SU330714A1 - Elastic enclosure of the air cushion of the aircraft - Google Patents
Elastic enclosure of the air cushion of the aircraftInfo
- Publication number
- SU330714A1 SU330714A1 SU1341817A SU1341817A SU330714A1 SU 330714 A1 SU330714 A1 SU 330714A1 SU 1341817 A SU1341817 A SU 1341817A SU 1341817 A SU1341817 A SU 1341817A SU 330714 A1 SU330714 A1 SU 330714A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- air cushion
- aircraft
- sections
- enclosure
- stability
- Prior art date
Links
Landscapes
- Tires In General (AREA)
Description
Изобретение относитс к авиационной технике и может быть использованно на аппаратах с воздушной подушкой дл взлета посадки , передвижени по грунту, а также другого назначени .The invention relates to aeronautical engineering and can be used on air cushion vehicles for take-off landing, moving on the ground, as well as for other purposes.
Известны эластичные ограждени полости воздушной подушки летательного аппарата, содержащие надувные неразъемные меридианальные секции с параллельным подводом сжатого воздуха из кольцевого канала.Elastic enclosures of the air cushion of an aircraft are known, which contain inflatable one-piece meridian sections with parallel supply of compressed air from the annular channel.
Известные ограждени недостаточно устойчивы при действии вертикальной нагрузки в процессе посадки летательного аппарата и не обеспечивают достаточной стабильности пол давлений в полости воздушной подушки при приземлении и при движении аппарата по грунту.Known fences are not sufficiently stable under the action of a vertical load during the landing process of the aircraft and do not provide sufficient stability of the pressure floor in the cavity of the air cushion during landing and when the vehicle is moving along the ground.
Дл повышени устойчивости ограждени при посадке летательного аппарата и повышени стабильности пол давлений в полости воздушной подушки при движении аппарата по грунту предлагаемое ограждение выполнено To increase the stability of the fence when landing the aircraft and to increase the stability of the floor pressure in the cavity of the air cushion when the vehicle moves on the ground, the proposed fence is made
из горизонтально расположенных тороидальных секций, скрепленных между собой легкоразъемными соединени ми, внутренние полости секций последовательно сообщены разъемными соединительными патрубками, а нижн секци снабжена сменным протектором из износостойкого ворсистого материала.from horizontally located toroidal sections fastened to each other by easily detachable joints, the internal cavities of the sections are sequentially connected by detachable connecting pipes, and the lower section is provided with a replaceable tread made of wear-resistant fuzzy material.
На чертеже показано предложенное эластичное ограждение полости воздушной подушки .The drawing shows the proposed elastic enclosure cavity air cushion.
Горизонтально расположенные надувные тороидальные секции 1 .установлены, друг на друге и скрепленны между собой легкоразъемными соединени ми 2, в качестве которых могут быть использованы замок-застежка , замок-молни , шнуровка посредством петель. Между секци ми смонтированы разъемные соединительные патрубки 3, с помошью которых внутренние полости секций 1 последовательно сообщены между собой .Horizontally located inflatable toroidal sections 1. Are mounted one on another and fastened together by easily detachable joints 2, in which quality can be used fastener lock, zipper lock, lacing by means of loops. Between the sections, detachable connecting pipes 3 are mounted, with the help of which the internal cavities of sections 1 are successively connected to each other.
К нижней секции посредством легкоразъ емного соединени прикреплен сменный протектор 4 из износоустойчивого ворсистого материала.A removable tread 4 of wear-resistant fuzzy material is attached to the lower section by means of an easily detachable joint.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1341817A SU330714A1 (en) | 1969-06-06 | 1969-06-06 | Elastic enclosure of the air cushion of the aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1341817A SU330714A1 (en) | 1969-06-06 | 1969-06-06 | Elastic enclosure of the air cushion of the aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
SU330714A1 true SU330714A1 (en) | 1976-08-25 |
Family
ID=20446283
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1341817A SU330714A1 (en) | 1969-06-06 | 1969-06-06 | Elastic enclosure of the air cushion of the aircraft |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU330714A1 (en) |
-
1969
- 1969-06-06 SU SU1341817A patent/SU330714A1/en active
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