IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
|
출원번호 |
US-0457368
(2003-06-10)
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발명자
/ 주소 |
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출원인 / 주소 |
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
9 인용 특허 :
2 |
초록
▼
A ducted fan integrated power plant unit having a propeller with a central blade wheel comprises a ducted fan stator, which stator includes an outer ring having the central air intake guide ring, an inner ring; stator guide blades connecting the outer ring and the inner ring and a fixing support, a
A ducted fan integrated power plant unit having a propeller with a central blade wheel comprises a ducted fan stator, which stator includes an outer ring having the central air intake guide ring, an inner ring; stator guide blades connecting the outer ring and the inner ring and a fixing support, a propeller, which includes main blades, a retaining ring, the later has central conical blades, between which guide openings are formed, and an engine and a fuel tank etc. When they are mounted together, the inner ring opening of the stator can be communicated with the guide openings, thereby the air flow volume is increased and air stream can be also guided to be exhausted towards the rear by these openings, at the same time the crankcase of the engine can be effectively cooled and the power and propulsion of engine can be increased.
대표청구항
▼
1. A ducted fan integrated power plant unit having a propeller with a central blade wheel, comprising:a ducted fan stator, which includes:an outer ring,an inner ring,several blade shaped connecting bars which connect the outer ring and the inner ring and which act as stator guide blades,a fixing sup
1. A ducted fan integrated power plant unit having a propeller with a central blade wheel, comprising:a ducted fan stator, which includes:an outer ring,an inner ring,several blade shaped connecting bars which connect the outer ring and the inner ring and which act as stator guide blades,a fixing support arranged on one side of the inner ring, anda conical air intake guide ring provided in a front portion of the outer ring for increasing an intake of air flow, an inner diameter of the guide ring being more large upstream than downstream;an air exhaust duct connected to a rear portion of the ducted fan stator, the air exhaust duct and the ducted fan stator having a common central axis;an internal combustion reciprocating engine having a fuel intake port and a power shaft;a fuel tank having a fuel supplying port, the engine and the fuel tank being mounted one after the other on the fixing support and being situated in the air exhaust duct, the fuel supplying port of the fuel tank being in communication with the fuel intake port of the internal combustion engine through a fuel pipe;a propeller, which includes several main blades, a conical retaining ring having a central shaft hole, and having a blade wheel that is defined by several central conical blades arranged in the retaining ring, the main blades being disposed on a periphery of the retaining ring the propeller being mounted on the power shaft of the engine through the central shaft hole of the retaining ring; anda cap, which is conical and mounted on an end portion of the power shaft and being situated in a center portion of the retaining ring of the propeller so that the central conical blades are exposed to an outside of the cap; and a spaced guide between two adjacent central conical blades communicates with an inner ring opening of the inner ring of the ducted fan stator. 2. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein a plurality of radially and uniformly distributed blade-shaped inner ring guide blades are disposed on an inner surface of the inner ring. 3. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein a rear end of the fuel tank includes tail cap. 4. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein an outer diameter of an end portion of the main blades is gradually reduced from a front to a rear, the end portion having approximately a same inclination angle as that of a peripheral surface of the air intake guide ring. 5. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein a number of the central conical blades is 4˜10. 6. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein the outer ring of the ducted fan stator includes a fixing member used for mounting the power plant unit on a model airplane. 7. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein the inner ring includes 2 to 6 guide blades. 8. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein a number of the stator guide blades is 3˜8. 9. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, wherein an inner diameter of the air exhaust duct is gradually reduced from a front to a rear. 10. The ducted fan integrated power plant unit having a propeller with central blade wheel according to claim 1, further comprising a pawl wheel starter with which the engine is easily started, and including a pawl wheel that is a cylindrical member having a bottom portion on one end and an opening on another end, the bottom portion having a connecting hole for connecting with the power shaft of the mot or, an end face of an opening end having three integrally formed protruding teeth, each protruding tooth having an inclining face with a certain inclining angle on one of the right and the left sides.
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