TR200706725A2 - Jiroskoplu mekanizma ile uzay aracı itiş sistemi - Google Patents
Jiroskoplu mekanizma ile uzay aracı itiş sistemiInfo
- Publication number
- TR200706725A2 TR200706725A2 TR2007/06725A TR200706725A TR200706725A2 TR 200706725 A2 TR200706725 A2 TR 200706725A2 TR 2007/06725 A TR2007/06725 A TR 2007/06725A TR 200706725 A TR200706725 A TR 200706725A TR 200706725 A2 TR200706725 A2 TR 200706725A2
- Authority
- TR
- Turkey
- Prior art keywords
- movement
- spacecraft
- gyroscopes
- difference
- gyros
- Prior art date
Links
- 238000010438 heat treatment Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 230000000737 periodic effect Effects 0.000 abstract 1
- 230000005855 radiation Effects 0.000 abstract 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
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/409—Unconventional spacecraft propulsion systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
- F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
- F03G7/10—Alleged perpetua mobilia
-
- 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
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/408—Nuclear spacecraft propulsion
-
- 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
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
-
- 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
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
- B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
- B64G1/503—Radiator panels
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Motorcycle And Bicycle Frame (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Details Of Aerials (AREA)
Abstract
Buluş uzay araçlarına itiş kuvveti vermek için araca izafi olarak periyodik kapalı bir eğri çizdirilerek hareket ettirilen jiroskoplarm kullanılması şeklinde bir yöntemdir. Jiroskoplar kendileri ile beraber hareket eden elektrik motorlarına sahiptir. İtiş kuvveti sağlanacak yönde ve aksi yönde periyodik olarak yaptırılan harekette jiroskopların dönme ekseni döndürülmekte ve bir yöne olan hareketten kaynaklanan tepki kuvveti ile diğer yönde hareketten kaynaklanan tepki kuvveti arasında fark olması sağlanmaktadır. Bu fark itiş amaçlı kuvvet olarak kullanılmaktadır. Buluşun ikinci uygulaması uzay aracını yavaşlatmakta jeneratöre bağlı jiroskoplar kullanmak, yavaşlamada jiroskopta oluşan momenti elektrik enerjisine çevirmek, ısıtma dirençli panellerde ışımayla ısı transferi şeklinde dış uzaya yaymaktır.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR2007/06725A TR200706725A2 (tr) | 2007-09-28 | 2007-09-28 | Jiroskoplu mekanizma ile uzay aracı itiş sistemi |
PCT/TR2008/000116 WO2009041928A2 (en) | 2007-09-28 | 2008-09-24 | Spacecraft propulsion system with gyroscopic mechanism |
US12/452,971 US20100176248A1 (en) | 2007-09-28 | 2008-09-28 | Spacecraft propulsion system with gyroscopic mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR2007/06725A TR200706725A2 (tr) | 2007-09-28 | 2007-09-28 | Jiroskoplu mekanizma ile uzay aracı itiş sistemi |
Publications (1)
Publication Number | Publication Date |
---|---|
TR200706725A2 true TR200706725A2 (tr) | 2009-04-21 |
Family
ID=40365423
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TR2007/06725A TR200706725A2 (tr) | 2007-09-28 | 2007-09-28 | Jiroskoplu mekanizma ile uzay aracı itiş sistemi |
Country Status (3)
Country | Link |
---|---|
US (1) | US20100176248A1 (tr) |
TR (1) | TR200706725A2 (tr) |
WO (1) | WO2009041928A2 (tr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9180984B2 (en) | 2012-05-11 | 2015-11-10 | The Boeing Company | Methods and apparatus for performing propulsion operations using electric propulsion systems |
US8915472B2 (en) * | 2012-05-11 | 2014-12-23 | The Boeing Company | Multiple space vehicle launch system |
BE1022906B1 (fr) * | 2015-04-07 | 2016-10-11 | Salcedo Ranfis Aristides LIZARDO | Generateur de mouvements via transfert de force par des masses accelerer |
CN110562489B (zh) * | 2019-09-18 | 2021-04-09 | 北京工业大学 | 一种陀螺驱动的可重复展开的太阳能帆板 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030192988A1 (en) * | 2002-04-12 | 2003-10-16 | Fitzgerald David | Propulsion device with rotating elastic material |
US7028953B2 (en) * | 2001-11-11 | 2006-04-18 | Space Systems/Loral | Two-sided deployable thermal radiator system and method |
US8234943B2 (en) * | 2002-03-01 | 2012-08-07 | Ganid Productions, Llc | Apparatus and method for gyroscopic propulsion |
US7121159B2 (en) * | 2002-03-01 | 2006-10-17 | Ganid Productions, Llc | Apparatus and method for gyroscopic propulsion |
US6945063B2 (en) * | 2002-06-28 | 2005-09-20 | Marine Desalination Systems, L.L.C. | Apparatus and method for harvesting atmospheric moisture |
DE10309827A1 (de) * | 2003-03-05 | 2004-09-16 | Karl Wagner | Hubantrieb |
US6921269B2 (en) * | 2003-07-30 | 2005-07-26 | Honeywell International Inc. | Relative rotation signal transfer assembly |
US7240879B1 (en) * | 2005-05-06 | 2007-07-10 | United States of America as represented by the Administration of the National Aeronautics and Space Administration | Method and associated apparatus for capturing, servicing and de-orbiting earth satellites using robotics |
IL175596A0 (en) * | 2006-05-11 | 2007-07-04 | Rafael Advanced Defense Sys | Low orbit missile-shaped satellite for electro-optical earth surveillance and other missions |
FR2905933B1 (fr) * | 2006-09-15 | 2008-12-26 | Astrium Sas Soc Par Actions Si | Dispositif de gestion des flux thermiques dans un engin spatial et engin spatial equipe d'un tel dispositif |
US7805226B2 (en) * | 2006-09-29 | 2010-09-28 | Honeywell International Inc. | Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes |
US20080297120A1 (en) * | 2006-12-12 | 2008-12-04 | Honeywell International, Inc. | Electronically redundant spacecraft power and attitude control system |
US20100258681A1 (en) * | 2007-03-31 | 2010-10-14 | Jiubin Chen | Flying Saucer |
US8210062B2 (en) * | 2007-04-18 | 2012-07-03 | Ithaco Space Systems, Inc. | Control moment gyroscope array and method of power distribution therefor |
US8115994B2 (en) * | 2007-07-10 | 2012-02-14 | Lockheed Martin Corporation | Scanning wide field telescope and method |
US8205514B2 (en) * | 2008-01-18 | 2012-06-26 | Honeywell International Inc. | Control moment gyroscope |
US7900874B2 (en) * | 2008-01-22 | 2011-03-08 | Harvey Emanuel Fiala | Device to move an object back and forth |
US7997157B2 (en) * | 2008-02-11 | 2011-08-16 | Honeywell International Inc. | Control moment gyroscope |
-
2007
- 2007-09-28 TR TR2007/06725A patent/TR200706725A2/tr unknown
-
2008
- 2008-09-24 WO PCT/TR2008/000116 patent/WO2009041928A2/en active Application Filing
- 2008-09-28 US US12/452,971 patent/US20100176248A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
WO2009041928A2 (en) | 2009-04-02 |
WO2009041928A4 (en) | 2009-08-06 |
WO2009041928A3 (en) | 2009-05-14 |
US20100176248A1 (en) | 2010-07-15 |
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