CN105089850A - Space aircraft carrier engine - Google Patents
Space aircraft carrier engine Download PDFInfo
- Publication number
- CN105089850A CN105089850A CN201510274696.1A CN201510274696A CN105089850A CN 105089850 A CN105089850 A CN 105089850A CN 201510274696 A CN201510274696 A CN 201510274696A CN 105089850 A CN105089850 A CN 105089850A
- Authority
- CN
- China
- Prior art keywords
- aircraft carrier
- engine
- aeroengine
- fan
- space aircraft
- 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.)
- Pending
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Abstract
The invention relates to a novel aircraft carrier engine. At present, an aeto-turbofan engine only comprises a fan and a turbine, is simplex in shape and has less functions. However, the space aircraft carrier engine is provided with a plurality of fans and a plurality of turbines or piston engines, so that the security of the space aircraft carrier engine is improved. The space aircraft carrier engine can be square, rectangular, trapezoidal and the like in shape. Besides impetus, in the function aspects, such actions as vertical take-off, fore-and-aft flight, up-and-down nutation and left-and-right rotation are provided.
Description
The present invention relates to a kind of novel aeroengine.
An existing aviation turbofan engine only have a fan and a turbo machine profile single, function is few.
The present invention overcomes above-mentioned deficiency, with the fan of multiple aviation turbofan engine as in figure 1., be arranged in square, rectangular, trapezoidal, upper and lower two ends have venetian blind as in figure 2., the bottom of groove box, trigonum between two fans as in figure 3., that installation lift car is taken turns respectively, turbo machine or piston engine, the place of fuel booster, its working principle is that turbo machine or piston engine pass to multiple fan by gear connecting rod power, by venetian blind control into, discharge directions takes off vertically, front and back flight, nod up and down, left rotation and right rotation etc., when fan power of taking off is not enough, available fuel booster helps to take off.This universe aircraft carrier motor has multiple fan, multiple stage turbo machine or piston engine, improve the Security of universe aircraft carrier motor, profile has square, rectangular, trapezoidal equal length can increase according to the length of universe aircraft carrier fuselage, functionally except power, provide take off vertically, the action such as fly in front and back, nod up and down, left rotation and right rotation.Accompanying drawing illustrates: Fig. 1 is rectangular universe aircraft carrier engine map, and Fig. 2 is trapezoidal universe aircraft carrier engine map, and Fig. 3 is in square universe aircraft carrier machine, is 1. take off position of fan and arrange diagram in figure.2. be shutter control cock above in figure, beneath shutter control cock, 3. two ends shutter control cock figure is installation lift car wheel respectively in figure, turbo machine or piston engine, two trigonum figure taken off between fan of fuel booster.
Claims (5)
1. be arranged in parallel within groove box fan, aeroengine.
2. use the aeroengine of switch groove box door or venetian blind control action.
3. universe aircraft carrier motor has multiple fan and multiple stage turbo machine or piston-engined aeroengine.
4. the aeroengine that can lengthen in universe aircraft carrier fuselage length.
5. there is the aeroengine of square, rectangular, the various shape such as trapezoidal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510274696.1A CN105089850A (en) | 2015-05-27 | 2015-05-27 | Space aircraft carrier engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510274696.1A CN105089850A (en) | 2015-05-27 | 2015-05-27 | Space aircraft carrier engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105089850A true CN105089850A (en) | 2015-11-25 |
Family
ID=54571028
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510274696.1A Pending CN105089850A (en) | 2015-05-27 | 2015-05-27 | Space aircraft carrier engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105089850A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3388878A (en) * | 1965-06-01 | 1968-06-18 | Ryan Aeronautical Co | Vtol aircraft with balanced power, retractible lift fan system |
| WO2001004495A1 (en) * | 1999-07-10 | 2001-01-18 | Frank Iles | Axial flow fan |
| US20030062443A1 (en) * | 2001-10-02 | 2003-04-03 | Joseph Wagner | VTOL personal aircraft |
| JP2008075582A (en) * | 2006-09-22 | 2008-04-03 | Japan Aerospace Exploration Agency | Propelling system for v/stol aircraft |
| US20080098715A1 (en) * | 2006-10-31 | 2008-05-01 | Robert Joseph Orlando | Turbofan engine assembly and method of assembling same |
| CN101850845A (en) * | 2009-04-02 | 2010-10-06 | 余志刚 | Vertical landing lifting system of vertical landing plane |
| CN101857085A (en) * | 2010-06-03 | 2010-10-13 | 刘春� | Aircraft |
| US20130062455A1 (en) * | 2005-04-20 | 2013-03-14 | Richard H. Lugg | Hybrid jet/electric vtol aircraft |
| CN103967650A (en) * | 2013-01-24 | 2014-08-06 | 李吉光 | Turbofan engine |
-
2015
- 2015-05-27 CN CN201510274696.1A patent/CN105089850A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3388878A (en) * | 1965-06-01 | 1968-06-18 | Ryan Aeronautical Co | Vtol aircraft with balanced power, retractible lift fan system |
| WO2001004495A1 (en) * | 1999-07-10 | 2001-01-18 | Frank Iles | Axial flow fan |
| US20030062443A1 (en) * | 2001-10-02 | 2003-04-03 | Joseph Wagner | VTOL personal aircraft |
| US20130062455A1 (en) * | 2005-04-20 | 2013-03-14 | Richard H. Lugg | Hybrid jet/electric vtol aircraft |
| JP2008075582A (en) * | 2006-09-22 | 2008-04-03 | Japan Aerospace Exploration Agency | Propelling system for v/stol aircraft |
| US20080098715A1 (en) * | 2006-10-31 | 2008-05-01 | Robert Joseph Orlando | Turbofan engine assembly and method of assembling same |
| CN101850845A (en) * | 2009-04-02 | 2010-10-06 | 余志刚 | Vertical landing lifting system of vertical landing plane |
| CN101857085A (en) * | 2010-06-03 | 2010-10-13 | 刘春� | Aircraft |
| CN103967650A (en) * | 2013-01-24 | 2014-08-06 | 李吉光 | Turbofan engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20151125 |