CA468294A - Dispositifs detecteurs de givrage sur avions - Google Patents
Dispositifs detecteurs de givrage sur avionsInfo
- Publication number
- CA468294A CA468294A CA468294A CA468294DA CA468294A CA 468294 A CA468294 A CA 468294A CA 468294 A CA468294 A CA 468294A CA 468294D A CA468294D A CA 468294DA CA 468294 A CA468294 A CA 468294A
- Authority
- CA
- Canada
- Prior art keywords
- aircraft
- formation
- detecting ice
- ice
- detecting
- 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 |
---|---|---|---|
CA468294T |
Publications (1)
Publication Number | Publication Date |
---|---|
CA468294A true CA468294A (fr) | 1950-09-26 |
Family
ID=35602217
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA468294A Expired CA468294A (fr) | Dispositifs detecteurs de givrage sur avions |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA468294A (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2670912A (en) * | 1950-04-29 | 1954-03-02 | Armstrong Siddeley Motors Ltd | Means for preventing the formation of ice on an aircraft or in a gas turbine engine therefor |
US2764373A (en) * | 1953-05-18 | 1956-09-25 | Boeing Co | Heated vortex generator |
US4508295A (en) * | 1982-06-09 | 1985-04-02 | S.N.E.C.M.A. | Device for detecting and preventing the formation of ice on contoured surfaces |
-
0
- CA CA468294A patent/CA468294A/fr not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2670912A (en) * | 1950-04-29 | 1954-03-02 | Armstrong Siddeley Motors Ltd | Means for preventing the formation of ice on an aircraft or in a gas turbine engine therefor |
US2764373A (en) * | 1953-05-18 | 1956-09-25 | Boeing Co | Heated vortex generator |
US4508295A (en) * | 1982-06-09 | 1985-04-02 | S.N.E.C.M.A. | Device for detecting and preventing the formation of ice on contoured surfaces |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA468294A (fr) | Dispositifs detecteurs de givrage sur avions | |
CA463044A (fr) | Appareil pour river des parties | |
CA472591A (fr) | Avion | |
CA470226A (fr) | Moyens de freinage d'avions | |
CA463548A (fr) | Systeme de mesure | |
CA468546A (fr) | Avions | |
CA470098A (fr) | Avion | |
CA470124A (fr) | Avion | |
CA465409A (fr) | Systeme indicateur de position | |
CA470398A (fr) | Systemes radiogoniometriques | |
CA467062A (fr) | Systemes de detection | |
CA469872A (fr) | Systemes de detection | |
CA466502A (fr) | Dispositif d'atterrissage d'avion | |
AU148281B2 (en) | Aircraft deicing means | |
CA462615A (fr) | Stabilisateur automatique pour avions | |
CA464983A (fr) | Systeme de reglage de pression d'air dans avion | |
CA469641A (fr) | Dispositifs de ramassage pour avions | |
AU145584B2 (en) | Underwing refuelling system | |
CA469745A (fr) | Dispositifs de parachutes | |
AU151297B2 (en) | Thrust indicator system | |
CA462978A (fr) | Avion | |
CA464171A (fr) | Systeme indicateur d'emplacement | |
CA465415A (fr) | Flotteur d'avion | |
CA469100A (fr) | Systemes indicateurs | |
AU148919B2 (en) | Improvements in gyro-verticals for aircraft |