FIELD: lighter-than-air flying vehicles. SUBSTANCE: proposed device has pneumatically strained envelope filled with air and made for change of density of air both by change of volume of envelope and amount of air contained in it. Pneumatic strain of envelope is ensured by tension of it on spiral structure formed by kevlar stiffeners. EFFECT: enhanced safety and reliability. 3 cl, 7 dwg, 3 ex
Title | Year | Author | Number |
---|---|---|---|
UNBALLASTED AEROSTATIC FLYING VEHICLE | 1997 |
|
RU2126342C1 |
DEVICE FOR INJECTION OF SATELLITE INTO ORBIT | 1996 |
|
RU2117610C1 |
SEMIRIGID CONTROLLABLE AEROSTATIC FLYING VEHICLE | 1994 |
|
RU2114027C1 |
HYBRID AIRCRAFT | 1996 |
|
RU2160689C2 |
METHOD FOR STIFFENING AIRSHIPE SHELL WITH SEMI-RIGID STRUCTURE | 2020 |
|
RU2763322C1 |
METHOD AND DEVICE FOR MULTIPLE LAUNCHING TO SPACE AND RETURN OF OVERSIZED CARGO AND METHOD OF USE OF OVERSIZED CARGO ON OTHER PLANETS | 2012 |
|
RU2627902C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2742496C2 |
SERPENT-LIKE AIRCRAFT | 1992 |
|
RU2005649C1 |
MULTILAYER AEROSTATIC SHELL, FILLED WITH ELECTRONS | 2007 |
|
RU2376195C2 |
CONTROLLABLE AEROSTATIC FLYING CRANE | 1995 |
|
RU2098318C1 |
Authors
Dates
2004-03-10—Published
2001-06-13—Filed