CN103786896A - Manned spacecraft with gravity loading device - Google Patents
Manned spacecraft with gravity loading device Download PDFInfo
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- CN103786896A CN103786896A CN201410074280.0A CN201410074280A CN103786896A CN 103786896 A CN103786896 A CN 103786896A CN 201410074280 A CN201410074280 A CN 201410074280A CN 103786896 A CN103786896 A CN 103786896A
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Abstract
The invention relates to a manned spacecraft, in particular to a manned spacecraft with a gravity loading device. The manned spacecraft with the gravity loading device comprises a manned space capsule, a chassis propeller, a fuel compartment of a gravity controller, a movable cover, a power device of the gravity controller, a space rope, a rotary shaft, an arc cross bar, a space rope storage bin, rope rings, a rope lug and a space capsule head. The manned space capsule and the chassis propeller are connected with the space capsule head. The chassis propeller is connected with the rope lug. The power device of the gravity controller is fixedly connected to the bottom of the fuel compartment of the gravity controller, the bottom of the space rope storage bin and the bottom of the rotary shaft. The two ends of the space rope are fixedly connected with two rope rings respectively, the arc cross bar is sleeved with one rope ring, and the rope lug is sleeved with the other rope ring.
Description
Technical field
The present invention relates to a kind of manned spacecraft, specifically a kind of manned spacecraft with gravitational load device.
Background technology
Astronaut is in long-term space flight, because weightlessness can produce a series of and old and feeble similar physiological change: osteoporosis, muscular atrophy etc.Take osteoporosis as example, people's bone density reaches maxim at one's mid-30s, afterwards with approximately annual 0.5% speed decline.But astronaut is in the time of rule flight, and just by losing the bone amount of 1%--2%, be equivalent to the amount of two to four years at ordinary times average every month.
Another physiological change that weightlessness is brought is the change of cardiac function.Under weightlessness impact, body fluid is to shifting above the waist, blood engorgement in thoracic cavity, neck and head.This liquid shifts, and forces heart to expand, to control the CBF increasing.
The weightless health that not only threatens astronaut, also can cause " environmental pollution ".In spacecraft, various tiny particles can adrift, pollute gas in cabin always.And astronaut must take long to exercise in weightlessness, have a meal, drink water, go to toilet, the daily behaviors such as sleep.
It is more than the existing weak point of prior art.
Summary of the invention
For the defect existing in prior art, extend the service life of paintbrush.The object of the present invention is to provide a kind of manned spacecraft with gravitational load device.
For reaching above object, the technical scheme that the present invention takes is: a kind of manned spacecraft with gravitational load device, comprises manned space capsule, chassis propelling unit, the bunker of gravity control device, removable cover, the engine installation of gravity control device, space rope, S. A., circular arc whippletree, space rope deposit cabin, becket bridle, rope bolt, space capsule head; Described chassis propelling unit is positioned at the bottom of manned space capsule, and described space capsule head is positioned at the top of manned space capsule; Described chassis propelling unit and described rope tie and connect; Described removable cover is positioned at the lateral opening place in space rope deposit cabin; The engine installation of described gravity control device is fixedly connected on the bottom of the bunker of described gravity control device, described space rope deposit cabin and described S. A.; The two ends of described space rope are fixedly connected with two becket bridles respectively, and a described becket bridle is enclosed within on described circular arc whippletree, and another becket bridle is enclosed within on described rope bolt.
The present invention can also be such: described circular arc whippletree is fixed on point line position in described space rope deposit cabin parallel with described S. A..
The present invention can also be such: the bunker of described gravity control device and described space rope deposit cabin are round described S. A..
The present invention can also be such: the engine installation of described gravity control device comprises two power systems, and one is the power system that level advances, and one is the rotary power system take S. A. as axle center.
The present invention can also be such: described space rope length is more than or equal to 24.85 meters.
The present invention can also be such: described circular arc whippletree is by the annulus take described S. A. as the center of circle, intercepts 0 degree--45 degree parts form.
Accompanying drawing explanation
Fig. 1 is the structural representation that the present invention decomposes.
Fig. 2 is the structural representation that the present invention combines.
Referring to Fig. 1-2,1 is manned space capsule, and 2 is chassis propelling unit, 3 bunkers of attaching most importance to force controller, and 4 is removable cover, 5 engine installations of attaching most importance to force controller, 6 is space rope, and 7 is S. A., and 8 is circular arc whippletree, 9 is space rope deposit cabin, and 10 is becket bridle, and 11 is rope bolt, and 12 is space capsule head.
The specific embodiment
Referring to Fig. 1-2, the present invention is a kind of manned spacecraft with gravitational load device, comprises manned space capsule 1, chassis propelling unit 2, the bunker 3 of gravity control device, removable cover 4, the engine installation 5 of gravity control device, space rope 6, S. A. 7, circular arc whippletree 8, space rope deposit cabin 9, becket bridle 10, rope bolt 11, space capsule head 12.
