WO2003033344A3 - Vertical lift flying craft with suspended payload - Google Patents
Vertical lift flying craft with suspended payload Download PDFInfo
- Publication number
- WO2003033344A3 WO2003033344A3 PCT/US2002/003007 US0203007W WO03033344A3 WO 2003033344 A3 WO2003033344 A3 WO 2003033344A3 US 0203007 W US0203007 W US 0203007W WO 03033344 A3 WO03033344 A3 WO 03033344A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- unit
- lift
- payload
- flying craft
- vertical lift
- Prior art date
Links
- 230000002411 adverse Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 239000000725 suspension Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
- B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
- B64C17/04—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by pendular bodies
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
- B64C31/036—Hang-glider-type aircraft; Microlight-type aircraft having parachute-type wing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Vibration Prevention Devices (AREA)
Abstract
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02706116A EP1441946A2 (en) | 2001-10-12 | 2002-01-31 | Vertical lift flying craft |
AU2002240223A AU2002240223A1 (en) | 2001-10-12 | 2002-01-31 | Vertical lift flying craft with suspended payload |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/976,348 US6783096B2 (en) | 2001-01-31 | 2001-10-12 | Vertical lift flying craft |
US09/976,348 | 2001-10-12 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2003033344A2 WO2003033344A2 (en) | 2003-04-24 |
WO2003033344A3 true WO2003033344A3 (en) | 2003-11-06 |
Family
ID=25524008
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2002/003007 WO2003033344A2 (en) | 2001-10-12 | 2002-01-31 | Vertical lift flying craft with suspended payload |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1441946A2 (en) |
AU (1) | AU2002240223A1 (en) |
RU (1) | RU2004114833A (en) |
WO (1) | WO2003033344A2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8328130B2 (en) | 2008-12-08 | 2012-12-11 | Honeywell International Inc. | Vertical take off and landing unmanned aerial vehicle airframe structure |
JP6213713B2 (en) | 2013-05-16 | 2017-10-18 | 株式会社Ihi | Vertical take-off and landing aircraft |
US9550567B1 (en) | 2014-10-27 | 2017-01-24 | Amazon Technologies, Inc. | In-flight reconfigurable hybrid unmanned aerial vehicle |
US11299267B2 (en) * | 2019-07-29 | 2022-04-12 | Ryan Evaristo Pinto | Electric powered paraglider |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2448392A (en) * | 1946-04-04 | 1948-08-31 | John C Quady | Convertible type aircraft |
US3113747A (en) * | 1959-12-23 | 1963-12-10 | Stanley W Smith | Tug aircraft combination |
US3211429A (en) * | 1963-07-17 | 1965-10-12 | Frank H Steward | Means and method of hoisting cargo |
US4116405A (en) * | 1977-03-28 | 1978-09-26 | Grumman Aerospace Corporation | Airplane |
US5188313A (en) * | 1992-01-03 | 1993-02-23 | Piasecki Aircraft Corporation | Glider aircraft tow control system |
-
2002
- 2002-01-31 AU AU2002240223A patent/AU2002240223A1/en not_active Abandoned
- 2002-01-31 RU RU2004114833/11A patent/RU2004114833A/en not_active Application Discontinuation
- 2002-01-31 EP EP02706116A patent/EP1441946A2/en not_active Withdrawn
- 2002-01-31 WO PCT/US2002/003007 patent/WO2003033344A2/en not_active Application Discontinuation
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2448392A (en) * | 1946-04-04 | 1948-08-31 | John C Quady | Convertible type aircraft |
US3113747A (en) * | 1959-12-23 | 1963-12-10 | Stanley W Smith | Tug aircraft combination |
US3211429A (en) * | 1963-07-17 | 1965-10-12 | Frank H Steward | Means and method of hoisting cargo |
US4116405A (en) * | 1977-03-28 | 1978-09-26 | Grumman Aerospace Corporation | Airplane |
US5188313A (en) * | 1992-01-03 | 1993-02-23 | Piasecki Aircraft Corporation | Glider aircraft tow control system |
Also Published As
Publication number | Publication date |
---|---|
RU2004114833A (en) | 2005-04-27 |
WO2003033344A2 (en) | 2003-04-24 |
AU2002240223A1 (en) | 2003-04-28 |
EP1441946A2 (en) | 2004-08-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN205480075U (en) | Cloud platform damping device and unmanned aerial vehicle | |
WO2008105851A3 (en) | Lenticular airship | |
JP4803509B1 (en) | Horizontal attitude stabilization device for disk-type flying object | |
EP1511671A4 (en) | Control of an aircraft as a thrust-vectored pendulum in vertical, horizontal and all flight transitional modes thereof | |
FR2877312B1 (en) | METHOD AND DEVICE FOR IMPROVING THE BRAKING EFFICIENCY OF A FLYING AIRCRAFT ON THE GROUND | |
WO2005072255A3 (en) | Stabilizing surface for flight deck or other uses | |
CN204477173U (en) | A kind of damping device for holder for aerial photographing | |
CN107298178A (en) | Unmanned plane relieving mechanism and fixed-wing unmanned plane and its method that takes off vertically | |
WO2003033344A3 (en) | Vertical lift flying craft with suspended payload | |
CN207595275U (en) | Unmanned plane damper mechanism | |
CN205078695U (en) | A damping device for on multiaxis aircraft | |
CN209455023U (en) | Bolt retaining mechanism | |
CA2106227A1 (en) | Space frame structure with widened base for supporting offshore platform | |
CN110550220B (en) | Aerial photography unmanned aerial vehicle with falling protection function | |
WO2001065136A3 (en) | Apparatus for semi-active isolation of payloads with low transmissibility | |
JPS6463500A (en) | Method and device for producing state of fine gravity in gravity field | |
KR200489054Y1 (en) | Flight Attitude For Education | |
CN217268270U (en) | Assembled suspended ceiling leveling system | |
CN211935553U (en) | Electromagnetic suspension device for amusement | |
CN209956241U (en) | Support structure suitable for flight device and helicopter | |
CN113264189A (en) | Commodity circulation unmanned aerial vehicle convenient to keep balance | |
CN206544601U (en) | A kind of goods and materials carrying platform of unmanned plane | |
CN206437228U (en) | A kind of buffer device of unmanned vehicle | |
CN204916209U (en) | Platform carrier for unmanned aerial vehicle | |
CN211724657U (en) | Electromagnetic suspension device for amusement |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A2 Designated state(s): AE AG AL AM AT AU AZ BA BB BG BY BZ CA CH CN CO CR CU CZ DE DM DZ EC EE ES FI GB GD GE GH HR HU ID IL IN IS JP KE KG KP KR LC LK LR LS LT LU LV MA MD MG MN MW MX MZ NO NZ OM PH PL PT RU SD SE SG SI SK SL TJ TM TN TR TZ UA UG US UZ VN YU ZA ZM |
|
AL | Designated countries for regional patents |
Kind code of ref document: A2 Designated state(s): GH GM KE LS MW MZ SD SL SZ UG ZM ZW AM AZ BY KG KZ RU TJ TM AT BE CH CY DE DK FI FR GB GR IE IT LU MC NL PT SE TR BF BJ CF CG CI CM GA GN GQ ML MR NE SN TD TG |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
WWE | Wipo information: entry into national phase |
Ref document number: 2002706116 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 2002706116 Country of ref document: EP |
|
NENP | Non-entry into the national phase |
Ref country code: JP |
|
WWW | Wipo information: withdrawn in national office |
Country of ref document: JP |
|
WWW | Wipo information: withdrawn in national office |
Ref document number: 2002706116 Country of ref document: EP |