RU94017618A - Combination vertical take-off and landing rotary-wing aircraft and method of conversion of rotary-wing flying vehicle into aircraft configuration - Google Patents
Combination vertical take-off and landing rotary-wing aircraft and method of conversion of rotary-wing flying vehicle into aircraft configurationInfo
- Publication number
- RU94017618A RU94017618A RU94017618/11A RU94017618A RU94017618A RU 94017618 A RU94017618 A RU 94017618A RU 94017618/11 A RU94017618/11 A RU 94017618/11A RU 94017618 A RU94017618 A RU 94017618A RU 94017618 A RU94017618 A RU 94017618A
- Authority
- RU
- Russia
- Prior art keywords
- aircraft
- rotary
- blade
- wing
- rotor
- Prior art date
Links
Landscapes
- Tires In General (AREA)
- Toys (AREA)
Abstract
FIELD: aeronautical engineering. SUBSTANCE: combination vertical take-off and landing aircraft possess properties of helicopter and aircraft. Method of conversion of rotary-wing flying vehicle into aircraft configuration makes it possible to exclude drag of main rotor at aircraft modes of flight. Combination vertical take-off and landing aircraft has all main components of aircraft and helicopter. It is made by single-rotor lay-out with steering rotor and tractor propeller and single-blade main rotor with mass balance weight. Conversion of combination vertical take-off and landing flying vehicle from rotary-wing configuration into aircraft configuration is effected in horizontal flight through bracing the blade and shifting it to feathered pitch followed by approach of blade and mass balance weight with fuselage; in course of approach, blade and mass balance weight get coupled with fuselage, thus forming common aerodynamic lines. EFFECT: enhanced reliability. 3 cl, 3 dwg
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU94017618A RU2092392C1 (en) | 1994-05-17 | 1994-05-17 | Method of conversion of rotary-wing aircraft into aeroplane configuration and combined vertical take-off and landing rotary-wing aircraft for realization of this method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU94017618A RU2092392C1 (en) | 1994-05-17 | 1994-05-17 | Method of conversion of rotary-wing aircraft into aeroplane configuration and combined vertical take-off and landing rotary-wing aircraft for realization of this method |
Publications (2)
Publication Number | Publication Date |
---|---|
RU94017618A true RU94017618A (en) | 1996-07-27 |
RU2092392C1 RU2092392C1 (en) | 1997-10-10 |
Family
ID=20155909
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU94017618A RU2092392C1 (en) | 1994-05-17 | 1994-05-17 | Method of conversion of rotary-wing aircraft into aeroplane configuration and combined vertical take-off and landing rotary-wing aircraft for realization of this method |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2092392C1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2810886C1 (en) * | 2023-06-13 | 2023-12-29 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Воронежский государственный технический университет" | Unmanned aerial vehicle |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2230688C1 (en) * | 2003-08-08 | 2004-06-20 | Демин Александр Павлович | Multi-purpose heavier-than-air flying vehicle |
FR2916418B1 (en) * | 2007-05-22 | 2009-08-28 | Eurocopter France | FAST HYBRID HELICOPTER WITH EXTENDABLE HIGH DISTANCE. |
FR2916419B1 (en) * | 2007-05-22 | 2010-04-23 | Eurocopter France | HIGH FREQUENCY FAST HYBRID HELICOPTER WITH OPTIMIZED SUSTENTATION ROTOR. |
RU2661277C1 (en) * | 2017-03-14 | 2018-07-13 | Дмитрий Сергеевич Дуров | Unmanned carrier-based convertible rotorcraft |
RU2653953C1 (en) * | 2017-06-01 | 2018-05-15 | Дмитрий Сергеевич Дуров | Unmanned high-speed helicopter-airplane |
RU2658736C1 (en) * | 2017-06-13 | 2018-06-22 | Дмитрий Сергеевич Дуров | Multirotor high-speed helicopter-aircraft |
RU2684160C1 (en) * | 2017-11-20 | 2019-04-04 | Дмитрий Сергеевич Дуров | Deck-based aircraft unmanned anti-submarine complex (dauac) |
RU2706295C2 (en) * | 2018-03-12 | 2019-11-15 | Дмитрий Сергеевич Дуров | Anti-ship missile system with flying rockets robot-carrier and method for use thereof |
-
1994
- 1994-05-17 RU RU94017618A patent/RU2092392C1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2810886C1 (en) * | 2023-06-13 | 2023-12-29 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Воронежский государственный технический университет" | Unmanned aerial vehicle |
Also Published As
Publication number | Publication date |
---|---|
RU2092392C1 (en) | 1997-10-10 |
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