SU470725A1 - Copier support for aircraft landing gear testing - Google Patents

Copier support for aircraft landing gear testing

Info

Publication number
SU470725A1
SU470725A1 SU1640561A SU1640561A SU470725A1 SU 470725 A1 SU470725 A1 SU 470725A1 SU 1640561 A SU1640561 A SU 1640561A SU 1640561 A SU1640561 A SU 1640561A SU 470725 A1 SU470725 A1 SU 470725A1
Authority
SU
USSR - Soviet Union
Prior art keywords
support
landing gear
aircraft landing
frame
runway
Prior art date
Application number
SU1640561A
Other languages
Russian (ru)
Inventor
Михаил Семенович Данилов
Виктор Михайлович Дмитриев
Айзик Яковлевич Рябой
Original Assignee
Предприятие П/Я В-2616
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 Предприятие П/Я В-2616 filed Critical Предприятие П/Я В-2616
Priority to SU1640561A priority Critical patent/SU470725A1/en
Application granted granted Critical
Publication of SU470725A1 publication Critical patent/SU470725A1/en

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  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Description

ос м Х; У; Z (Р-,, P,j, Р) определ ютс  углом ai и углом 02 клиньев 12.os m x; W; Z (P-, P, j, P) are determined by the angle ai and the angle 02 of the wedges 12.

Предмет нзобретенн Subject matter

Claims (2)

1. Опорное устройство к копру дл  пспытапи  шасси летательиых аппаратов, содержащее раму и св занный с ней имитатор взлетно-посадочиой полосы, включающий тела качени  и оиирающуюс  на них плиту, на которую сбрасываетс  испытуемое изделие, отличающеес  тем, что, с целью повышени 1. A support device for a scraper for testing chassis of flying vehicles, comprising a frame and a runway strip simulator associated with it, including rolling elements and a slab supported on them, on which the test article is being dropped, characterized in that, in order to increase точности воспроизведени  эксплуатационных нагрузок, имитатор взлетно-посадочной полосы св зан с рамой с возможностью установки его под углом к горизонтальной плоскости .the accuracy of the reproduction of operational loads; the simulator of the runway is connected to the frame with the possibility of installing it at an angle to the horizontal plane. 2. Устройство по п. 1, отличающеес  тем, что имитатор взлетно-посадочной полосы снабжен опорной плитой, шарппрно св занной с рамой и образующей совместно с телами качени  и плитой, на которую сбрасываетс  испытуемое изделие, плоскую опору качени .2. A device according to claim 1, characterized in that the simulator of the runway is provided with a support plate, which is associated with the frame and forms together with the rolling elements and the plate on which the test article is dropped, a flat rolling support. I - --ф- Ье -ф-фI - - f-bе-ф-ф
SU1640561A 1971-03-22 1971-03-22 Copier support for aircraft landing gear testing SU470725A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1640561A SU470725A1 (en) 1971-03-22 1971-03-22 Copier support for aircraft landing gear testing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1640561A SU470725A1 (en) 1971-03-22 1971-03-22 Copier support for aircraft landing gear testing

Related Child Applications (1)

Application Number Title Priority Date Filing Date
SU904798054A Addition SU1728692A2 (en) 1990-03-05 1990-03-05 Device to test tightness of gas-filled articles

Publications (1)

Publication Number Publication Date
SU470725A1 true SU470725A1 (en) 1975-05-15

Family

ID=20470672

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1640561A SU470725A1 (en) 1971-03-22 1971-03-22 Copier support for aircraft landing gear testing

Country Status (1)

Country Link
SU (1) SU470725A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104142221A (en) * 2013-05-10 2014-11-12 中国直升机设计研究所 Device for driving helicopter wheel to rotate
CN106644347A (en) * 2017-01-16 2017-05-10 南京航空航天大学 Drop test device and drop test method of lander landing gear
CN110155367A (en) * 2019-05-29 2019-08-23 南京工业职业技术学院 A kind of aircraft main landing gear anti-impact force test device
CN111693309A (en) * 2020-05-13 2020-09-22 南京航空航天大学 Suspension releasing device for observing landing attitude change of lander and test method
CN113049207A (en) * 2021-03-30 2021-06-29 中国飞机强度研究所 Drop test device and method thereof

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104142221A (en) * 2013-05-10 2014-11-12 中国直升机设计研究所 Device for driving helicopter wheel to rotate
CN104142221B (en) * 2013-05-10 2016-10-19 中国直升机设计研究所 A kind of machine wheel rotating device
CN106644347A (en) * 2017-01-16 2017-05-10 南京航空航天大学 Drop test device and drop test method of lander landing gear
CN106644347B (en) * 2017-01-16 2019-04-19 南京航空航天大学 A kind of lander take-off and landing device drop test device and test method
CN110155367A (en) * 2019-05-29 2019-08-23 南京工业职业技术学院 A kind of aircraft main landing gear anti-impact force test device
CN111693309A (en) * 2020-05-13 2020-09-22 南京航空航天大学 Suspension releasing device for observing landing attitude change of lander and test method
US20230055684A1 (en) * 2020-05-13 2023-02-23 Nanjing University Of Aeronautics And Astronautics Suspending release device for observing drop vibration attitude changes of lander and test method
CN113049207A (en) * 2021-03-30 2021-06-29 中国飞机强度研究所 Drop test device and method thereof

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