GEP19991787BGEAP19984276AGEAP1998004276AGEP19991787BGE P19991787 BGEP19991787 BGE P19991787BGE AP19984276 AGEAP19984276 AGE AP19984276AGE AP1998004276 AGEAP1998004276 AGE AP1998004276AGE P19991787 BGEP19991787 BGE P19991787B
Authority
GE
Georgia
Prior art keywords
helicopter
nozzles
processor
control
turbine
Prior art date
Application number
GEAP19984276A
Inventor
Omar Bilonashvili
Original Assignee
Omar Bilonashvili
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Omar BilonashvilifiledCriticalOmar Bilonashvili
Priority to GEAP19984276ApriorityCriticalpatent/GEP19991787B/en
Publication of GEP19991787BpublicationCriticalpatent/GEP19991787B/en
Increase of helicopter maneuverability. 2. Essence A helicopter comprises a body 1, a rotor 2, a gas turbine 3, a processor 4 of on-board control, horizontally disposed nozzles 5, vertically disposed nozzles 6, the angle between the nozzles makes 85-90°, in respect to the shank axis - 85-90°. It also contains a turbine and between the nozzles a regulator-distributor 7 of gas jets, connected with the control processor 4. 3. Field of Application Helicopter control systems. 3 fig.
Life for the lifting-body[blunt nose cone asymmetric wingless craft capable of supersonic and hypersonic flight between Earth and the Freedom space station]