UA98129C2 - Air propeller - Google Patents
Air propellerInfo
- Publication number
- UA98129C2 UA98129C2 UAA200906836A UAA200906836A UA98129C2 UA 98129 C2 UA98129 C2 UA 98129C2 UA A200906836 A UAA200906836 A UA A200906836A UA A200906836 A UAA200906836 A UA A200906836A UA 98129 C2 UA98129 C2 UA 98129C2
- Authority
- UA
- Ukraine
- Prior art keywords
- blades
- rotors
- primary
- possibility
- paired
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/02—Propulsive elements directly acting on water of rotary type
- B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
- B63H1/14—Propellers
- B63H1/16—Propellers having a shrouding ring attached to blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H3/00—Propeller-blade pitch changing
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
- Supercharger (AREA)
Abstract
The invention relates to aircraft equipment and can be used for manufacture of helicopter rotors. An air motor comprises primary and secondary upper rotors, as well as primary and secondary bottom rotors, whose blades are attached to solid and hollow shafts. The blades of primary and additional rotors are paired and installed at an angle of 10-30° relative to the axis of shafts with possibility of change of the rotor pitch. The ends of paired blades are joined by a common ring. The drive mechanism of the engine is mounted on the hollow shaft with possibility of movement. The disclosed air motor provides increased lift and eliminates overshoot of the blades.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200906836A UA98129C2 (en) | 2009-06-30 | 2009-06-30 | Air propeller |
PCT/UA2009/000060 WO2011002427A1 (en) | 2009-06-30 | 2009-11-30 | Air propulsion unit |
RU2011147883/11A RU2505457C2 (en) | 2009-06-30 | 2009-11-30 | Air propulsor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200906836A UA98129C2 (en) | 2009-06-30 | 2009-06-30 | Air propeller |
Publications (1)
Publication Number | Publication Date |
---|---|
UA98129C2 true UA98129C2 (en) | 2012-04-25 |
Family
ID=43411300
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200906836A UA98129C2 (en) | 2009-06-30 | 2009-06-30 | Air propeller |
Country Status (3)
Country | Link |
---|---|
RU (1) | RU2505457C2 (en) |
UA (1) | UA98129C2 (en) |
WO (1) | WO2011002427A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2896753A1 (en) | 2013-03-05 | 2015-04-02 | Rolls-Royce North American Technologies, Inc. | Composite gas turbine engine blade having multiple airfoils |
RU2620501C2 (en) * | 2015-02-26 | 2017-05-26 | Игорь Викторович Лентов | Helicopter type aircraft rotor |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USD543928S1 (en) * | 2003-01-23 | 2007-06-05 | Ufoz, Llc | Hovercraft with stacked rotor thruster and winglets |
RU36345U1 (en) * | 2003-12-02 | 2004-03-10 | Погорелов Владимир Иванович | Vertical takeoff and landing aircraft |
JP4220941B2 (en) * | 2004-06-30 | 2009-02-04 | 三菱重工業株式会社 | Power transmission device for flying object |
UA76882C2 (en) * | 2004-12-17 | 2006-09-15 | Voda Production Technological | Rotorcraft flight structure |
RU50976U1 (en) * | 2005-02-24 | 2006-01-27 | Открытое акционерное общество "Казанское научно-производственное предприятие "Вертолеты-МИ" | CARRYING SURFACE OF A RUNWING AIRCRAFT |
RU2314972C2 (en) * | 2005-05-03 | 2008-01-20 | Алексей Александрович Анищенко | Helicopter |
RU51966U1 (en) * | 2005-09-15 | 2006-03-10 | Федеральное государственное унитарное предприятие "Государственный научно-исследовательский институт прикладных проблем" | UNMANNED AERIAL VEHICLE |
RU2335432C2 (en) * | 2006-10-24 | 2008-10-10 | Николай Евгеньевич Староверов | Rescue helicopter (versions) |
-
2009
- 2009-06-30 UA UAA200906836A patent/UA98129C2/en unknown
- 2009-11-30 RU RU2011147883/11A patent/RU2505457C2/en not_active IP Right Cessation
- 2009-11-30 WO PCT/UA2009/000060 patent/WO2011002427A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
RU2505457C2 (en) | 2014-01-27 |
RU2011147883A (en) | 2013-08-10 |
WO2011002427A1 (en) | 2011-01-06 |
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