FR980347A - Use of a knowingly established gradient along the walls of a solid effrps submerged in a liquid or gaseous fluid - Google Patents
Use of a knowingly established gradient along the walls of a solid effrps submerged in a liquid or gaseous fluidInfo
- Publication number
- FR980347A FR980347A FR980347DA FR980347A FR 980347 A FR980347 A FR 980347A FR 980347D A FR980347D A FR 980347DA FR 980347 A FR980347 A FR 980347A
- Authority
- FR
- France
- Prior art keywords
- effrps
- knowingly
- submerged
- walls
- solid
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H11/00—Marine propulsion by water jets
- B63H11/02—Marine propulsion by water jets the propulsive medium being ambient water
- B63H11/04—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
- B63H11/08—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H11/00—Marine propulsion by water jets
- B63H11/02—Marine propulsion by water jets the propulsive medium being ambient water
- B63H11/04—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
- B63H11/08—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type
- B63H2011/088—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type using shear forces, e.g. disc pumps or Tesla pumps
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR980347T | 1943-02-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR980347A true FR980347A (en) | 1951-05-10 |
Family
ID=9524305
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR980347D Expired FR980347A (en) | 1943-02-05 | 1943-02-05 | Use of a knowingly established gradient along the walls of a solid effrps submerged in a liquid or gaseous fluid |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR980347A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2946540A (en) * | 1948-09-13 | 1960-07-26 | Sebac Nouvelle Sa | Jet propelled aircraft |
DE1108525B (en) * | 1956-06-11 | 1961-06-08 | Voith Gmbh J M | Diffuser with a device for blowing the boundary layer |
DE1129080B (en) * | 1954-11-17 | 1962-05-03 | Hanns Freiherr Von Schertel | In buoyancy controllable water wing for vessels |
EP1921291A3 (en) * | 2006-11-10 | 2011-09-21 | United Technologies Corporation | Gas turbine engine providing simulated boundary layer thickness increase |
US8186942B2 (en) | 2007-12-14 | 2012-05-29 | United Technologies Corporation | Nacelle assembly with turbulators |
US8192147B2 (en) | 2007-12-14 | 2012-06-05 | United Technologies Corporation | Nacelle assembly having inlet bleed |
US8282037B2 (en) | 2007-11-13 | 2012-10-09 | United Technologies Corporation | Nacelle flow assembly |
US8353164B2 (en) | 2006-10-20 | 2013-01-15 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US8408491B2 (en) | 2007-04-24 | 2013-04-02 | United Technologies Corporation | Nacelle assembly having inlet airfoil for a gas turbine engine |
-
1943
- 1943-02-05 FR FR980347D patent/FR980347A/en not_active Expired
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2946540A (en) * | 1948-09-13 | 1960-07-26 | Sebac Nouvelle Sa | Jet propelled aircraft |
DE1129080B (en) * | 1954-11-17 | 1962-05-03 | Hanns Freiherr Von Schertel | In buoyancy controllable water wing for vessels |
DE1108525B (en) * | 1956-06-11 | 1961-06-08 | Voith Gmbh J M | Diffuser with a device for blowing the boundary layer |
US8844294B2 (en) | 2006-10-20 | 2014-09-30 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US8726632B2 (en) | 2006-10-20 | 2014-05-20 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US8353164B2 (en) | 2006-10-20 | 2013-01-15 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US8209953B2 (en) | 2006-11-10 | 2012-07-03 | United Technologies Corporation | Gas turbine engine system providing simulated boundary layer thickness increase |
EP1921291A3 (en) * | 2006-11-10 | 2011-09-21 | United Technologies Corporation | Gas turbine engine providing simulated boundary layer thickness increase |
US8408491B2 (en) | 2007-04-24 | 2013-04-02 | United Technologies Corporation | Nacelle assembly having inlet airfoil for a gas turbine engine |
US8282037B2 (en) | 2007-11-13 | 2012-10-09 | United Technologies Corporation | Nacelle flow assembly |
US8596573B2 (en) | 2007-11-13 | 2013-12-03 | United Technologies Corporation | Nacelle flow assembly |
US9004399B2 (en) | 2007-11-13 | 2015-04-14 | United Technologies Corporation | Nacelle flow assembly |
US8192147B2 (en) | 2007-12-14 | 2012-06-05 | United Technologies Corporation | Nacelle assembly having inlet bleed |
US8186942B2 (en) | 2007-12-14 | 2012-05-29 | United Technologies Corporation | Nacelle assembly with turbulators |
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