FLIGHT VEHICLE
FIELD: transport. ^ SUBSTANCE: flight vehicle comprises body, two jet engines, two shock absorbers with outlets communicating with two outlets of shock absorber control unit outlets, cylinder, exhaust nozzle and two exhaust pipes. The body is rigidly coupled with the said shock absorber control unit...
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| creator | KIRILLOV NIKOLAJ ALEKSANDROVICH CHASOVSKOJ ALEKSANDR ABRAMOVICH |
| description | FIELD: transport. ^ SUBSTANCE: flight vehicle comprises body, two jet engines, two shock absorbers with outlets communicating with two outlets of shock absorber control unit outlets, cylinder, exhaust nozzle and two exhaust pipes. The body is rigidly coupled with the said shock absorber control unit and the cylinder, in its turn, rigidly coupled with two inflamed gas exhaust pipes. The first shock absorber is rigidly coupled with the body, in its turn, rigidly linked up with two jet engines. The second shock absorber is rigidly coupled with waste gas exhaust nozzle and furnished with two safety shock absorbers and plate with two ledges arranged between the first and second shock absorbers. The cylinder is provided with two recesses. The aforesaid ledges of the plates can shift along appropriate holes of exhaust pipes and move in compliance with the cylinder recesses. The said cylinder recesses accommodate safety shock absorbers arranged between plates ledges and auxiliary exhaust nozzles rigidly coupled with the cylinder recesses. The safety shock absorbers have outlets communicating with the third outlet of the shock absorbers control unit. ^ EFFECT: reduced overall dimensions. ^ 1 dwg |
| format | Patent |
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The body is rigidly coupled with the said shock absorber control unit and the cylinder, in its turn, rigidly coupled with two inflamed gas exhaust pipes. The first shock absorber is rigidly coupled with the body, in its turn, rigidly linked up with two jet engines. The second shock absorber is rigidly coupled with waste gas exhaust nozzle and furnished with two safety shock absorbers and plate with two ledges arranged between the first and second shock absorbers. The cylinder is provided with two recesses. The aforesaid ledges of the plates can shift along appropriate holes of exhaust pipes and move in compliance with the cylinder recesses. The said cylinder recesses accommodate safety shock absorbers arranged between plates ledges and auxiliary exhaust nozzles rigidly coupled with the cylinder recesses. 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The body is rigidly coupled with the said shock absorber control unit and the cylinder, in its turn, rigidly coupled with two inflamed gas exhaust pipes. The first shock absorber is rigidly coupled with the body, in its turn, rigidly linked up with two jet engines. The second shock absorber is rigidly coupled with waste gas exhaust nozzle and furnished with two safety shock absorbers and plate with two ledges arranged between the first and second shock absorbers. The cylinder is provided with two recesses. The aforesaid ledges of the plates can shift along appropriate holes of exhaust pipes and move in compliance with the cylinder recesses. The said cylinder recesses accommodate safety shock absorbers arranged between plates ledges and auxiliary exhaust nozzles rigidly coupled with the cylinder recesses. 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The body is rigidly coupled with the said shock absorber control unit and the cylinder, in its turn, rigidly coupled with two inflamed gas exhaust pipes. The first shock absorber is rigidly coupled with the body, in its turn, rigidly linked up with two jet engines. The second shock absorber is rigidly coupled with waste gas exhaust nozzle and furnished with two safety shock absorbers and plate with two ledges arranged between the first and second shock absorbers. The cylinder is provided with two recesses. The aforesaid ledges of the plates can shift along appropriate holes of exhaust pipes and move in compliance with the cylinder recesses. The said cylinder recesses accommodate safety shock absorbers arranged between plates ledges and auxiliary exhaust nozzles rigidly coupled with the cylinder recesses. The safety shock absorbers have outlets communicating with the third outlet of the shock absorbers control unit. ^ EFFECT: reduced overall dimensions. ^ 1 dwg</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; rus |
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| subjects | AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
| title | FLIGHT VEHICLE |
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