CN100999257A - Special Divine land airship with special fuel engine as power - Google Patents
Special Divine land airship with special fuel engine as power Download PDFInfo
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- CN100999257A CN100999257A CN 200710066709 CN200710066709A CN100999257A CN 100999257 A CN100999257 A CN 100999257A CN 200710066709 CN200710066709 CN 200710066709 CN 200710066709 A CN200710066709 A CN 200710066709A CN 100999257 A CN100999257 A CN 100999257A
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- space flying
- special fuel
- magnalium
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Abstract
The present invention relates to a flying boat with new-type engine providing power. Said flying boat is composed of series machine and component system, electric circuit system, course system and special fuel of engine. Besides, said invention also provides the concrete structure and composition of above-mentioned every system.
Description
Technical field
The present invention relates to a kind of spacecraft with special engine, be mainly used in divine boat's flight and moonfall.The space flying of a kind of special fuel engine priming of the present invention power is made up of series mechanical and component system, appliance circuit system, heading control system and the used special fuel of special fuel engine:
(1) space flying is one-body molded and under-chassis rises automatically, the compression system device by four groups of wings of short wing, body afterbody of the lead aircraft wing, body upper and the bottom on body, body both sides.
(2) the body both sides lead aircraft wing bottom moment place's ascending, descending device system and device and the body afterbody wing moment place left and right heading device system and device of space flying.
(3) the special fuel engine system of space flying.
(4) change speed gear box of space flying, propelling unit, propeller and empty round shell device.
(5) appliance circuit system, lamp system, the heading control system of space flying.
(6) the used special fuel of the special fuel engine of space flying.Prescription (1) oxygen (O
2), hydrogen (H
2).
Existing space flight Shenzhou (Divine Vessel) is generally all used rocket launching, and rocket launching requires the safety factor high percentage, otherwise consequence can not be imagined, yet, rocket is once launched the back can not launch use once more with regard to scrapping fully, safety factor required also very highly when simultaneously recovery bin fell after rise, just in case do not open parachute or umbrella rope have broken the consequence that can not imagine can take place all.
Summary of the invention
The object of the invention, avoid the weak point in the background, the space flying of special fuel engine priming power of the present invention, not only can safe divine boat aerial mission outside, add special fuel again in the fuel cylinder after airship returns and lands, airship can continue to carry out new divine boat's aerial mission again.
Technical solution of the present invention
(1) the present invention selects for use a kind of special fuel engine to do the power of space flying.
(2) the present invention is to the repacking of driving engine, and to body, wing and series mechanical and parts strict design and accurate manufacturing, space flying has had the function of flying and landing on the moon in divine boat.
(3) the used special fuel of space flying of a kind of special fuel engine priming of the present invention power; Prescription (1) oxygen (O
2), hydrogen (H
2).
The present invention compares with background technology
One, under equal situation, the present invention can finish divine boat's flight detection mission very safely.
Two, under equal situation, the present invention only needs to add special fuel in the special fuel bomb can continue to carry out new divine boat's aerial mission again.
Example 1: a kind of space flying of special fuel engine priming power, it is characterized in that airship is one-body molded and under-chassis rises automatically, the compression system device by the wing of four groups of weak points of short wing, body afterbody of the lead aircraft wing on body, body both sides and body upper bottom;
(1) be placed in the model of system space flying body with magnalium tungsten alloy plate and make the various parts of body behind the hydraulic pressure, assembling is welded into the body of space flying then, and the body inwall is by the dress insulating layer material.
(2) be placed in the wing model of system space flying body two length of sides with magnalium tungsten alloy plate, make the various parts of the lead aircraft wing behind the hydraulic pressure, be placed in the short wing model in system space flying body upper bottom with the alloy plate equally, make the various parts of short wing behind the hydraulic pressure, the short wing of the lead aircraft wing on moment assembling then, the body that is welded into the complete one of space flying, body both sides and body upper bottom.Long wing is installed in the level attitude on body both sides, and short wing is installed in the bottom and the top of body, and all becomes 90 degree positions between each wing.
