CA2776121A1 - Aeronef a rotor coaxial/ailes - Google Patents

Aeronef a rotor coaxial/ailes Download PDF

Info

Publication number: CA2776121A1
Authority: CA; Canada
Prior art keywords: rotor; wings; wing; aircraft; fuselage
Prior art date: 2012-04-30
Legal status (The legal status 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 status listed.): Abandoned

Application number

CA2776121A

Other languages

English (en)

Inventor

Gaonjur Rajesh

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Individual

Original Assignee

Individual

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.)

2012-04-30

Filing date

2012-04-30

Publication date

2013-10-30

2012-04-30 Application filed by Individual filed Critical Individual

2012-04-30 Priority to CA2776121A priority Critical patent/CA2776121A1/fr

2013-10-30 Publication of CA2776121A1 publication Critical patent/CA2776121A1/fr

Status Abandoned legal-status Critical Current

Links

230000007704 transition Effects 0.000 claims abstract description 63
230000005540 biological transmission Effects 0.000 claims description 30
239000003381 stabilizer Substances 0.000 claims description 20
241000272517 Anseriformes Species 0.000 claims description 14
230000000368 destabilizing effect Effects 0.000 claims description 8
238000006243 chemical reaction Methods 0.000 abstract description 13
238000000034 method Methods 0.000 abstract description 4
230000001360 synchronised effect Effects 0.000 abstract description 4
230000005484 gravity Effects 0.000 description 13
230000007246 mechanism Effects 0.000 description 12
230000008901 benefit Effects 0.000 description 8
239000000446 fuel Substances 0.000 description 5
230000009467 reduction Effects 0.000 description 4
230000002829 reductive effect Effects 0.000 description 4
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230000002441 reversible effect Effects 0.000 description 3
230000003068 static effect Effects 0.000 description 3
238000004873 anchoring Methods 0.000 description 2
230000008878 coupling Effects 0.000 description 2
238000010168 coupling process Methods 0.000 description 2
238000005859 coupling reaction Methods 0.000 description 2
241000238633 Odonata Species 0.000 description 1
230000009471 action Effects 0.000 description 1
230000000712 assembly Effects 0.000 description 1
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125000004122 cyclic group Chemical group 0.000 description 1
238000013016 damping Methods 0.000 description 1
230000001419 dependent effect Effects 0.000 description 1
230000009977 dual effect Effects 0.000 description 1
239000002828 fuel tank Substances 0.000 description 1
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230000002452 interceptive effect Effects 0.000 description 1
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238000004513 sizing Methods 0.000 description 1

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
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
- 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
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
- 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
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors

Landscapes

Engineering & Computer Science (AREA)
Mechanical Engineering (AREA)
Aviation & Aerospace Engineering (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Transmission Devices (AREA)

CA2776121A 2012-04-30 2012-04-30 Aeronef a rotor coaxial/ailes Abandoned CA2776121A1 (fr)

Priority Applications (1)

Application Number	Priority Date	Filing Date	Title
CA2776121A CA2776121A1 (fr)	2012-04-30	2012-04-30	Aeronef a rotor coaxial/ailes

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
CA2776121A CA2776121A1 (fr)	2012-04-30	2012-04-30	Aeronef a rotor coaxial/ailes

Publications (1)

Publication Number	Publication Date
CA2776121A1 true CA2776121A1 (fr)	2013-10-30

Family

ID=49510707

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CA2776121A Abandoned CA2776121A1 (fr)	2012-04-30	2012-04-30	Aeronef a rotor coaxial/ailes

Country Status (1)

Country	Link
CA (1)	CA2776121A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US10464668B2 (en)	2015-09-02	2019-11-05	Jetoptera, Inc.	Configuration for vertical take-off and landing system for aerial vehicles
US10875658B2 (en)	2015-09-02	2020-12-29	Jetoptera, Inc.	Ejector and airfoil configurations
US11001378B2 (en)	2016-08-08	2021-05-11	Jetoptera, Inc.	Configuration for vertical take-off and landing system for aerial vehicles
US11148801B2 (en)	2017-06-27	2021-10-19	Jetoptera, Inc.	Configuration for vertical take-off and landing system for aerial vehicles
CN115107430A (zh) *	2022-07-25	2022-09-27	朱上翔	一种单叶双桨共轴旋翼的垂直起降飞行汽车

2012
- 2012-04-30 CA CA2776121A patent/CA2776121A1/fr not_active Abandoned

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US10464668B2 (en)	2015-09-02	2019-11-05	Jetoptera, Inc.	Configuration for vertical take-off and landing system for aerial vehicles
US10875658B2 (en)	2015-09-02	2020-12-29	Jetoptera, Inc.	Ejector and airfoil configurations
US11001378B2 (en)	2016-08-08	2021-05-11	Jetoptera, Inc.	Configuration for vertical take-off and landing system for aerial vehicles
US11148801B2 (en)	2017-06-27	2021-10-19	Jetoptera, Inc.	Configuration for vertical take-off and landing system for aerial vehicles
CN115107430A (zh) *	2022-07-25	2022-09-27	朱上翔	一种单叶双桨共轴旋翼的垂直起降飞行汽车

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Legal Events

Date	Code	Title	Description
2016-06-13	FZDE	Discontinued	Effective date: 20160502