SU1716709A1 - VIEWING WINDOW OF AIRCRAFT DOOR - Google Patents

VIEWING WINDOW OF AIRCRAFT DOOR

Info

Publication number
SU1716709A1
SU1716709A1 SU4493684/23A SU4493684A SU1716709A1 SU 1716709 A1 SU1716709 A1 SU 1716709A1 SU 4493684/23 A SU4493684/23 A SU 4493684/23A SU 4493684 A SU4493684 A SU 4493684A SU 1716709 A1 SU1716709 A1 SU 1716709A1
Authority
SU
USSR - Soviet Union
Prior art keywords
viewing window
door
perimeter
aircraft door
glasses
Prior art date
Application number
SU4493684/23A
Other languages
Russian (ru)
Inventor
Д.Ф. Воронков
А.Ф. Гречишко
В.Т. Жвакин
Ю.Г. Зезера
В.И. Комаров
Original Assignee
Авиационный научно-технический комплекс им. А.Н.Туполева
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 Авиационный научно-технический комплекс им. А.Н.Туполева filed Critical Авиационный научно-технический комплекс им. А.Н.Туполева
Priority to SU4493684/23A priority Critical patent/SU1716709A1/en
Application granted granted Critical
Publication of SU1716709A1 publication Critical patent/SU1716709A1/en

Links

Abstract

Смотровое окно двери летательного аппарата, содержащее наружное и внутреннее стекла, установленные соответственно в вырезах, выполненных в наружной и внутренней обшивках двери, с помощью эластичных окантовок, при этом одно из стекол выполнено в виде клина с вершиной, контактирующей с верхней кромкой выреза, а между стеклами по их периметру установлен тубус, закрепленный на одной из обшивок двери, отличающееся тем, что, с целью повышения удобства и безопасности при аварийной высадке пассажиров за счет расширения зоны обзора местности, внутренний вырез выполнен большим по площади и смещен вверх относительно наружного выреза, в котором и установлено выполненное в виде клина стекло, при этом закрепленный между стеклами тубус выполнен по форме усеченного конуса с большим основанием, примыкающим к внутреннему стеклу по его периметру.Viewing window of the aircraft door, containing outer and inner glasses, installed respectively in cutouts made in the outer and inner door linings, using elastic edging a tube mounted on one of the door trims is installed around the perimeter, characterized in that, in order to increase convenience and safety during an emergency disembarkation of passengers by expanding the area of view, The cutout is large and offset upward relative to the outside cutout, in which the wedge-shaped glass is installed, while the tube fixed between the glasses is made in the shape of a truncated cone with a large base adjacent to the inside glass around its perimeter.

SU4493684/23A 1988-10-14 1988-10-14 VIEWING WINDOW OF AIRCRAFT DOOR SU1716709A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4493684/23A SU1716709A1 (en) 1988-10-14 1988-10-14 VIEWING WINDOW OF AIRCRAFT DOOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4493684/23A SU1716709A1 (en) 1988-10-14 1988-10-14 VIEWING WINDOW OF AIRCRAFT DOOR

Publications (1)

Publication Number Publication Date
SU1716709A1 true SU1716709A1 (en) 2002-02-20

Family

ID=60532398

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4493684/23A SU1716709A1 (en) 1988-10-14 1988-10-14 VIEWING WINDOW OF AIRCRAFT DOOR

Country Status (1)

Country Link
SU (1) SU1716709A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2711946C2 (en) * 2015-11-10 2020-01-23 Эмбраер С.А. Devices and methods of reconfiguring aircraft fuselage doors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2711946C2 (en) * 2015-11-10 2020-01-23 Эмбраер С.А. Devices and methods of reconfiguring aircraft fuselage doors

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