Described chassis propelling unit 2 is positioned at the bottom of manned space capsule 1, and described space capsule head 12 is positioned at the top of manned space capsule 1; Described chassis propelling unit 2 is connected with described rope bolt 11.In the time that described manned space capsule 1 is wanted Returning ball, described rope bolt 11 can separate with described chassis propelling unit 2 voluntarily, and the two ends of described space rope 6 are fixedly connected with two becket bridles 10 respectively, a described becket bridle 10 is enclosed within on described circular arc whippletree 8, another becket bridle 10 is enclosed within on described rope bolt 11, that is to say that the object that space rope connects all can depart from described chassis propelling unit 2 voluntarily, manned space capsule 1 and space capsule head 12 are pushed away earth 's orbit by chassis propelling unit 2, will automatic trip from manned space capsule 1, manned space capsule 1 and space capsule head 12 can be got back to the earth by universal gravitation.
Described chassis propelling unit 2 is positioned at the bottom of described manned space capsule 1, and the power of described chassis propelling unit 2 can promote described manned space capsule 1 from described manned space capsule 1 bottom, makes it change tracks, and last described manned space capsule 1 makes a return voyage.
Terrestrial time leaves when the manned spacecraft with gravitational load device in the lateral opening place that described removable cover 4 is positioned at space rope deposit cabin 9, in order to prevent that space rope 6 from scattering too early.And in the time thering is the manned spacecraft of gravitational load device and enter planned orbit, removable cover 4 meeting self fallings, described chassis propelling unit 2, manned space capsule 1, described space capsule head 12 can be voluntarily and the bunker 3 of gravity control device, space rope 6 is laid in cabin 9, the engine installation 5 of gravity control device separates, because described chassis propelling unit 2 is positioned at the bottom of manned space capsule 1, promote from behind manned space capsule 1 and accelerate with described space capsule head 12 speed separating, because described chassis propelling unit 2 is connected with described rope bolt 11, and the two ends of described space rope are fixedly connected with two becket bridles 10 respectively, a described becket bridle 10 is enclosed within on described circular arc whippletree 8, another becket bridle 10 is enclosed within on described rope bolt 11, so space rope 6 is due to the traction of described chassis propelling unit 2, pull-out from space rope deposit cabin 9.
The engine installation 5 of described gravity control device comprises two power systems, one is the power system that level advances, the effect of the power system that this level advances is: in the time that manned spacecraft will be transmitted in space, enough power can be provided, make manned spacecraft leave gravitational constraint; One is the rotary power system take S. A. 7 as axle center, is the power for the rotation of gravitational load device is provided.
The engine installation 5 of described gravity control device is fixedly connected on the bottom of the bunker 3 of described gravity control device, described space rope deposit cabin 9 and described S. A. 7; The two ends of described space rope 6 are fixedly connected with two becket bridles 10 respectively, and a described becket bridle 10 is enclosed within on described circular arc whippletree 8, and another becket bridle 10 is enclosed within on described rope bolt 11.
Such benefit is: described becket bridle 10 is enclosed within described circular arc whippletree 8, centripetal force is delivered to described circular arc whippletree 8 by described becket bridle 10, described circular arc whippletree 8 is fixed on point line position in described space rope deposit cabin 9 parallel with described S. A. 7, this position can make that centripetal force is even must be delivered on S. A. 7, and can not make S. A. 7 unbalance stress.
The bunker 3 of described gravity control device and described space rope deposit cabin 9 are round described S. A. 7.In the time that described S. A. 7 rotates, the bunker 3 of described gravity control device and described space rope deposit cabin 9 also can rotate thereupon and drive space rope 6 to drag described chassis propelling unit 2, manned space capsule 1, described space capsule head 12 to be rotated round S. A..The benefit of such design is: utilize manned space capsule 1 owing to rotating the centripetal force universal gravitation that replaces the earth to produce producing round S. A. 7.
Described space rope length is more than or equal to 24.85 meters.According to scientific experiment, in the time that cireular frequency reaches per minute and turns lower than 6, through 6 days to 8 days, people just can adapt to, and follow-up stop can not affect healthy and working ability.In the time that cireular frequency exceedes per minute 6 and turns, people just there will be disequilibrium.So angular velocity omega=(2*3.14*6)/60, therefore angular velocity omega should be controlled at below 0.628 radian per second.According to centripetal force formula F=mr ω
2, and gravity formulat is G=mg, and wherein F is centripetal force, the quality that m is object, and ω is cireular frequency, and r is radius of rotation, and G is gravity, and g is gravity coefficient.Make centripetal force replace gravity, namely make mr ω
2=mg, the m of both members, can approximately fall, i.e. r ω
2=g, again because of angular velocity omega=0.628 radian per second, g=9.8N/kg, 24.85 meters of r ≈, namely radius of rotation can not be less than 24.85 meters.Gravitational load device rotates slowlyer, and it is more comfortable that the astronaut in space capsule will feel, but according to centripetal force formula F=mr ω
2, and gravity formulat is G=mg, rotates slowlyer, and radius of rotation is just larger, and space rope 6 is just longer, and due to prior art, space rope 6 can not infinitely extend, the long easy fracture of space rope 6.
