GB650710A - - Google Patents
Info
- Publication number
- GB650710A GB650710A GB650710DA GB650710A GB 650710 A GB650710 A GB 650710A GB 650710D A GB650710D A GB 650710DA GB 650710 A GB650710 A GB 650710A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- axial
- anxionnaz
- rateau
- iet
- 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
Abstract
650,710. Jet propulsion plant; axial-flow compressors. SOC. RATEAU, and ANXIONNAZ, R. Jan. 21, 1941, No. 7478/50. Convention date, Dec. 4, 1939. Divided out of 650,661. Drawings to Specification. [Classes 110(i) and 110(iii)] A iet reaction propulsion unit comprises a casing having a front inlet passage, a multi-stage axial flow compressor, arranged axially and driven by a gas turbine and heating devices for the compressor output. All the arrangements of the apparatus are contained in Specification 650,661. Specification 471,368 also is referred to.
Publications (1)
Publication Number | Publication Date |
---|---|
GB650710A true GB650710A (en) | 1900-01-01 |
Family
ID=1749999
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB650710D Expired GB650710A (en) |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB650710A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE963203C (en) * | 1952-05-06 | 1957-05-02 | Alfred Buechi | Propeller turbine engine |
DE1032605B (en) * | 1952-05-06 | 1958-06-19 | Sc Techn H C Eth Alfred Buechi | Turbine jet engine |
DE1118538B (en) * | 1957-04-03 | 1961-11-30 | Rolls Royce | Bypass gas turbine jet engine |
US3202383A (en) * | 1961-10-25 | 1965-08-24 | Bel John P Le | Aircraft |
DE1217140B (en) * | 1960-08-25 | 1966-05-18 | Rolls Royce | Gas turbine jet engine with additional compressor |
DE1233210B (en) * | 1963-09-27 | 1967-01-26 | Christian Hoefer | Gas turbine jet engine |
DE1242415B (en) * | 1960-09-29 | 1967-06-15 | Rolls Royce | Gas turbine jet engine |
-
0
- GB GB650710D patent/GB650710A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE963203C (en) * | 1952-05-06 | 1957-05-02 | Alfred Buechi | Propeller turbine engine |
DE1032605B (en) * | 1952-05-06 | 1958-06-19 | Sc Techn H C Eth Alfred Buechi | Turbine jet engine |
DE1118538B (en) * | 1957-04-03 | 1961-11-30 | Rolls Royce | Bypass gas turbine jet engine |
DE1217140B (en) * | 1960-08-25 | 1966-05-18 | Rolls Royce | Gas turbine jet engine with additional compressor |
DE1242415B (en) * | 1960-09-29 | 1967-06-15 | Rolls Royce | Gas turbine jet engine |
US3202383A (en) * | 1961-10-25 | 1965-08-24 | Bel John P Le | Aircraft |
DE1233210B (en) * | 1963-09-27 | 1967-01-26 | Christian Hoefer | Gas turbine jet engine |
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