AU1478401A - Method and apparatus for minimizing the transmission of acoustic vibrations to apayload - Google Patents
Method and apparatus for minimizing the transmission of acoustic vibrations to apayloadInfo
- Publication number
- AU1478401A AU1478401A AU14784/01A AU1478401A AU1478401A AU 1478401 A AU1478401 A AU 1478401A AU 14784/01 A AU14784/01 A AU 14784/01A AU 1478401 A AU1478401 A AU 1478401A AU 1478401 A AU1478401 A AU 1478401A
- Authority
- AU
- Australia
- Prior art keywords
- apayload
- minimizing
- transmission
- acoustic vibrations
- payload
- 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.)
- Abandoned
Links
- 230000005540 biological transmission Effects 0.000 title 1
Classifications
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
-
- 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
- B64G1/228—Damping of high-frequency vibration effects on spacecraft elements, e.g. by using acoustic vibration dampers
-
- 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
- B64G1/6425—Interstage or payload connectors arrangements for damping vibrations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Multimedia (AREA)
- Vibration Prevention Devices (AREA)
- Telephone Set Structure (AREA)
- Piezo-Electric Transducers For Audible Bands (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/438,713 US6371412B1 (en) | 1999-11-11 | 1999-11-11 | Method and apparatus for reducing acoustic coupling |
| US09438713 | 1999-11-11 | ||
| PCT/US2000/030783 WO2001034468A1 (en) | 1999-11-11 | 2000-11-09 | Method and apparatus for minimizing the transmission of acoustic vibrations to a payload |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AU1478401A true AU1478401A (en) | 2001-06-06 |
Family
ID=23741725
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU14784/01A Abandoned AU1478401A (en) | 1999-11-11 | 2000-11-09 | Method and apparatus for minimizing the transmission of acoustic vibrations to apayload |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US6371412B1 (enExample) |
| EP (1) | EP1227977B1 (enExample) |
| JP (1) | JP4722362B2 (enExample) |
| AT (1) | ATE317352T1 (enExample) |
| AU (1) | AU1478401A (enExample) |
| CA (1) | CA2391217A1 (enExample) |
| DE (1) | DE60025941T2 (enExample) |
| WO (1) | WO2001034468A1 (enExample) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6977314B2 (en) | 2001-12-19 | 2005-12-20 | Rohm And Haas Company | Metal-doped sulfonated ion exchange resin catalysts |
| JP5569136B2 (ja) * | 2010-05-12 | 2014-08-13 | 株式会社Ihi | ペイロード保護装置 |
| FR3022995B1 (fr) * | 2014-06-25 | 2017-06-09 | Mbda France | Missile pourvu d'une coiffe de protection separable |
| KR101856191B1 (ko) * | 2016-09-27 | 2018-05-09 | 한국항공우주연구원 | 우주비행체 및 우주비행체의 발사 방법 |
| US10562650B2 (en) * | 2017-06-28 | 2020-02-18 | The Boeing Company | Corrugated payload adaptor structure |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2387708A (en) * | 1944-05-09 | 1945-10-30 | Solar Aircraft Co | Spill for aircraft |
| US4164339A (en) * | 1973-06-06 | 1979-08-14 | Mcclenny Carl O | Environmental protection system |
| US4436036A (en) * | 1979-09-28 | 1984-03-13 | Thiokol Corporation | Projectile for dispensing gaseous material |
| US4849276A (en) * | 1984-02-17 | 1989-07-18 | The Boeing Company | Thermal insulation structure |
| JPS6432999A (en) * | 1987-07-29 | 1989-02-02 | Mitsubishi Electric Corp | Fairing |
| US4817889A (en) * | 1987-08-17 | 1989-04-04 | Henry Richard D | Foolproof simplified vacuum systems |
| JPH04362499A (ja) * | 1991-06-11 | 1992-12-15 | Mitsubishi Heavy Ind Ltd | ロケットの衛星フェアリング |
| US5526692A (en) * | 1993-12-29 | 1996-06-18 | Keiser Corporation | Sensor |
| US5743492A (en) * | 1994-02-18 | 1998-04-28 | Lockheed Martin Corporation | Payload housing and assembly joint for a launch vehicle |
| US5844815A (en) * | 1996-10-08 | 1998-12-01 | Mcdonnell Douglas Corporation | Umbilical and follower assembly utilized in microgravity platform system |
| US5947240A (en) | 1997-02-03 | 1999-09-07 | Honeywell, Inc. | Load vibration isolation apparatus |
| US5961078A (en) * | 1997-06-27 | 1999-10-05 | Mcdonnell Douglas Corporation | Passive axial vibration isolation system for a spacecraft launch vehicle |
| US6042057A (en) * | 1998-03-19 | 2000-03-28 | The Boeing Company | Aerodynamically actuated magnetic ascent vent cover |
| JP3978861B2 (ja) * | 1998-04-22 | 2007-09-19 | 株式会社Ihi | ペイロード緩衝支持機構 |
-
1999
- 1999-11-11 US US09/438,713 patent/US6371412B1/en not_active Expired - Lifetime
-
2000
- 2000-11-09 DE DE60025941T patent/DE60025941T2/de not_active Expired - Lifetime
- 2000-11-09 WO PCT/US2000/030783 patent/WO2001034468A1/en not_active Ceased
- 2000-11-09 JP JP2001536431A patent/JP4722362B2/ja not_active Expired - Fee Related
- 2000-11-09 AT AT00977100T patent/ATE317352T1/de not_active IP Right Cessation
- 2000-11-09 AU AU14784/01A patent/AU1478401A/en not_active Abandoned
- 2000-11-09 CA CA002391217A patent/CA2391217A1/en not_active Abandoned
- 2000-11-09 EP EP00977100A patent/EP1227977B1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JP4722362B2 (ja) | 2011-07-13 |
| US6371412B1 (en) | 2002-04-16 |
| WO2001034468A9 (en) | 2002-08-15 |
| EP1227977A1 (en) | 2002-08-07 |
| WO2001034468A1 (en) | 2001-05-17 |
| DE60025941T2 (de) | 2006-08-24 |
| CA2391217A1 (en) | 2001-05-17 |
| JP2003513858A (ja) | 2003-04-15 |
| EP1227977B1 (en) | 2006-02-08 |
| DE60025941D1 (de) | 2006-04-20 |
| ATE317352T1 (de) | 2006-02-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MK6 | Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase |