RU96103171A - NON-BALLAST AEROSTATIC AIRCRAFT - Google Patents

NON-BALLAST AEROSTATIC AIRCRAFT

Info

Publication number
RU96103171A
RU96103171A RU96103171/11A RU96103171A RU96103171A RU 96103171 A RU96103171 A RU 96103171A RU 96103171/11 A RU96103171/11 A RU 96103171/11A RU 96103171 A RU96103171 A RU 96103171A RU 96103171 A RU96103171 A RU 96103171A
Authority
RU
Russia
Prior art keywords
ballast
aerostatic
aerostatic aircraft
shells
aircraft
Prior art date
Application number
RU96103171/11A
Other languages
Russian (ru)
Original Assignee
Зайдель Р.М.
Filing date
Publication date
Application filed by Зайдель Р.М. filed Critical Зайдель Р.М.
Publication of RU96103171A publication Critical patent/RU96103171A/en

Links

Claims (1)

Аэростатический летательный аппарат выполнен в виде пневмонапряженной конструкции замкнутой формы, наружная и внутренняя оболочки которой соединены поперечными связями, отличающийся тем, что жесткость конструкции обеспечивается закачиванием легкого несущего газа под избыточным давлением в пространство между оболочками, а регулирование аэростатической подъемной силы производится изменением массы воздуха во внутреннем объеме конструкции.The aerostatic aircraft is made in the form of a closed-circuit pneumatic tension structure, the outer and inner shells of which are connected by transverse connections, characterized in that the structural rigidity is provided by pumping a light carrier gas under excessive pressure into the space between the shells, and aerostatic lifting force is controlled by changing the air mass in the inner scope of construction.
RU96103171/11A 1996-02-19 NON-BALLAST AEROSTATIC AIRCRAFT RU96103171A (en)

Publications (1)

Publication Number Publication Date
RU96103171A true RU96103171A (en) 1998-04-27

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