TR201914768A2 - VIBRATION ISOLATOR FOR LAUNCHING VEHICLE - Google Patents
VIBRATION ISOLATOR FOR LAUNCHING VEHICLE Download PDFInfo
- Publication number
- TR201914768A2 TR201914768A2 TR2019/14768A TR201914768A TR201914768A2 TR 201914768 A2 TR201914768 A2 TR 201914768A2 TR 2019/14768 A TR2019/14768 A TR 2019/14768A TR 201914768 A TR201914768 A TR 201914768A TR 201914768 A2 TR201914768 A2 TR 201914768A2
- Authority
- TR
- Turkey
- Prior art keywords
- vibration isolator
- adapter
- arm
- support arm
- launching vehicle
- Prior art date
Links
- 230000008878 coupling Effects 0.000 abstract 2
- 238000010168 coupling process Methods 0.000 abstract 2
- 238000005859 coupling reaction Methods 0.000 abstract 2
Classifications
-
- 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
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/08—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with rubber springs ; with springs made of rubber and metal
- F16F15/085—Use of both rubber and metal springs
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Cage And Drive Apparatuses For Elevators (AREA)
- Lift-Guide Devices, And Elevator Ropes And Cables (AREA)
Abstract
FIRLATMA ARACI İÇİN TİTREŞİM İZOLATÖRÜ Buluş, bir fırlatma aracında (1) sağlanan bir adaptör (3) üzerine yerleştirilen bir faydalı yüke (2) bağlanır şekilde ayarlanan bir üst bağlantı elemanı (20) ve adaptöre (3) bağlanır şekilde ayarlanan bir alt bağlantı elemanı (40) içeren ve adaptör (3) üzerinde birbirine komşu olarak çoklu sayıda dizilen bir titreşim izolatörü (10) ile ilgilidir. Titreşim izolatörü (10), üst bağlantı elemanının (20) ve alt bağlantı elemanının (40) karşılıklı olarak sahip olduğu ve bir yakın uçlarında (26, 46) sağlanan birer montaj kısmına (22, 42) sahip sırasıyla bir taşıyıcı kol (24) ve bir destek kolu (44) içermesi ve ayrıca birer uzak uçlarından (28, 48) taşıyıcı kol (24) ve destek kolunu (44) birbirine mesafeli şekilde sabitler biçimde aralarında uzanan bir yükseltici kola (34) sahip bir yükseltme elemanı (30) içermektedir. Şekil 3aVIBRATION ISOLATOR FOR LAUNCHING VEHICLE The invention consists of an upper coupling (20) arranged to be connected to a payload (2) placed on an adapter (3) provided on a launch vehicle (1) and a lower coupling (adjusted to be connected to the adapter (3)). 40) and arranged in multiple numbers adjacent to each other on the adapter (3). The vibration isolator (10) is a carrier arm (24) and a carrier arm (24) having a mounting portion (22, 42) mutually owned by the upper connecting member (20) and the lower connecting member (40) and provided at one of their proximal ends (26, 46). a support arm (44) and also a raising member (30) having a riser arm (34) extending between them in a way that fixes the support arm (24) and the support arm (44) at a distance from each other at their distal ends (28, 48). Figure 3a
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR2019/14768A TR201914768A2 (en) | 2019-09-27 | 2019-09-27 | VIBRATION ISOLATOR FOR LAUNCHING VEHICLE |
PCT/TR2020/050878 WO2021061079A1 (en) | 2019-09-27 | 2020-09-23 | Vibration isolator for launch vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR2019/14768A TR201914768A2 (en) | 2019-09-27 | 2019-09-27 | VIBRATION ISOLATOR FOR LAUNCHING VEHICLE |
Publications (1)
Publication Number | Publication Date |
---|---|
TR201914768A2 true TR201914768A2 (en) | 2021-04-21 |
Family
ID=75167073
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TR2019/14768A TR201914768A2 (en) | 2019-09-27 | 2019-09-27 | VIBRATION ISOLATOR FOR LAUNCHING VEHICLE |
Country Status (2)
Country | Link |
---|---|
TR (1) | TR201914768A2 (en) |
WO (1) | WO2021061079A1 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6609681B2 (en) * | 2001-07-05 | 2003-08-26 | The Boeing Company | Method and apparatus for damping vibration |
EP1467121A2 (en) * | 2003-03-31 | 2004-10-13 | Com Dev Ltd. | Shock attenuating mounting bracket |
FR3012553B1 (en) * | 2013-10-31 | 2016-06-24 | Astrium Sas | VIBRATION ISOLATION MODULE WITH REDUCED NON-LINEAR EFFECTS |
-
2019
- 2019-09-27 TR TR2019/14768A patent/TR201914768A2/en unknown
-
2020
- 2020-09-23 WO PCT/TR2020/050878 patent/WO2021061079A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2021061079A1 (en) | 2021-04-01 |
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