patent/US20130101369A1/en not_active Abandoned
- 2011-05-05 WO PCT/FR2011/051026 patent/WO2011138566A1/fr active Application Filing
- 2011-05-05 RU RU2012150162/11A patent/RU2012150162A/ru not_active Application Discontinuation
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4187759A (en) * | 1977-09-16 | 1980-02-12 | The United States Of America As Represented By The Secretary Of The Navy | Separation nut system |
EP0296936A1 (fr) * | 1987-06-16 | 1988-12-28 | AEROSPATIALE Société Nationale Industrielle | Mécanisme de commande d'écartement rapide et contrôle de deux pièces en contact |
FR2807123A1 (fr) | 2000-03-29 | 2001-10-05 | Pyroalliance | Ecrou de separation rearmable a faible niveau de choc induit |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012018600A1 (de) * | 2012-09-20 | 2014-03-20 | Audi Ag | Drehgelenk für eine Fahrzeugtür und korrespondierende Fahrzeugtür |
DE102012018600B4 (de) * | 2012-09-20 | 2015-02-12 | Audi Ag | Drehgelenk mit pyrotechnischer Notentriegelung für eine Fahrzeugtür und korrespondierende Fahrzeugtür |
CN104781564A (zh) * | 2012-11-13 | 2015-07-15 | 奥托立夫开发公司 | 主动式螺栓松脱装置 |
CN105416615A (zh) * | 2015-11-12 | 2016-03-23 | 哈尔滨工业大学 | 一种微小卫星分离装置 |
GB2587360A (en) * | 2019-09-24 | 2021-03-31 | Martin Baker Aircraft Co Ltd | A linkage |
GB2587360B (en) * | 2019-09-24 | 2022-01-19 | Martin Baker Aircraft Co Ltd | A linkage |
Also Published As
Publication number | Publication date |
---|---|
RU2012150162A (ru) | 2014-06-20 |
US20130101369A1 (en) | 2013-04-25 |
ES2472460T3 (es) | 2014-07-01 |
FR2959787B1 (fr) | 2012-06-08 |
FR2959787A1 (fr) | 2011-11-11 |
BR112012028364A2 (pt) | 2017-03-21 |
EP2566758B1 (fr) | 2014-03-19 |
EP2566758A1 (fr) | 2013-03-13 |
CA2798037A1 (fr) | 2011-11-10 |
KR20140016134A (ko) | 2014-02-07 |
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