SU35578A1 - Aircraft landing device - Google Patents

Aircraft landing device

Info

Publication number
SU35578A1
SU35578A1 SU132798A SU132798A SU35578A1 SU 35578 A1 SU35578 A1 SU 35578A1 SU 132798 A SU132798 A SU 132798A SU 132798 A SU132798 A SU 132798A SU 35578 A1 SU35578 A1 SU 35578A1
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft
landing
aircraft landing
landing device
cable
Prior art date
Application number
SU132798A
Other languages
Russian (ru)
Inventor
М.В. Стародубцев
Original Assignee
М.В. Стародубцев
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 М.В. Стародубцев filed Critical М.В. Стародубцев
Priority to SU132798A priority Critical patent/SU35578A1/en
Application granted granted Critical
Publication of SU35578A1 publication Critical patent/SU35578A1/en

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Description

Предлагаемое устройство дл  посадки самолета состоит из двух тросовых лучей , укрепленных на столбах и сход щихс  своими средними част ми дл  затормаживани  самолета нри носадке. Дл  выхода и посадки пассажиров по сторонам тросовых лучей расположены платформы.The proposed aircraft landing device consists of two cable beams, mounted on poles and converging into their middle parts for slowing the aircraft into a nasal. Platforms are located on the sides of the cords for exiting and landing passengers.

На чертеже фиг. 1 изображает вид устройства сбоку; фиг. 2 - поперечный разрез устройства; фиг. 3 - вид устройства сверху.In FIG. 1 is a side view of the device; FIG. 2 is a cross section of the device; FIG. 3 shows the device from above.

Предлагаемое устройство (фиг. 1 - 3) состоит из двух тросовых лучей 1, укрепленных .при помощи Tiyr 3 на ,столбах 2. Означенные столбы, с целью затормаживани  самолета 4, сход тс  своими средними част ми. По сторонам тросовых лучей 1 расположены дл  выхода и йосадки пассажиров платформы 5, огражденные сетками б. На платформах 5 установлены вышки 7, внутри которых помещаютс  подъемные машины 8 дл  подъема и спуска вниз пассажиров и груза. Дл  освещени  посадочной площадки предназначены прожекторы 9, установленные на крышах вышек 7.The proposed device (Figs. 1–3) consists of two cable beams 1, fortified with Tiyr 3 on pillars 2. These poles, in order to slow down the aircraft 4, converge with their middle parts. On the sides of the cable 1 are located for the exit and passenger landing platform 5, fenced with nets b. On platforms 5, towers 7 are installed, inside of which lifting machines 8 are placed for lifting and lowering passengers and cargo. Spotlights 9 mounted on the roofs of towers 7 are designed to illuminate the landing area.

Причаливание самолета к предлагаемому устройству осуществл етс  приApproaching the aircraft to the proposed device is carried out at

помощи шасси, на распорках которого укрепл етс  пластинка 10, а по концам ее полуцилиндрические пластинки 11, изогнутые в разные стороны. При посредстве этих пластинок происходит приземление самолета.assistance to the chassis, on the struts of which the plate 10 is fastened, and at the ends of its semi-cylindrical plates 11, bent in different directions. With the help of these plates landing of the aircraft.

При посадке самолета последний спускаетс  над расширенной частью тросовых лучей 1 так, что пластинка 10 почти скользит по последним. Установившись на этой высоте, самолет входит в суженую часть площадки, и тогда тросовые лучи 1 вход т в цилиндрические пластинки 11 (при этом работа мотора останавливаетс ), вследствие чего происходит затормаживание самолета.When the aircraft lands, the latter descends over the extended part of the cord rays 1 so that the plate 10 almost slides over the latter. Having established at this height, the aircraft enters the constricted part of the platform, and then the cable rays 1 enter the cylindrical plates 11 (the motor stops working), as a result of which the aircraft is braked.

Предмет изобретени .The subject matter of the invention.

Устройство дл  - посадки самолета, отличающеев  тем, что оно состоит из двух тросовых лучей 1, укрепленных на столбах 2 и сход щихс  своими средними част ми дл  затормаживани  самолета при посадке, причем по сторонам тросовых лучей расположены платформы 5 дл  выхода и посадки пассажиров .A device for landing an aircraft, characterized in that it consists of two cable beams 1 fixed on pillars 2 and converging with their middle parts to decelerate the aircraft during landing, with platforms 5 for getting out and landing of passengers on the sides of the cable beams.

SU132798A 1933-07-30 1933-07-30 Aircraft landing device SU35578A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU132798A SU35578A1 (en) 1933-07-30 1933-07-30 Aircraft landing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU132798A SU35578A1 (en) 1933-07-30 1933-07-30 Aircraft landing device

Publications (1)

Publication Number Publication Date
SU35578A1 true SU35578A1 (en) 1934-03-31

Family

ID=48352273

Family Applications (1)

Application Number Title Priority Date Filing Date
SU132798A SU35578A1 (en) 1933-07-30 1933-07-30 Aircraft landing device

Country Status (1)

Country Link
SU (1) SU35578A1 (en)

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