SG11201908488WA - Method and system for decelerating and redirecting an airborne platform - Google Patents
Method and system for decelerating and redirecting an airborne platformInfo
- Publication number
- SG11201908488WA SG11201908488WA SG11201908488WA SG11201908488WA SG 11201908488W A SG11201908488W A SG 11201908488WA SG 11201908488W A SG11201908488W A SG 11201908488WA SG 11201908488W A SG11201908488W A SG 11201908488WA
- Authority
- SG
- Singapore
- Prior art keywords
- international
- drone
- rotor arm
- airfoils
- pct
- Prior art date
Links
- 230000008520 organization Effects 0.000 abstract 1
- 230000000717 retained effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D19/00—Non-canopied parachutes
- B64D19/02—Rotary-wing parachutes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/50—Glider-type UAVs, e.g. with parachute, parasail or kite
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
- B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
- G05D1/106—Change initiated in response to external conditions, e.g. avoidance of elevated terrain or of no-fly zones
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
- Prostheses (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Title: METHOD AND SYSTEM FOR DECELERATING AND REDIRECTING AN AIRBORNE PLATFORM (57) : The present invention provides a method for decelerat- 10 ing and redirecting an airborne platform, comprising the steps of retain- ing a flexible airfoil in non-deployed form in controllably releasable se- cured relation with each corresponding rotor arm of a multi-rotor drone; and upon detecting rate of descent of said drone in a first direction to 4b be greater than a predetermined value, triggering release of one or more of said retained airfoils from said corresponding rotor arm and causing each of said released airfoils to be circumferentially displaced from a first rotor arm to a second rotor arm of said drone to occlude an adja- cent inter-arm region, wherein each of said circumferentially displaced airfoils generates a sufficient value of localized lift that causes said de- scending drone to change its direction of descent from said first direction to a second direction. W O 20 18/ 17 30 40 Al Fig. 1 (12) INTERNATIONAL APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (19) World Intellectual Property Organization International Bureau (43) International Publication Date 27 September 2018 (27.09.2018) WIP0 I PCT IiiimmomiolollmonolomolomilmomolioluovoimIE (10) International Publication Number WO 2018/173040 Al (51) International Patent Classification: B64D 19/02 (2006.01) G05D 1/10 (2006.01) (21) International Application Number: PCT/IL2018/050303 (22) International Filing Date: 15 March 2018 (15.03.2018) (25) Filing Language: English (26) Publication Language: English (30) Priority Data: 251342 22 March 2017 (22.03.2017) IL (71) Applicant: PARAZERO LTD. [IL/IL]; 30 Dov Hoz Street, 5555626 Kiryat Ono (IL). (72) Inventor: TSALIAH, Amir; 15/23 Mandel Zinger Street, 3498415 Haifa (IL). (74) Agent: CROITORO, Boaz et al.; LUZZATTO & LUZ- ZATTO, P.O. Box 5352, 8415202 Beer Sheva (IL). (81) Designated States (unless otherwise indicated, for every kind of national protection available): AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW. (84) Designated States (unless otherwise indicated, for every kind of regional protection available): ARIPO (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW), Eurasian (AM, AZ, BY, KG, KZ, RU, TJ, TM), European (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR), OAPI (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG). Declarations under Rule 4.17: — of inventorship (Rule 4.17(iv)) Published: with international search report (Art. 21(3))
