FIELD: aviation.
SUBSTANCE: invention relates to aeronautics. Airship according to the first version is characterised by that body is composed of interconnected groups of carriers and cargo frame modules fixed on load-carrying platform and form a cellular structure. Internal volume of each bearing module is filled with hollow shell with gas. Internal volume of each cargo module is divided into two functional parts. Top functional part is filled with hollow shell with gas, and lower functional part is not filled. Lower functional parts of adjacent cargo modules, which are not filled, form a cargo compartment inside body. In airship according to a second version, body is formed by interconnected groups of carriers and cargo frame modules which form a cellular structure in lower part of which are fixed segments of carrying platform, connected to each other. Internal volume of each carrier module is filled with hollow shell with gas, and inner volume of each cargo module is divided into two functional parts. Top functional part is filled with hollow shell with gas, and lower functional part is not filled. Lower functional parts of adjacent cargo modules, which are not filled, form a cargo compartment inside body. Airship according to first and second versions of invention comprises additional group of carrier modules mounted on outer side of main frame and forming an external cellular structure with streamlined shape. External streamlined cellular structure consists of internal modules with trapezoidal cross-section and external modules with triangular cross-section. Airship shell is formed by outer walls of covers of modules, reinforced with an additional frame and attached to each other. Comprises angular streamlined modules. Comprises cargo door closed by flap-ramp.
EFFECT: group of inventions is aimed at improvement of manufacturability due to increased variability of possible configurations of planning configurations, higher reliability and convenience in operation.
12 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HIGH-CAPACITY UNIVERSAL VEHICLE (VERSIONS) | 2015 |
|
RU2585380C1 |
| SEMI-RIGID AEROSTATIC FLYING VEHICLE WITH VARIABLE-CONFIGURATION CASE | 1994 |
|
RU2070136C1 |
| AEROSTATIC APPARATUS | 2015 |
|
RU2612071C2 |
| AIRSHIP AND ITS DISC-SHAPED BODY | 2006 |
|
RU2317226C2 |
| NON-BALLAST AIRSHIP OF TRANSFORMABLE AERODYNAMIC CONFIGURATION AND MODULE ARTICULATION ROD CONSTRUCTION | 2003 |
|
RU2257311C2 |
| DISC-SHAPED AIRSHIP FRAME AND AIRSHIP CONTAINING SUCH FRAME | 2023 |
|
RU2820177C1 |
| DESIGN OF THE CARGO AREA OF AN AIRSHIP | 2021 |
|
RU2783321C1 |
| POWER UNIT OF AEROSTATIC MODULE OF TRANSPORT SYSTEM | 2021 |
|
RU2796433C2 |
| METHOD OF FLIGHT AND AIRCRAFT TO THIS END | 2009 |
|
RU2410284C1 |
| AIRSHIP MODULAR TRANSPORT SYSTEM | 2021 |
|
RU2787114C1 |
