NO125949B - - Google Patents
Download PDFInfo
- Publication number
- NO125949B NO125949B NO4500/69A NO450069A NO125949B NO 125949 B NO125949 B NO 125949B NO 4500/69 A NO4500/69 A NO 4500/69A NO 450069 A NO450069 A NO 450069A NO 125949 B NO125949 B NO 125949B
- Authority
- NO
- Norway
- Prior art keywords
- downstream
- cascade
- rod
- assemblies
- chamber
- Prior art date
Links
- 230000000712 assembly Effects 0.000 claims description 46
- 238000000429 assembly Methods 0.000 claims description 46
- 238000011144 upstream manufacturing Methods 0.000 claims description 36
- 239000000567 combustion gas Substances 0.000 claims description 25
- 239000012530 fluid Substances 0.000 claims description 18
- 239000007789 gas Substances 0.000 claims description 10
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 230000010355 oscillation Effects 0.000 claims description 2
- 230000006378 damage Effects 0.000 claims 1
- 238000010276 construction Methods 0.000 description 9
- 238000006073 displacement reaction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000006386 neutralization reaction Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US78032768A | 1968-12-02 | 1968-12-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NO125949B true NO125949B (enrdf_load_stackoverflow) | 1972-11-27 |
Family
ID=25119281
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO4500/69A NO125949B (enrdf_load_stackoverflow) | 1968-12-02 | 1969-11-13 |
Country Status (9)
| Country | Link |
|---|---|
| BE (1) | BE740622A (enrdf_load_stackoverflow) |
| CH (1) | CH524764A (enrdf_load_stackoverflow) |
| DE (1) | DE1959543A1 (enrdf_load_stackoverflow) |
| DK (1) | DK124700B (enrdf_load_stackoverflow) |
| FR (1) | FR2025052A1 (enrdf_load_stackoverflow) |
| GB (1) | GB1258148A (enrdf_load_stackoverflow) |
| NL (1) | NL6918101A (enrdf_load_stackoverflow) |
| NO (1) | NO125949B (enrdf_load_stackoverflow) |
| SE (1) | SE358603B (enrdf_load_stackoverflow) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4585207A (en) * | 1985-09-03 | 1986-04-29 | Joy Manufacturing Company | Expanding gate valve with pneumatic actuator |
| FR3066788B1 (fr) * | 2017-05-23 | 2019-07-12 | Airbus Operations | Moteur pour aeronef comprenant au moins un actionneur de systeme d'inversion de poussee agence dans un cone d'ejection des gaz |
-
1969
- 1969-10-22 BE BE740622D patent/BE740622A/xx unknown
- 1969-11-13 NO NO4500/69A patent/NO125949B/no unknown
- 1969-11-21 CH CH1740369A patent/CH524764A/de not_active IP Right Cessation
- 1969-11-25 GB GB1258148D patent/GB1258148A/en not_active Expired
- 1969-11-27 DE DE19691959543 patent/DE1959543A1/de active Pending
- 1969-12-01 SE SE16499/69A patent/SE358603B/xx unknown
- 1969-12-01 DK DK635169AA patent/DK124700B/da unknown
- 1969-12-02 FR FR6941583A patent/FR2025052A1/fr not_active Withdrawn
- 1969-12-02 NL NL6918101A patent/NL6918101A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| CH524764A (de) | 1972-06-30 |
| BE740622A (enrdf_load_stackoverflow) | 1970-04-01 |
| GB1258148A (enrdf_load_stackoverflow) | 1971-12-22 |
| DK124700B (da) | 1972-11-13 |
| NL6918101A (enrdf_load_stackoverflow) | 1970-06-04 |
| SE358603B (enrdf_load_stackoverflow) | 1973-08-06 |
| FR2025052A1 (enrdf_load_stackoverflow) | 1970-09-04 |
| DE1959543A1 (de) | 1970-06-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3988889A (en) | Cowling arrangement for a turbofan engine | |
| US3514053A (en) | Aircraft,especially of the vtol type | |
| US3500646A (en) | Thrust reverser | |
| USRE24703E (en) | Jet spoiler for gas turbine jet propulsion plant | |
| BRPI0611975A2 (pt) | redutor de empuxo em núcleo de turboventilador | |
| US4396073A (en) | Underground boring apparatus with controlled steering capabilities | |
| US3492821A (en) | Thrust reversing means for a gas turbine bypass engine | |
| US2944395A (en) | Means and methods of neutralizing and converting thrust components | |
| US2523842A (en) | Adjustable jet nozzle for jet propulsion units | |
| ES2950004T3 (es) | Una tobera de escape para un motor de turbina de gas | |
| US3814324A (en) | Propulsion nozzle and actuator system employed therein | |
| EP1621744B1 (fr) | Ensemble de cône d'entrée d'une turbomachine et d'un arbre portant des aubes de soufflante | |
| NO125949B (enrdf_load_stackoverflow) | ||
| CA2610056A1 (fr) | Turbopropulseur comportant un ensemble de pales a orientation reglable | |
| FR2596809A1 (fr) | Perfectionnements de tuyeres orientables pour aeronefs | |
| RU2001110078A (ru) | Осесимметричное сверхзвуковое реактивное сопло | |
| US20040068977A1 (en) | Thrust reverser for a jet engine and hydraulic actuator | |
| US3525577A (en) | Propellers | |
| US2475022A (en) | Fluid reaction propulsive device | |
| GB1188391A (en) | Improvements in or relating to Helicopter Rotors | |
| US2735499A (en) | ehlers | |
| DK146276B (da) | Indstillingsmekanisme for bladene i en stilbar propeller | |
| FR2903454A1 (fr) | Nacelle de reacteur d'aeronef et aeronef comprenant une telle nacelle | |
| US5142862A (en) | Thrust reversing system for high bypass fan engines | |
| US3355889A (en) | Movable power plant for direct lift and forward propulsion |