SU362742A1 - PILON SUSPENSION OF AIRCRAFT ENGINE - Google Patents

PILON SUSPENSION OF AIRCRAFT ENGINE

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Publication number
SU362742A1
SU362742A1 SU1667669/23A SU1667669A SU362742A1 SU 362742 A1 SU362742 A1 SU 362742A1 SU 1667669/23 A SU1667669/23 A SU 1667669/23A SU 1667669 A SU1667669 A SU 1667669A SU 362742 A1 SU362742 A1 SU 362742A1
Authority
SU
USSR - Soviet Union
Prior art keywords
pylon
caisson
pilon
suspension
aircraft engine
Prior art date
Application number
SU1667669/23A
Other languages
Russian (ru)
Inventor
Е.И. Санков
Р.И. Рокитянский
Ф.Д. Репетюк
В.И. Абрамов
Original Assignee
Е.И. Санков
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 Е.И. Санков filed Critical Е.И. Санков
Priority to SU1667669/23A priority Critical patent/SU362742A1/en
Application granted granted Critical
Publication of SU362742A1 publication Critical patent/SU362742A1/en

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Abstract

Пилон подвески двигателя летательного аппарата, содержащий носовую, среднюю и хвостовую части, отличающийся тем, что, с целью увеличения жесткости конструкции и снижения ее веса, средняя часть пилона выполнена в виде кессона, образованного верхней и нижней балками, боковыми обшивками и рамами и связанного с задними узлами с помощью балки-подкоса, состоящей из поясов и стенки, образующих нижнюю балку кессона, причем передние и задние узлы соединены поясами, закрепленными на нижней обшивке крыла и передающими нагрузки с пилона на кессон крыла.The pylon of the engine mount of the aircraft, containing the nose, middle and tail parts, characterized in that, in order to increase the rigidity of the structure and reduce its weight, the middle part of the pylon is made in the form of a caisson formed by upper and lower beams, side skins and frames and associated with rear nodes using a beam-strut consisting of belts and walls forming the lower beam of the caisson, with the front and rear nodes connected by belts attached to the lower wing casing and transmitting loads from the pylon to the caisson of the wing la

SU1667669/23A 1971-05-31 1971-05-31 PILON SUSPENSION OF AIRCRAFT ENGINE SU362742A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1667669/23A SU362742A1 (en) 1971-05-31 1971-05-31 PILON SUSPENSION OF AIRCRAFT ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1667669/23A SU362742A1 (en) 1971-05-31 1971-05-31 PILON SUSPENSION OF AIRCRAFT ENGINE

Publications (1)

Publication Number Publication Date
SU362742A1 true SU362742A1 (en) 2004-11-20

Family

ID=60514761

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1667669/23A SU362742A1 (en) 1971-05-31 1971-05-31 PILON SUSPENSION OF AIRCRAFT ENGINE

Country Status (1)

Country Link
SU (1) SU362742A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2721958C2 (en) * 2015-09-24 2020-05-25 Иабора Индустриа Аэронаутика С.А. Aircraft engine pylon attachment to wing assembly
RU2729129C2 (en) * 2016-01-07 2020-08-04 Зе Боинг Компани Improved pylons of jet engines attachment

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2721958C2 (en) * 2015-09-24 2020-05-25 Иабора Индустриа Аэронаутика С.А. Aircraft engine pylon attachment to wing assembly
RU2729129C2 (en) * 2016-01-07 2020-08-04 Зе Боинг Компани Improved pylons of jet engines attachment

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