CN105173091A - Parachute with aircraft - Google Patents
Parachute with aircraft Download PDFInfo
- Publication number
- CN105173091A CN105173091A CN201510595104.6A CN201510595104A CN105173091A CN 105173091 A CN105173091 A CN 105173091A CN 201510595104 A CN201510595104 A CN 201510595104A CN 105173091 A CN105173091 A CN 105173091A
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- aircraft
- parachute
- external power
- control system
- power source
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Abstract
Disclosed is a parachute with an aircraft. The parachute with the aircraft is characterized by comprising a parachute body and the rotor aircraft. A hole is formed in the top of the parachute body, and the rotor aircraft is in seamless connection with the hole formed in the top of the parachute body. The aircraft comprises a plurality of electric rotors, an isolating layer, a flight state computer-control system, a power source, an external power source, a remote controller and a man-machine connecting interface. The isolating layer is a planar object. The flight state computer-control system comprises a satellite positioning terminal, an accelerometer and a communication module. Two or more power transmission lines which are combined with the external power source and a power utilization load of the aircraft to form a circuit are adopted by the aircraft. According to the invention, the parachute with the aircraft can maintain a suspension state and a stretched state of the parachute body at any position, and therefore persons in high buildings can be conveniently rescued. Due to the fact that two or more power transmission lines which are combined with the external power source and the power utilization load of the aircraft to form the circuit are adopted, the external power source can continuously supply electric energy to the aircraft through the power transmission lines, and the air-staying capacity of the aircraft can be enhanced in an almost unlimited mode.
Description
Technical field
The present invention relates to a kind of parachute with aircraft.
Background technology
Existing a kind of parachute, for alleviating speed when free-falling body lands, but keep hovering and moving lifting under its state can not opened at parachute, and its volume dislikes excessive sometimes for the purposes such as high-rise building life saving.
Summary of the invention
Keep hovering under the object of the invention is to provide the state can opened at parachute and carry out the parachute that loads.
The present invention realizes the technical scheme of its object: manufacture the parachute of a band aircraft, comprise parachute and a rotor craft, parachute top with center vertical pivot symmetric mode perforate, an edge seamless link rotor craft in hole; Described aircraft comprises several electronic rotors, isolation layer, state of flight computer control system, power supply, external power supply, remote controller and man-machine linkage interface, isolation layer is a plane object, the plane-parallel at isolation layer and rotor fin place and the distance from rotor fin place horizontal surface be no more than ± and 340 millimeters, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module; Described aircraft adopts one group more than two to form the power transmission line in loop with the electricity consumption load of external power supply and described aircraft.
A man-machine linkage interface be connected with state of flight computer control system signal can also be adopted; Man-machine linkage interface comprises earphone and microphone.
Parachute cable can also be made to be connected with the caged thing of below it; Caged thing can hold a people and contain handrail.
Rotor craft comprises a post and multiaxis rotor craft, and a post comprises single-blade and double-vane.
Beneficial effect: the parachute of band aircraft of the present invention can keep the open configuration of hovering and parachute in any position, conveniently implement rescue to high building personnel.Adopt one group more than two form the power transmission line in loop with the electricity consumption load of external power supply and described aircraft, make external power supply continue to supply described aircraft electric energy by power transmission line, almost unrestrictedly can strengthen the stagnant empty ability of described aircraft.
Accompanying drawing explanation
Fig. 1 is the fundamental diagram of the parachute of a band aircraft.
Fig. 2 is the top view of the parachute of a band aircraft.
Fig. 3 is the structural representation of the aircraft of the parachute of a band aircraft.
1. parachutes in figure; 2. aircraft; 3. center vertical pivot; 4. electronic rotor; 5. isolation layer; 6. external power supply; 7. remote controller; 8. man-machine linkage interface; 9. fin; 10. power transmission line; 11. choose high bar; 12. cables; 13. windows; 14. caged things; 15. handrails; 16. cushion pads; 17. retaining frames; 18. landing platforms.
