RU97101423A - FRONT PLANE CHASSIS BRACKET - Google Patents

FRONT PLANE CHASSIS BRACKET

Info

Publication number
RU97101423A
RU97101423A RU97101423/28A RU97101423A RU97101423A RU 97101423 A RU97101423 A RU 97101423A RU 97101423/28 A RU97101423/28 A RU 97101423/28A RU 97101423 A RU97101423 A RU 97101423A RU 97101423 A RU97101423 A RU 97101423A
Authority
RU
Russia
Prior art keywords
front plane
chassis bracket
vibration damper
axis
wheel fork
Prior art date
Application number
RU97101423/28A
Other languages
Russian (ru)
Other versions
RU2123961C1 (en
Inventor
В.И. Долгов
Н.Н. Горюнов
Н.В. Мухин
Original Assignee
Открытое акционерное общество "Авиационный комплекс им.С.В.Ильюшина"
Filing date
Publication date
Application filed by Открытое акционерное общество "Авиационный комплекс им.С.В.Ильюшина" filed Critical Открытое акционерное общество "Авиационный комплекс им.С.В.Ильюшина"
Priority to RU97101423A priority Critical patent/RU2123961C1/en
Priority claimed from RU97101423A external-priority patent/RU2123961C1/en
Application granted granted Critical
Publication of RU2123961C1 publication Critical patent/RU2123961C1/en
Publication of RU97101423A publication Critical patent/RU97101423A/en

Links

Claims (1)

Передняя опора шасси самолета, содержащая амортизационную стойку, шарнирно соединенную с конструкцией фюзеляжа и с вилкой колеса, и гаситель колебаний, отличающаяся тем, что амортизационная стойка выполнена в виде изогнутой пластины и снабжена дополнительной опорой, выполненной в виде плавающей подвески, жестко связанной с конструкцией фюзеляжа, при этом с вилкой колеса амортизационная стойка соединена посредством оси, жестко закрепленной на конце пластины, а гаситель колебаний выполнен в виде установленного на этой оси набора упругих элементов, опирающихся через промежуточную шайбу на фрикционную втулку, имеющую возможность перемещения вдоль оси.The front landing gear support of the aircraft, comprising a shock absorber pivotally connected to the fuselage structure and a wheel fork, and an vibration damper, characterized in that the shock strut is made in the form of a curved plate and is provided with an additional support made in the form of a floating suspension, rigidly connected with the fuselage structure wherein, the suspension strut is connected to the wheel fork by means of an axis rigidly fixed at the end of the plate, and the vibration damper is made in the form of a set of elastic elements resting via an intermediate friction washer on the hub having the ability to move along the axis.
RU97101423A 1997-01-29 1997-01-29 Aircraft nose undercarriage leg RU2123961C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97101423A RU2123961C1 (en) 1997-01-29 1997-01-29 Aircraft nose undercarriage leg

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97101423A RU2123961C1 (en) 1997-01-29 1997-01-29 Aircraft nose undercarriage leg

Publications (2)

Publication Number Publication Date
RU2123961C1 RU2123961C1 (en) 1998-12-27
RU97101423A true RU97101423A (en) 1999-02-20

Family

ID=20189491

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97101423A RU2123961C1 (en) 1997-01-29 1997-01-29 Aircraft nose undercarriage leg

Country Status (1)

Country Link
RU (1) RU2123961C1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2495999B (en) 2012-02-24 2013-11-13 Messier Dowty Ltd Landing gear
RU2582591C1 (en) * 2014-12-23 2016-04-27 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Spring for main landing gear light
CN107244412B (en) * 2017-06-12 2019-06-04 西北工业大学 It is a kind of for promoting the undercarriage plate spring structure of UAV Landing cushion performance
CN114148509B (en) * 2021-12-03 2023-12-22 中国特种飞行器研究所 Light-duty sport aircraft nose landing gear steering structure and assembly method thereof

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