HRP960498A2 - - Google Patents
Download PDFInfo
- Publication number
- HRP960498A2 HRP960498A2 HRP960498A HRP960498A2 HR P960498 A2 HRP960498 A2 HR P960498A2 HR P960498 A HRP960498 A HR P960498A HR P960498 A2 HRP960498 A2 HR P960498A2
- Authority
- HR
- Croatia
- Prior art keywords
- chamber
- nozzles
- compressor
- engine according
- aircraft
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims description 19
- 239000007789 gas Substances 0.000 claims description 9
- 238000002485 combustion reaction Methods 0.000 claims description 8
- 238000002347 injection Methods 0.000 claims description 5
- 239000007924 injection Substances 0.000 claims description 5
- 238000010892 electric spark Methods 0.000 claims description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 1
- 229910052799 carbon Inorganic materials 0.000 claims 1
- 238000009434 installation Methods 0.000 description 3
- 230000001141 propulsive effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Landscapes
- Transmission Devices (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| HRP960498 HRP960498B1 (enrdf_load_stackoverflow) | 1996-10-24 | 1996-10-24 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| HRP960498 HRP960498B1 (enrdf_load_stackoverflow) | 1996-10-24 | 1996-10-24 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| HRP960498A2 true HRP960498A2 (enrdf_load_stackoverflow) | 1998-04-30 |
| HRP960498B1 HRP960498B1 (enrdf_load_stackoverflow) | 2005-04-30 |
Family
ID=10946480
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| HRP960498 HRP960498B1 (enrdf_load_stackoverflow) | 1996-10-24 | 1996-10-24 |
Country Status (1)
| Country | Link |
|---|---|
| HR (1) | HRP960498B1 (enrdf_load_stackoverflow) |
-
1996
- 1996-10-24 HR HRP960498 patent/HRP960498B1/xx not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| HRP960498B1 (enrdf_load_stackoverflow) | 2005-04-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3219937B1 (en) | Engine bleed system with turbo-compressor and corresponding method | |
| EP3344537B1 (en) | Fluidic propulsive system and thrust and lift generator for aerial vehicles | |
| US11473497B2 (en) | Engine bleed system with motorized compressor | |
| US2411227A (en) | Power plant for airplanes | |
| US2478206A (en) | Multirotor gas turbine power plant with propeller | |
| US2430399A (en) | Jet augmenter for combustion turbine propulsion plants | |
| CN107191276A (zh) | 具有多分接头引气阵列的发动机引气系统 | |
| US20210140641A1 (en) | Method and system for rotating detonation combustion | |
| CN109236494B (zh) | 超高速推力矢量喷气发动机 | |
| US3111005A (en) | Jet propulsion plant | |
| CN2695659Y (zh) | 复式冲压涡扇发动机 | |
| CA3159326A1 (en) | Segmented augmented turbine assembly | |
| US9109535B2 (en) | Propulsion system and method | |
| US3812672A (en) | Supercharged ejector ramjet aircraft engine | |
| US2818223A (en) | Jet propulsion of helicopters | |
| US2713243A (en) | Rocket and turbine engine combination for aircraft | |
| CN103726952B (zh) | 分流式燃气涡轮发动机 | |
| CN103807022B (zh) | 一种双向涡叶内冷负压航空氢动力发动机 | |
| HRP960498A2 (enrdf_load_stackoverflow) | ||
| US3486340A (en) | Gas turbine powerplant with means for cooling compressed air | |
| Meher-Homji et al. | Pioneering Turbojet Developments of Dr. Hans Von Ohain—From the HeS 1 to the HeS 011 | |
| CN106523187A (zh) | 分流式燃气涡轮发动机 | |
| US3204403A (en) | Jet propulsion gas turbine engines with selectively operable air cooling means | |
| US2644301A (en) | Ram jet turbine | |
| GB1211064A (en) | Improvements in gas turbine engines |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A1OB | Publication of a patent application | ||
| AIPI | Request for the grant of a patent on the basis of a substantive examination of a patent application | ||
| B1PR | Patent granted | ||
| PB20 | Patent expired after termination of 20 years |
Effective date: 20161024 |