ATE312754T1 - Flugzeug mit einem antriebssystem bestehend aus mehreren pulsierten detonationskraftmaschinen - Google Patents
Flugzeug mit einem antriebssystem bestehend aus mehreren pulsierten detonationskraftmaschinenInfo
- Publication number
- ATE312754T1 ATE312754T1 AT04425043T AT04425043T ATE312754T1 AT E312754 T1 ATE312754 T1 AT E312754T1 AT 04425043 T AT04425043 T AT 04425043T AT 04425043 T AT04425043 T AT 04425043T AT E312754 T1 ATE312754 T1 AT E312754T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- propulsion system
- system consisting
- pulse detonation
- power machines
- Prior art date
Links
- 238000005474 detonation Methods 0.000 title abstract 5
- 239000000446 fuel Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
- F02K7/075—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with multiple pulse-jet engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/10—All-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
- Toys (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP04425043A EP1557356B1 (de) | 2004-01-26 | 2004-01-26 | Flugzeug mit einem Antriebssystem bestehend aus mehreren pulsierten Detonationskraftmaschinen |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE312754T1 true ATE312754T1 (de) | 2005-12-15 |
Family
ID=34626575
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT04425043T ATE312754T1 (de) | 2004-01-26 | 2004-01-26 | Flugzeug mit einem antriebssystem bestehend aus mehreren pulsierten detonationskraftmaschinen |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP1557356B1 (de) |
| CN (1) | CN1647999A (de) |
| AT (1) | ATE312754T1 (de) |
| DE (1) | DE602004000238T2 (de) |
| ES (1) | ES2252728T3 (de) |
| RU (1) | RU2005101733A (de) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2493053C1 (ru) * | 2012-02-27 | 2013-09-20 | Андрей Вячеславович Канунников | Летательный аппарат |
| RU2587186C1 (ru) * | 2014-12-29 | 2016-06-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования Московский авиационный институт (национальный исследовательский университет) (МАИ) | Способ создания подъемной силы и вектора тяги крыла |
| CN106988927B (zh) * | 2017-05-22 | 2018-04-24 | 西南交通大学 | 一种高频率脉冲喷注装置 |
| CN109083765B (zh) * | 2018-07-19 | 2020-06-16 | 西北工业大学 | 一种弹用嵌入型分布式爆震发动机 |
| US11105511B2 (en) * | 2018-12-14 | 2021-08-31 | General Electric Company | Rotating detonation propulsion system |
| CN114313253B (zh) * | 2022-03-03 | 2022-05-17 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种高升阻比吸气式高超声速飞机气动布局及设计方法 |
| CN114893322B (zh) * | 2022-04-08 | 2024-10-25 | 中国人民解放军空军工程大学 | 一种周向均布的若干微激波管轴向激波入射起爆爆震装置及操作方法 |
| CN114954955A (zh) * | 2022-05-12 | 2022-08-30 | 西北工业大学 | 一种采用旋转爆震发动机的短距/垂直起降飞行器动力系统布局 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2377247A (en) * | 1941-12-09 | 1945-05-29 | Lagelbauer Ernest | Method and means for direct propulsion of aircraft or the like |
| NL91484C (de) * | 1953-04-08 | |||
| US2972862A (en) * | 1958-05-06 | 1961-02-28 | Snecma | Pulse reactor |
| FR2166324A1 (de) * | 1972-01-03 | 1973-08-17 | Guillon Marcel | |
| RU2130407C1 (ru) * | 1998-04-14 | 1999-05-20 | Анакин Анатолий Тимофеевич | Летательный аппарат с комбинированной двигательной установкой |
| GB2383823B (en) * | 2001-10-09 | 2005-06-08 | Harold Birkett | Improved propulsion engine |
-
2004
- 2004-01-26 EP EP04425043A patent/EP1557356B1/de not_active Expired - Lifetime
- 2004-01-26 ES ES04425043T patent/ES2252728T3/es not_active Expired - Lifetime
- 2004-01-26 AT AT04425043T patent/ATE312754T1/de not_active IP Right Cessation
- 2004-01-26 DE DE602004000238T patent/DE602004000238T2/de not_active Expired - Fee Related
-
2005
- 2005-01-25 RU RU2005101733/11A patent/RU2005101733A/ru not_active Application Discontinuation
- 2005-01-26 CN CNA2005100063251A patent/CN1647999A/zh active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| DE602004000238D1 (de) | 2006-01-19 |
| EP1557356A1 (de) | 2005-07-27 |
| EP1557356B1 (de) | 2005-12-14 |
| CN1647999A (zh) | 2005-08-03 |
| DE602004000238T2 (de) | 2006-07-27 |
| RU2005101733A (ru) | 2006-07-10 |
| ES2252728T3 (es) | 2006-05-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |