SU137405A1 - Hovercraft - Google Patents

Hovercraft

Info

Publication number
SU137405A1
SU137405A1 SU576881A SU576881A SU137405A1 SU 137405 A1 SU137405 A1 SU 137405A1 SU 576881 A SU576881 A SU 576881A SU 576881 A SU576881 A SU 576881A SU 137405 A1 SU137405 A1 SU 137405A1
Authority
SU
USSR - Soviet Union
Prior art keywords
machine
nozzles
air
overpressure
hovercraft
Prior art date
Application number
SU576881A
Other languages
Russian (ru)
Inventor
Г.С. Туркин
Original Assignee
Г.С. Туркин
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 Г.С. Туркин filed Critical Г.С. Туркин
Priority to SU576881A priority Critical patent/SU137405A1/en
Application granted granted Critical
Publication of SU137405A1 publication Critical patent/SU137405A1/en

Links

Description

Известны машины на воздушной подушке с вентил торами, создающими под днишем машины избыточное давление, с эластичными закрылками перед соплами. Однако в этих машинах имеет место перетекание воздуха из зоны избыточного давлени  в атмосферу.Air-cushioned machines are known with fans which create overpressure under the bottom of the machine, with elastic flaps in front of the nozzles. However, in these machines air overflows from the overpressure zone into the atmosphere.

Дл  устранени  этого недостатка в описываемой машине сопла расположены по периметру дниш,а машины и наклонены внутрь, а дл  улучшени  продольной и поперечной устойчивости дниш.е снабжено перегородками , раздел ющими зону избыточного давлени  на отсеки.To eliminate this drawback, in the described machine, the nozzles are arranged around the perimeter of the bottom, and the machines are tilted inwards, and to improve the longitudinal and lateral stability, the bottom is equipped with partitions dividing the overpressure zone into compartments.

На фиг. 1 схематически изображена машина, вид сбоку; на фиг. 2 - то же, вид снизу; на фиг. 3 - то же в поперечном разрезе.FIG. 1 shows a schematic side view of a machine; in fig. 2 - the same, bottom view; in fig. 3 - the same in cross section.

Вентил торы / нагнетают под днище 2 корпуса 5 машины воздух, который подаетс  через наклоненные внутрь сопла 4, расположенные по всему периметру днища. Перед соплами, с внешней стороны, размещены эластичные закрылки 5.Fans / pumps under the bottom 2 of the housing 5 of the machine air, which is supplied through the nozzle 4 inclined inside, located around the entire perimeter of the bottom. Elastic flaps 5 are placed in front of the nozzles, from the outside.

При таком расположении сопел и закрылков задерживаетс  перетекание воздуха из зоны избыточного давлени  в атмосферу.With this arrangement, the nozzles and flaps delay the flow of air from the overpressure zone to the atmosphere.

Зона избыточного давлени , образованна  соплами и днищем, разделена на отсеки эластичными перегородками 6, которые обеспечивают поперечна  и продольна  устойчивость машины.The overpressure zone formed by the nozzles and the bottom is divided into compartments by elastic partitions 6, which provide transverse and longitudinal stability of the machine.

Предмет изобретени Subject invention

1.Машина на воздушной подушке с вентил торами, создающимипод днищем машины избыточное давление, с эластичными закрылками перед соплами, отличающа с  тем, что дл  задержки перетекани  воздуха из зоны избыточного давлени  в атмосферу сопла расположены по периметру днища машины и наклонены внутрь.1. The machine on an air cushion with overpressure fans under the bottom of the machine, with elastic flaps in front of the nozzles, characterized in that, to delay the flow of air from the overpressure zone into the atmosphere, the nozzles are located around the bottom of the machine and are tilted inward.

2.Мащина на воздушной подушке по н. 1, отличающа с  тем, что дл  улучшени  продольной и поперечной устойчивости днище снабжено перегородками, раздел ющими зону избыточного давлени  на отсеки .2.Maschina air cushion on n. 1, characterized in that, in order to improve the longitudinal and lateral stability, the bottom is provided with partitions dividing the overpressure zone into compartments.

SU576881A 1953-10-08 1953-10-08 Hovercraft SU137405A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU576881A SU137405A1 (en) 1953-10-08 1953-10-08 Hovercraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU576881A SU137405A1 (en) 1953-10-08 1953-10-08 Hovercraft

Publications (1)

Publication Number Publication Date
SU137405A1 true SU137405A1 (en) 1960-11-30

Family

ID=48293618

Family Applications (1)

Application Number Title Priority Date Filing Date
SU576881A SU137405A1 (en) 1953-10-08 1953-10-08 Hovercraft

Country Status (1)

Country Link
SU (1) SU137405A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3249167A (en) * 1964-05-01 1966-05-03 Tibbetts Industries Air-lift vehicle and filament skirt therefor
US3254731A (en) * 1962-03-08 1966-06-07 Ford Motor Co Vehicle skirt element for ground effect vehicle
US3265141A (en) * 1961-10-18 1966-08-09 Martin Marietta Corp Ground effect machine employing recirculation and controlled distribution of lift

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3265141A (en) * 1961-10-18 1966-08-09 Martin Marietta Corp Ground effect machine employing recirculation and controlled distribution of lift
US3254731A (en) * 1962-03-08 1966-06-07 Ford Motor Co Vehicle skirt element for ground effect vehicle
US3249167A (en) * 1964-05-01 1966-05-03 Tibbetts Industries Air-lift vehicle and filament skirt therefor

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