IT7828779A0 - Perfezionamenti nel o in riferimento all'effetto frenante di un invertitore di spinta di un motore a turbina a gas su un aeromobile connesso. - Google Patents
Perfezionamenti nel o in riferimento all'effetto frenante di un invertitore di spinta di un motore a turbina a gas su un aeromobile connesso.Info
- Publication number
- IT7828779A0 IT7828779A0 IT7828779A IT2877978A IT7828779A0 IT 7828779 A0 IT7828779 A0 IT 7828779A0 IT 7828779 A IT7828779 A IT 7828779A IT 2877978 A IT2877978 A IT 2877978A IT 7828779 A0 IT7828779 A0 IT 7828779A0
- Authority
- IT
- Italy
- Prior art keywords
- relating
- gas turbine
- turbine engine
- braking effect
- thrust reverser
- Prior art date
Links
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
- F02K1/74—Reversing at least one flow in relation to at least one other flow in a plural- flow engine
-
- 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
- F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
-
- 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
- F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
- F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings for the reversed flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4299477 | 1977-10-15 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IT7828779A0 true IT7828779A0 (it) | 1978-10-13 |
| IT1099715B IT1099715B (it) | 1985-09-28 |
Family
ID=10426882
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT28779/78A IT1099715B (it) | 1977-10-15 | 1978-10-13 | Perfezionamenti nel o in riferimento all'effetto fremante di un invertitore di spinta di un motore a turbina a gas su un apromobile connesso |
Country Status (4)
| Country | Link |
|---|---|
| JP (1) | JPS5466000A (it) |
| DE (1) | DE2844739A1 (it) |
| FR (1) | FR2406082A1 (it) |
| IT (1) | IT1099715B (it) |
-
1978
- 1978-10-12 FR FR7829148A patent/FR2406082A1/fr not_active Withdrawn
- 1978-10-13 IT IT28779/78A patent/IT1099715B/it active
- 1978-10-13 DE DE19782844739 patent/DE2844739A1/de active Pending
- 1978-10-16 JP JP12723578A patent/JPS5466000A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5466000A (en) | 1979-05-28 |
| IT1099715B (it) | 1985-09-28 |
| DE2844739A1 (de) | 1979-05-10 |
| FR2406082A1 (fr) | 1979-05-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB2038947B (en) | Gas turbine by-pass type jet engines | |
| IT8222040A0 (it) | Propulsore composito particolarmente applicabile a turbomotori a gas. | |
| IT1110712B (it) | Metodo e apparato per controllare la spinta in un turbomotore a gas | |
| GB2019947B (en) | Gas turbine engine combustor assembly | |
| IT7921628A0 (it) | Motore a turbina a gas. | |
| IT7821288A0 (it) | Motore per turbina a gas. | |
| GB2009683B (en) | Thrust reverser for an asymmetric aircraft exhaust nozzle | |
| IT8020445A0 (it) | Motore a turbina a gas. | |
| IL60648A (en) | Gas turbine exhaust thrust vectorable nozzle | |
| IT1096061B (it) | Dispositivo per la manutenzione di propulsori a turbina a gas,in particolare di propulsori a turbogetto | |
| GB2005356A (en) | Composite gas turbine engine for v/stol aircraft | |
| GB1545089A (en) | Jet engine thrust reverser and cowl structure | |
| GB1541066A (en) | Aircraft gas turbine engine flight manoeuverable exhaust nozzle | |
| IT8324164A0 (it) | Perfezionamenti apportati alle prese d'aria di motori a turbina agas montati su aeromobili. | |
| JPS5254826A (en) | Cowling structure for gas turbine engine | |
| GB1557817A (en) | Gas turbine ducted fan engines having expansion to sub atmospheric pressure | |
| JPS5582231A (en) | Gas turbine engine combustor | |
| IT1109876B (it) | Motori a turbina a gas | |
| GB1544826A (en) | Turbofan gas turbine engines | |
| JPS57198348A (en) | Thrust reversal/exhaust gas nozzle assemblage for gas turbine engine | |
| GB2038948B (en) | Gas turbine by-pass jet engines | |
| GB1542642A (en) | Thrust reverser for by-pass gas turbine engine | |
| IT7830937A0 (it) | Perfezionamenti apportati ai motori a turbina a gas. | |
| IT7828779A0 (it) | Perfezionamenti nel o in riferimento all'effetto frenante di un invertitore di spinta di un motore a turbina a gas su un aeromobile connesso. | |
| IT1158416B (it) | Motore a turbina a gas per la propulsione di missili |