RU2017103242A3 - - Google Patents

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Publication number
RU2017103242A3
RU2017103242A3 RU2017103242A RU2017103242A RU2017103242A3 RU 2017103242 A3 RU2017103242 A3 RU 2017103242A3 RU 2017103242 A RU2017103242 A RU 2017103242A RU 2017103242 A RU2017103242 A RU 2017103242A RU 2017103242 A3 RU2017103242 A3 RU 2017103242A3
Authority
RU
Russia
Application number
RU2017103242A
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Russian (ru)
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RU2017103242A (ru
RU2664024C2 (ru
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Publication date
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Priority to RU2017103242A priority Critical patent/RU2664024C2/ru
Publication of RU2017103242A publication Critical patent/RU2017103242A/ru
Publication of RU2017103242A3 publication Critical patent/RU2017103242A3/ru
Application granted granted Critical
Publication of RU2664024C2 publication Critical patent/RU2664024C2/ru

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/24—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with rotor blades fixed in flight to act as lifting surfaces

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
RU2017103242A 2017-01-31 2017-01-31 Беспилотный скоростной вертолет-самолет RU2664024C2 (ru)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2017103242A RU2664024C2 (ru) 2017-01-31 2017-01-31 Беспилотный скоростной вертолет-самолет

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2017103242A RU2664024C2 (ru) 2017-01-31 2017-01-31 Беспилотный скоростной вертолет-самолет

Publications (3)

Publication Number Publication Date
RU2017103242A RU2017103242A (ru) 2018-08-01
RU2017103242A3 true RU2017103242A3 (zh) 2018-08-01
RU2664024C2 RU2664024C2 (ru) 2018-08-14

Family

ID=63113018

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2017103242A RU2664024C2 (ru) 2017-01-31 2017-01-31 Беспилотный скоростной вертолет-самолет

Country Status (1)

Country Link
RU (1) RU2664024C2 (zh)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114018541A (zh) * 2021-09-26 2022-02-08 中国北方车辆研究所 一种适用于动态体系的全流场测量系统
CN116754174A (zh) * 2023-08-16 2023-09-15 中国空气动力研究与发展中心低速空气动力研究所 一种直升机风洞试验推力-拉力型尾桨的布局转换方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7665688B2 (en) * 2006-03-27 2010-02-23 The United States Of America As Represented By The Secretary Of The Navy Convertible aerial vehicle with contra-rotating wing/rotors and twin tilting wing and propeller units
RU2500578C1 (ru) * 2012-07-02 2013-12-10 Сергей Николаевич ПАВЛОВ Винтокрыл
US20140312177A1 (en) * 2013-04-18 2014-10-23 Rajesh Gaonjur Coaxial rotor/wing aircraft
RU141669U1 (ru) * 2014-01-24 2014-06-10 Закрытое Акционерное Общество "Транзас" Летательный аппарат вертикального взлета и посадки
US9896197B2 (en) * 2015-05-28 2018-02-20 Eugene H Vetter Devices and methods for in flight transition VTOL/fixed wing hybrid aircraft structures and flight modes

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114018541A (zh) * 2021-09-26 2022-02-08 中国北方车辆研究所 一种适用于动态体系的全流场测量系统
CN114018541B (zh) * 2021-09-26 2023-09-19 中国北方车辆研究所 一种适用于动态体系的全流场测量系统
CN116754174A (zh) * 2023-08-16 2023-09-15 中国空气动力研究与发展中心低速空气动力研究所 一种直升机风洞试验推力-拉力型尾桨的布局转换方法
CN116754174B (zh) * 2023-08-16 2023-10-31 中国空气动力研究与发展中心低速空气动力研究所 一种直升机风洞试验推力-拉力型尾桨的布局转换方法

Also Published As

Publication number Publication date
RU2017103242A (ru) 2018-08-01
RU2664024C2 (ru) 2018-08-14

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Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20190201