CA618830A - Device for varying the effective area of a jet propulsion nozzle - Google Patents
Device for varying the effective area of a jet propulsion nozzleInfo
- Publication number
- CA618830A CA618830A CA618830A CA618830DA CA618830A CA 618830 A CA618830 A CA 618830A CA 618830 A CA618830 A CA 618830A CA 618830D A CA618830D A CA 618830DA CA 618830 A CA618830 A CA 618830A
- Authority
- CA
- Canada
- Prior art keywords
- varying
- effective area
- jet propulsion
- propulsion nozzle
- nozzle
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA618830T |
Publications (1)
Publication Number | Publication Date |
---|---|
CA618830A true CA618830A (en) | 1961-04-25 |
Family
ID=35861118
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA618830A Expired CA618830A (en) | Device for varying the effective area of a jet propulsion nozzle |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA618830A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3660982A (en) * | 1969-07-28 | 1972-05-09 | Aerospatiale | Non-return device for fluid ducts and thrust reversers |
US4707981A (en) * | 1986-01-27 | 1987-11-24 | Rockwell International Corporation | Variable expansion ratio reaction engine |
US5996936A (en) * | 1997-09-29 | 1999-12-07 | General Electric Company | Fluidic throat exhaust nozzle |
US6021637A (en) * | 1997-09-29 | 2000-02-08 | General Electric Company | Integrated fluidic CD nozzle for gas turbine engine |
US6336319B1 (en) | 2000-05-26 | 2002-01-08 | General Electric Company | Fluidic nozzle control system |
-
0
- CA CA618830A patent/CA618830A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3660982A (en) * | 1969-07-28 | 1972-05-09 | Aerospatiale | Non-return device for fluid ducts and thrust reversers |
US4707981A (en) * | 1986-01-27 | 1987-11-24 | Rockwell International Corporation | Variable expansion ratio reaction engine |
US5996936A (en) * | 1997-09-29 | 1999-12-07 | General Electric Company | Fluidic throat exhaust nozzle |
US6021637A (en) * | 1997-09-29 | 2000-02-08 | General Electric Company | Integrated fluidic CD nozzle for gas turbine engine |
US6336319B1 (en) | 2000-05-26 | 2002-01-08 | General Electric Company | Fluidic nozzle control system |
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