GB750616A - Improvements in jet propulsion nozzles - Google Patents
Improvements in jet propulsion nozzlesInfo
- Publication number
- GB750616A GB750616A GB14052/53A GB1405253A GB750616A GB 750616 A GB750616 A GB 750616A GB 14052/53 A GB14052/53 A GB 14052/53A GB 1405253 A GB1405253 A GB 1405253A GB 750616 A GB750616 A GB 750616A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet
- nozzle
- jet propulsion
- auxiliary
- deflected
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Gas After Treatment (AREA)
Abstract
750,616. Jet propulsion plant. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. May 19, 1953 [May 21, 1952; May 6, 1953], No.. 14052/53. Class 110(3) [Also in Group XXXIII] In a jet propulsion nozzle in which the area of the nozzle is varied or the jet deflected by an auxiliary screen-like jet issuing into the nozzle in a direction which is generally perpendicular or inclined upstream with respect to the axis of the nozzle, the momentum of the auxiliary jet is increased by heating or by injecting a vaporizable liquid into it or both. In the gas turbine jet propulsion engine shown the propulsion nozzle 5 has an annular slot 6, inclined in the upstream direction, connected to a chamber 7 supplied with gas under pressure from the compressor 2 through a control vaive 9 and combustion chamber 10. The combustion chamber 10 may be replaced by a spray injector fed with water or other liquid such as methanol. The application of the invention to a gas turbine jet propulsion engine with an exhaust heater is described. In the arrangement shown in Fig. 3 the jet is deflected through vanes 17 by an auxiliary fluid supplied to a hollow streamlined body 13. Specifications 691,302, 745,630, 750,601 are referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR750616X | 1952-05-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB750616A true GB750616A (en) | 1956-06-20 |
Family
ID=9151819
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB14052/53A Expired GB750616A (en) | 1952-05-21 | 1953-05-19 | Improvements in jet propulsion nozzles |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB750616A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006049556A1 (en) * | 2004-11-05 | 2006-05-11 | Volvo Aero Corporation | A device for controlling a gas flow, a jet engine comprising the device and an aircraft somprising the device |
-
1953
- 1953-05-19 GB GB14052/53A patent/GB750616A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006049556A1 (en) * | 2004-11-05 | 2006-05-11 | Volvo Aero Corporation | A device for controlling a gas flow, a jet engine comprising the device and an aircraft somprising the device |
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