Described circular arc whippletree 8 is that such benefit is by the annulus take described S. A. 7 as the center of circle: in the time that S. A. 7 rotates, becket bridle 10 will slide on circular arc whippletree 8, and can not be wrapped in bunker 3 and the space rope deposit cabin 9 of gravity control device.
Described circular arc whippletree 8 is by the annulus take described S. A. 7 as the center of circle, intercepts 0 degree--45 degree parts form.Such benefit is: the space that can make the bunker 3 of gravity control device is 7 times of space rope deposit cabin 9, this ratio makes the bunker 3 of gravity control device have enough spaces to deposit solid fuel, and space rope deposit cabin 9 also has sufficient space to place space rope 6 simultaneously.
Claims (3)
1. a manned spacecraft with gravitational load device, is characterized in that: comprise manned space capsule (1), chassis propelling unit (2), the bunker (3) of gravity control device, removable cover (4), the engine installation (5) of gravity control device, space rope (6), S. A. (7), circular arc whippletree (8), space rope deposit cabin (9), becket bridle (10), rope bolt (11), space capsule head (12); Described chassis propelling unit (2) is positioned at the bottom of manned space capsule (1), and described space capsule head (12) is positioned at the top of manned space capsule (1); Described chassis propelling unit (2) is connected with described rope bolt (11); Described removable cover (4) is positioned at the lateral opening place in space rope deposit cabin (9); The engine installation (5) of described gravity control device is fixedly connected on the bottom of the bunker (3) of described gravity control device, described space rope deposit cabin (9) and described S. A. (7); The two ends of described space rope (6) are fixedly connected with two becket bridles (10) respectively, and it is upper that a described becket bridle (10) is enclosed within described circular arc whippletree (8), and another becket bridle (10) is enclosed within on described rope bolt (11).
2. a kind of manned spacecraft with gravitational load device according to claim 1, is characterized in that: described circular arc whippletree (8) is fixed on point line position in described space rope deposit cabin (9) parallel with described S. A. (7).
3. a kind of manned spacecraft with gravitational load device according to claim 1, is characterized in that: the bunker (3) of described gravity control device and described space rope deposit cabin (9) are round described S. A. (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410074280.0A CN103786896A (en) | 2014-03-03 | 2014-03-03 | Manned spacecraft with gravity loading device |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201410074280.0A CN103786896A (en) | 2014-03-03 | 2014-03-03 | Manned spacecraft with gravity loading device |
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| CN103786896A true CN103786896A (en) | 2014-05-14 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104071359A (en) * | 2014-06-11 | 2014-10-01 | 中国人民解放军第二炮兵装备研究院 | Space station for simulating ground gravity environment and using method |
| CN105947240A (en) * | 2016-05-26 | 2016-09-21 | 中国人民解放军第四军医大学 | Gravity cabin |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN87104891A (en) * | 1986-07-17 | 1988-03-30 | 休斯航空公司 | The method of the posture of rotator in the control track |
| US6206328B1 (en) * | 1998-11-09 | 2001-03-27 | Thomas C. Taylor | Centrifugal gravity habitation torus constructed of salvaged orbital debris |
| EP2161199A1 (en) * | 2008-09-03 | 2010-03-10 | Astrium GmbH | Holding and separation device for spacecraft |
| CN102616377A (en) * | 2012-04-05 | 2012-08-01 | 李海波 | Tai chi flying saucer |
-
2014
- 2014-03-03 CN CN201410074280.0A patent/CN103786896A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN87104891A (en) * | 1986-07-17 | 1988-03-30 | 休斯航空公司 | The method of the posture of rotator in the control track |
| US6206328B1 (en) * | 1998-11-09 | 2001-03-27 | Thomas C. Taylor | Centrifugal gravity habitation torus constructed of salvaged orbital debris |
| EP2161199A1 (en) * | 2008-09-03 | 2010-03-10 | Astrium GmbH | Holding and separation device for spacecraft |
| CN102616377A (en) * | 2012-04-05 | 2012-08-01 | 李海波 | Tai chi flying saucer |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104071359A (en) * | 2014-06-11 | 2014-10-01 | 中国人民解放军第二炮兵装备研究院 | Space station for simulating ground gravity environment and using method |
| CN104071359B (en) * | 2014-06-11 | 2016-03-30 | 中国人民解放军第二炮兵装备研究院 | The space station of simulation ground gravitational environment and using method |
| CN105947240A (en) * | 2016-05-26 | 2016-09-21 | 中国人民解放军第四军医大学 | Gravity cabin |
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Application publication date: 20140514 |