(3) be placed in the system space flying body afterbody wing model with magnalium tungsten alloy plate, make the various parts of body afterbody wing behind the hydraulic pressure, body, wing, the body afterbody wing of the complete one of space flying assembled, is welded into to moment then.Totally four groups on the wing of its body afterbody, all become between each position of four groups of wings 90 the degree, and with every pair of all same plane of preceding wing.
(4) make the under-chassis various parts that rise automatically, contract with magnalium tungsten alloy material precision, press the moment place, bottom of the installation body both sides level attitude lead aircraft wing then, automatically rise, contract various mould parts moments by place, installation body tail bottom with under-chassis equally, and three functions that under-chassis all has automatic liter, contracts and control.
Example 2: a kind of space flying of special fuel engine priming power is characterized in that the bottom moment place ascending, descending device system and device of the body both sides lead aircraft wing of space flying and body afterbody wing moment place left and right heading device system and device;
(1) make the various parts of ascending, descending device system with magnalium tungsten alloy material precision, moment is by place, lead aircraft wing bottom, installation body both sides then, and the ascending, descending automatic control function is arranged.
(2) make the various parts of left and right heading device system with magnalium tungsten alloy material precision, moment is by installation wing place, body afterbody top then, and left and right flight automatic control function is arranged.
Example 3: a kind of space flying of special fuel engine priming power is characterized in that the special fuel engine system of space flying;
(1) two kinds of different pressurized fuel gas (high-pressure liquid oxygen is housed, high-pressure liquid hydrogen) two high pressure magnalium tungsten alloy bottles, link with two metal tracheaes and two high pressure magnalium tungsten alloy bottles respectively, two gas high-voltage devices and two speed adjusters and two metal tracheal systems link then, gaseous fuel behind two gas high-voltage device high pressure inserts in the air inlet pipe of driving engine closed system with two metal tracheaes then, and establish the hole of a specification at enclosed air inlet pipe place, the little ball of a hole internal orifice dress activity, little ball has the function of the air only import but no export from the hole, establishes the collar extension of locating in the hole at enclosed air inlet pipe at last and loads onto the dust exhaustor system.
(2) two kinds of mixed fuels enter in the cylinder of driving engine, and the inlet valve and the exhaust valve of driving engine are all closed simultaneously.
(3) after the mixed fuel in the engine cylinder compresses high pressure, spark ignitor mixed fuel work by combustion.
(4) the mixed fuel waste gas after burning enters freeing pipe from the exhaust valve discharging in the engine cylinder.
Example 4: a kind of space flying of special fuel engine priming power is characterized in that the change speed gear box of space flying, propelling unit, propeller and empty circle shell systems device;
(1) the belt pulley gear of the belt pulley gear of special fuel engine and change speed gear box links, then, the blade wheel gear of change speed gear box and angle of rake belt pulley gear link, and fixedly load onto propeller in the propeller place in impeller system then, make propelling unit drive propeller and fly at a high speed to change.
(2) driving engine, change speed gear box, propelling unit and propeller integrated system are fixed in the round shell of sky of a magnalium tungsten alloy system, and again that the sky circle shell of magnalium tungsten alloy system is solid at the moment position of the body both sides lead aircraft wing with the front and back of short wing and body afterbody wing by dress.Wherein, moment is pressed dress front and back totally eight empty circle shells on the lead aircraft wing on body both sides, four groups of wings of the short wing of the top of body, bottom and body afterbody, and each moment of the front and back of each wing is by adorning an empty round shell.
Example 5: a kind of space flying of special fuel engine priming power is characterized in that the appliance circuit system of space flying, lamp system, heading control system;
(1) there is engine start circuit in the appliance circuit system of space flying, generator charging circuit, tally circuit.
(2) tally circuit of the space flying signal lamp that takes off, normal flight signal lamp, falling signal lamp.
