RU2018138692A3 - - Google Patents

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Publication number
RU2018138692A3
RU2018138692A3 RU2018138692A RU2018138692A RU2018138692A3 RU 2018138692 A3 RU2018138692 A3 RU 2018138692A3 RU 2018138692 A RU2018138692 A RU 2018138692A RU 2018138692 A RU2018138692 A RU 2018138692A RU 2018138692 A3 RU2018138692 A3 RU 2018138692A3
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RU
Russia
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RU2018138692A
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Russian (ru)
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RU2722650C2 (en
RU2018138692A (en
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Priority to RU2018138692A priority Critical patent/RU2722650C2/en
Publication of RU2018138692A3 publication Critical patent/RU2018138692A3/ru
Publication of RU2018138692A publication Critical patent/RU2018138692A/en
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Publication of RU2722650C2 publication Critical patent/RU2722650C2/en

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RU2018138692A 2018-11-02 2018-11-02 Apparatus for inspecting helicopter rotors in uncontrolled rotation mode RU2722650C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2018138692A RU2722650C2 (en) 2018-11-02 2018-11-02 Apparatus for inspecting helicopter rotors in uncontrolled rotation mode

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2018138692A RU2722650C2 (en) 2018-11-02 2018-11-02 Apparatus for inspecting helicopter rotors in uncontrolled rotation mode

Publications (3)

Publication Number Publication Date
RU2018138692A3 true RU2018138692A3 (en) 2020-05-12
RU2018138692A RU2018138692A (en) 2020-05-12
RU2722650C2 RU2722650C2 (en) 2020-06-02

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ID=70734674

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2018138692A RU2722650C2 (en) 2018-11-02 2018-11-02 Apparatus for inspecting helicopter rotors in uncontrolled rotation mode

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RU (1) RU2722650C2 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU375510A1 (en) * 1971-04-05 1973-03-23 LIBRARY
FR2683504A1 (en) * 1991-11-07 1993-05-14 Aerospatiale Anti-torque system with rear rotor for a helicopter
RU2158908C1 (en) * 1999-06-09 2000-11-10 Рогов Анатолий Павлович Full-scale test rig for testing flying vehicles
CN106525404B (en) * 2016-11-30 2018-09-07 中国直升机设计研究所 A kind of tail-rotor platform

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Publication number Publication date
RU2722650C2 (en) 2020-06-02
RU2018138692A (en) 2020-05-12

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20201103