| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | Aircraft propeller | US69601433 | 1933-10-31 | US1977072A | 1934-10-16 | LYMAN WILLIAM H |
| 102 | Propeller blade | US63302932 | 1932-09-14 | US1949611A | 1934-03-06 | MARTENS FRED J; THOMPSON CLINTON O |
| 103 | Propeller | US34005829 | 1929-02-15 | US1922179A | 1933-08-15 | JOHN SQUIRES |
| 104 | Propeller | US51066331 | 1931-01-23 | US1895252A | 1933-01-24 | KONTOS EMMANUEL G |
| 105 | Fluid-reactive device | US40502029 | 1929-11-05 | US1847866A | 1932-03-01 | DENINSON JACOB Z A |
| 106 | Propeller | US40603429 | 1929-11-09 | US1775568A | 1930-09-09 | STEFAN PIESIK |
| 107 | Air propeller | US75249124 | 1924-11-26 | US1742792A | 1930-01-07 | KARL STAHL |
| 108 | Propulsion screw | US25747328 | 1928-02-27 | US1717745A | 1929-06-18 | FRIEDRICH TISMER |
| 109 | Propeller | US24085327 | 1927-12-17 | US1663512A | 1928-03-20 | LOUIS BREGUET |
| 110 | Propeller | US4988825 | 1925-08-13 | US1658438A | 1928-02-07 | WARD HALL CHARLES |
| 111 | Propeller | US1610825 | 1925-03-17 | US1642803A | 1927-09-20 | BLONDIN JOSEPH A |
| 112 | Aerial propeller | US5315525 | 1925-08-28 | US1628716A | 1927-05-17 | JOSEPH FISCHER |
| 113 | Impeller | US4080625 | 1925-07-01 | US1622222A | 1927-03-22 | CALDWELL FRANK W |
| 114 | Aerial propeller | US7322725 | 1925-12-04 | US1621983A | 1927-03-22 | ALEXANDER HARPER; ALEXANDER HARPER STEWART |
| 115 | Method of controlling propellers | US24491118 | 1918-07-15 | US1501248A | 1924-07-15 | STRONG WILLIAM J H |
| 116 | Propeller | US32827319 | 1919-10-03 | US1421460A | 1922-07-04 | LEONIDAS GUILLEMET FRANCOIS |
| 117 | Airship. | US1910540868 | 1910-01-29 | US970532A | 1910-09-20 | MORRISON WILLIAM E |
| 118 | Improvement in churn-dashers | US113172D | US113172A | 1871-03-28 | ||
| 119 | Fly-expelling fan | US40746D | US40746A | 1863-12-01 | ||
| 120 | METHOD AND APPARATUS FOR INHIBITING FORMATION OF AND/OR REMOVING ICE FROM AIRCRAFT COMPONENTS | PCT/US2012049560 | 2012-08-03 | WO2013022767A3 | 2013-05-10 | GILES ALAN M; MACHIN JAMES T; GERIGUIS JOHN A |
| Methods and systems are generally described that inhibit debris (such as ice) accretions and/or remove debris (such as ice) accretions from the exterior surface of an aircraft. In some embodiments, the invention is a system (100) for an aircraft comprising: a component (120) of the aircraft having a surface; a plurality of piezo-kinetic actuators (114, 116, 118) each positioned proximate to a portion of the surface; and a control unit (102) coupled to the plurality of actuators, the control unit configured to actuate one or more of the actuators at one or more frequencies between about 1 Hz and about 1 kHz; wherein the actuators are each configured to introduce a displacement of the surface in three dimensions to inhibit a formation of ice on at least the portion of the surface and to break up existing ice formations on at least the portion of the surface. | ||||||
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