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL251342A IL251342B (en) | 2017-03-22 | 2017-03-22 | Method and system for decelerating and redirecting an airborne platform |
PCT/IL2018/050303 WO2018173040A1 (en) | 2017-03-22 | 2018-03-15 | Method and system for decelerating and redirecting an airborne platform |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201908488WA true SG11201908488WA (en) | 2019-10-30 |
Family
ID=62454751
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201908488W SG11201908488WA (en) | 2017-03-22 | 2018-03-15 | Method and system for decelerating and redirecting an airborne platform |
Country Status (8)
Country | Link |
---|---|
US (1) | US20210129999A1 (en) |
EP (1) | EP3601053A4 (en) |
JP (1) | JP7097905B2 (en) |
CN (1) | CN110603194A (en) |
CA (1) | CA3057273A1 (en) |
IL (1) | IL251342B (en) |
SG (1) | SG11201908488WA (en) |
WO (1) | WO2018173040A1 (en) |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1615682A (en) * | 1926-06-08 | 1927-01-25 | Hugh S Clark | Aeroplane |
JP2001120848A (en) | 1999-10-25 | 2001-05-08 | Heikon Ryu | Safety device for radio-controlled model flying matter and radio-controlled model flying matter |
US7677491B2 (en) * | 2005-08-05 | 2010-03-16 | Raytheon Company | Methods and apparatus for airborne systems |
US9208689B2 (en) * | 2011-08-19 | 2015-12-08 | Aerovironment Inc. | Deep stall aircraft landing |
CN202464133U (en) | 2011-12-29 | 2012-10-03 | 航宇救生装备有限公司 | Flying squirrel clothes |
US8733706B1 (en) * | 2012-05-15 | 2014-05-27 | The United States of America as represented by the Administrator of the National Aeronautics & Space Administration (NASA) | Transformable and reconfigurable entry, descent and landing systems and methods |
CN203889066U (en) * | 2014-01-17 | 2014-10-22 | 刘晓琳 | Four-rotor aircraft provided with rotor membranes and capable of realizing tilting rotation of rotors |
US9613539B1 (en) * | 2014-08-19 | 2017-04-04 | Amazon Technologies, Inc. | Damage avoidance system for unmanned aerial vehicle |
CN104527976B (en) * | 2014-12-18 | 2016-11-09 | 中国民航大学 | The flexible rotor aircraft that verts of ala |
GB201509509D0 (en) | 2015-06-01 | 2015-07-15 | Imp Innovations Ltd | Aerial devices capable of controlled flight |
CN106428577A (en) | 2015-08-11 | 2017-02-22 | 张奎 | Retractable propeller type parachute |
KR101609103B1 (en) | 2015-08-27 | 2016-04-04 | 한국항공우주연구원 | Crash prevention drone |
CN105691606B (en) * | 2016-05-04 | 2018-10-16 | 北方民族大学 | A kind of the unmanned plane device and control method in high cruise duration |
FR3062881B1 (en) * | 2017-02-15 | 2019-03-15 | Safran Helicopter Engines | METHOD AND SYSTEM FOR CONTROLLING AN EMERGENCY DEVICE |
CN106950986A (en) * | 2017-03-24 | 2017-07-14 | 西安旋飞电子科技有限公司 | A kind of obstacle detector of unmanned plane |
-
2017
- 2017-03-22 IL IL251342A patent/IL251342B/en active IP Right Grant
-
2018
- 2018-03-15 CA CA3057273A patent/CA3057273A1/en active Pending
- 2018-03-15 WO PCT/IL2018/050303 patent/WO2018173040A1/en unknown
- 2018-03-15 US US16/492,327 patent/US20210129999A1/en not_active Abandoned
- 2018-03-15 EP EP18771183.3A patent/EP3601053A4/en active Pending
- 2018-03-15 JP JP2019551441A patent/JP7097905B2/en active Active
- 2018-03-15 SG SG11201908488W patent/SG11201908488WA/en unknown
- 2018-03-15 CN CN201880020223.0A patent/CN110603194A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
WO2018173040A1 (en) | 2018-09-27 |
JP2020511356A (en) | 2020-04-16 |
EP3601053A1 (en) | 2020-02-05 |
CA3057273A1 (en) | 2018-09-27 |
IL251342B (en) | 2019-12-31 |
CN110603194A (en) | 2019-12-20 |
JP7097905B2 (en) | 2022-07-08 |
IL251342A0 (en) | 2017-06-29 |
US20210129999A1 (en) | 2021-05-06 |
EP3601053A4 (en) | 2020-12-30 |
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