(3) heading control system of space flying has compass, course line, aerophone, ground radar.
Example 6: a kind of space flying of special fuel engine priming power is characterized in that the special fuel that the special fuel engine of space flying is used; Prescription (1) oxygen (O
2), hydrogen (H
2), then two kinds of different pressurized fuel gas are contained in respectively in the bomb of two magnalium tungsten alloy systems of special fuel engine system (high-pressure liquid hydrogen, high-pressure liquid oxygen).
Claims (7)
1, a kind of space flying of special fuel engine priming power is characterized in that: the one-body molded and under-chassis of four groups short wings of short wing, body afterbody of the lead aircraft wing on the body of space flying, body both sides and body upper bottom the parts system and device that rises automatically, contracts; The lead aircraft wing bottom moment place's ascending, descending device system and device and the body afterbody wing moment place left and right heading device system and device on airship body both sides; The special fuel engine system of airship; The series mechanical machine equipment system and device of airship; The appliance circuit system of airship; The used special fuel of special fuel engine of the lamp system of airship, the heading control system of airship, airship.
2, the space flying of special fuel engine priming power according to claim 1, it is characterized in that airship is one-body molded and under-chassis rises automatically, the compression system device by the wing of the short four groups of weak points of wing, body afterbody in the lead aircraft wing of body, body both sides level attitude, body upper and bottom;
(1) be placed in the model of system space flying body with magnalium tungsten alloy plate and make the various parts of body behind the hydraulic pressure, assembling is welded into the body of space flying then, and the body inwall is by the dress insulating layer material.
(2) be placed in the wing model of system space flying body two length of sides with magnalium tungsten alloy plate, make the various parts of the lead aircraft wing behind the hydraulic pressure, be placed in the wing model of system space flying body upper, bottom weak point with the alloy plate equally, make the various parts of short wing, moment assembling then behind the hydraulic pressure, be welded into body, the body both sides level attitude lead aircraft wing of the complete one of space flying, the short wing in body upper and bottom, and all become 90 degree positions between each wing.
(3) be placed in the system space flying body afterbody wing model with magnalium tungsten alloy plate, make the various parts of body afterbody wing behind the hydraulic pressure, the lead aircraft wing of moment assembling then, the body that is welded into the complete one of space flying, body and short wing, body afterbody wing.Position between totally four groups on the wing of its body afterbody, four groups of wings all becomes 90 degree, and with every pair of all same plane of preceding wing.
(4) make the under-chassis various parts that rise automatically, contract with magnalium tungsten alloy material precision, press the moment place, bottom of the installation body both sides level attitude lead aircraft wing then, automatically rise, contract various parts moments by place, installation body afterbody bottom with under-chassis equally, and three functions that under-chassis all has automatic liter, contracts and control.
3, the space flying of special fuel engine priming power according to claim 1, it is characterized in that the lead aircraft wing bottom moment place's ascending, descending device system and device and the body afterbody wing moment place left and right heading device system and device on space flying body both sides;
(1) make the various parts of ascending, descending device system with magnalium tungsten alloy material precision, moment is by place, lead aircraft wing bottom, installation body both sides then, and the ascending, descending automatic control function is arranged.
(2) make the various parts of left and right heading device system with magnalium tungsten alloy material precision, moment is by installation wing place, body afterbody top then, and left and right flight automatic control function is arranged.
4, the space flying of special fuel engine priming power according to claim 1 is characterized in that, the special fuel engine system of space flying;
(1) two kinds of different pressurized fuel gas (high-pressure liquid oxygen is housed, high-pressure liquid hydrogen) two high pressure magnalium tungsten alloy bottles, link with two metal tracheaes and two high pressure magnalium tungsten alloy bottles respectively, two gas high-voltage devices and two speed adjusters and two metal tracheal systems link then, gaseous fuel behind two gas high-voltage device high pressure inserts in the air inlet pipe of driving engine closed system with two metal tracheaes then, and establish the hole of a specification at enclosed air inlet pipe place, the little ball of a hole internal orifice dress activity, little ball has the function of the air only import but no export from duck eye, establishes the collar extension of locating in the hole at enclosed air inlet pipe at last and loads onto the dust exhaustor system.
(2) two kinds of mixed fuels enter in the cylinder of driving engine, and the inlet valve and the exhaust valve of driving engine are all closed simultaneously.
(3) after the mixed fuel in the engine cylinder compresses high pressure, spark ignitor mixed fuel work by combustion.
(4) the mixed fuel waste gas after burning enters freeing pipe from the exhaust valve discharging in the engine cylinder.
5, the space flying of special fuel engine priming power according to claim 1 is characterized in that, the change speed gear box of space flying, propelling unit, propeller and empty circle shell systems device;
(1) the belt pulley gear of the belt pulley gear of special fuel engine and change speed gear box links, then, the blade wheel gear of change speed gear box and angle of rake belt pulley gear link, and fixedly load onto propeller in the propeller place in impeller system then, make propelling unit drive propeller and fly at a high speed to change.
(2) driving engine, change speed gear box, propelling unit and propeller integrated system are fixed in the sky circle shell of a magnalium tungsten alloy system, and again the sky circle shell of magnalium tungsten alloy system are fixed on the moment position of the front and back of the body both sides lead aircraft wing and short wing and body afterbody wing by dress.Wherein, moment is pressed dress front and back totally eight empty circle shells on the lead aircraft wing of body both sides, the top of body, the short wing in bottom and four groups of wings of body afterbody, and each moment of the front and back of each wing is by adorning a sky circle shell.
6, the space flying of special fuel engine priming power according to claim 1 is characterized in that, the appliance circuit system of space flying, lamp system, heading control system;
(1) there is engine start circuit in the appliance circuit system of space flying, generator charging circuit, tally circuit.
(2) tally circuit of the space flying signal lamp that takes off, normal flight signal lamp, falling signal lamp.
(3) heading control system of space flying has compass, course line, aerophone, ground radar.
7, the space flying of special fuel engine priming power according to claim 1 is characterized in that, the special fuel that the special fuel engine of space flying is used; Prescription (1) oxygen (O
2), hydrogen (H
2), then two kinds of different pressurized fuel gas are contained in respectively in the bomb of two magnalium tungsten alloy systems of special fuel engine system (high-pressure liquid oxygen, high-pressure liquid hydrogen).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710066709 CN100999257A (en) | 2007-01-15 | 2007-01-15 | Special Divine land airship with special fuel engine as power |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710066709 CN100999257A (en) | 2007-01-15 | 2007-01-15 | Special Divine land airship with special fuel engine as power |
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| Publication Number | Publication Date |
|---|---|
| CN100999257A true CN100999257A (en) | 2007-07-18 |
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ID=38258105
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|---|---|---|---|
| CN 200710066709 Pending CN100999257A (en) | 2007-01-15 | 2007-01-15 | Special Divine land airship with special fuel engine as power |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103823978A (en) * | 2014-02-25 | 2014-05-28 | 北京航空航天大学 | Method and system for authenticating safety of alternative fuel in aircraft engine |
| CN114852372A (en) * | 2022-07-06 | 2022-08-05 | 沈阳建筑大学 | Aerospace variant aircraft with folding wing function and launching system thereof |
-
2007
- 2007-01-15 CN CN 200710066709 patent/CN100999257A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103823978A (en) * | 2014-02-25 | 2014-05-28 | 北京航空航天大学 | Method and system for authenticating safety of alternative fuel in aircraft engine |
| CN103823978B (en) * | 2014-02-25 | 2017-05-17 | 北京航空航天大学 | Method and system for authenticating safety of alternative fuel in aircraft engine |
| CN114852372A (en) * | 2022-07-06 | 2022-08-05 | 沈阳建筑大学 | Aerospace variant aircraft with folding wing function and launching system thereof |
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Open date: 20070718 |