Detailed description of the invention
Fig. 1 provides embodiment 1.
In embodiment 1, manufacture the parachute of a band aircraft, comprise parachute 1 and a multiaxis rotor craft 2, parachute 1 top with the perforate of center vertical pivot 3 symmetric mode, an edge seamless link multiaxis rotor craft 2 in hole; Aircraft 2 comprises several electronic rotor 4, isolation layer 5, state of flight computer control system, power supply, external power supply 6, remote controller 7 and man-machine linkage interfaces 8, isolation layer 5 is a plane object, isolation layer 5 with the plane-parallel at rotor fin 9 place and the distance from rotor fin 9 place horizontal surface be no more than ± 340 millimeters, the distance be preferably from rotor fin 9 place horizontal surface is no more than ± 100 millimeters.State of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module.Aircraft 2 adopts one group more than two to form the power transmission line 10 in loop with the electricity consumption load of external power supply 6 and aircraft 2.Power transmission line 10 chooses a high segment distance with choosing high bar 11.
In embodiment 1, the parachute of band aircraft near the window 13 of building, and regulates and all around position adjustments at the height realizing parachute within the specific limits under the state can opened at parachute 1.Parachute cable 2 is connected with the caged thing 14 of below it; Caged thing 14 can hold a people and contain handrail 15; Handrail 15 people is used from caged thing 14, to enter window 13 easily or transfer in caged thing 14 from window 13.Be a cushion pad 16 bottom caged thing 14, contribute to reducing the impact to human body when landing.Aircraft 2 is containing a lightweight retaining frame 17, and retaining frame adopts carbon fiber material to make, and is directly clashed into for the protection of aircraft.Man-machine linkage interface 8 comprises wireless headset and wireless microphone, and the vicinity being arranged on handrail 15 contacts for the people on parachute 1 and the external world.
Isolation layer 3 is close or be positioned at rotor fin place plane, makes an efficient maintenance meiobar on isolation layer 5 form a pulling force upwards to aircraft, thus obviously reduces the blast loss of rotor craft.Isolation layer 5 also contributes to the leak tightness keeping parachute 1.Landing platform 18 for parking the parachute of band aircraft between non-operational period.
Claims (3)
1. the parachute with aircraft, is characterized in that comprising parachute and a rotor craft, parachute top with center vertical pivot symmetric mode perforate, an edge seamless link rotor craft in hole; Described aircraft comprises several electronic rotors, isolation layer, state of flight computer control system, power supply, external power supply, remote controller and man-machine linkage interface, isolation layer is a plane object, the plane-parallel at isolation layer and rotor fin place and the distance from rotor fin place horizontal surface be no more than ± and 340 millimeters, state of flight computer control system comprises satellite positioning-terminal, accelerometer and communication module; Described aircraft adopts one group more than two to form the power transmission line in loop with the electricity consumption load of external power supply and described aircraft.
2., according to a kind of parachute with aircraft according to claim 1, it is characterized in that containing a man-machine linkage interface be connected with state of flight computer control system signal; Man-machine linkage interface comprises earphone and microphone.
3., according to a kind of parachute with aircraft described in claims 1 or 2, it is characterized in that parachute cable is connected with the caged thing of below it; Caged thing can hold a people and contain handrail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595104.6A CN105173091A (en) | 2015-09-18 | 2015-09-18 | Parachute with aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595104.6A CN105173091A (en) | 2015-09-18 | 2015-09-18 | Parachute with aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105173091A true CN105173091A (en) | 2015-12-23 |
Family
ID=54895675
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510595104.6A Withdrawn CN105173091A (en) | 2015-09-18 | 2015-09-18 | Parachute with aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105173091A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112972918A (en) * | 2021-03-02 | 2021-06-18 | 焦作大学 | High-rise building escape device for disabled people |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2242220Y (en) * | 1995-08-01 | 1996-12-11 | 赵春伟 | Portable aircraft withlifting and lowering function |
| CN2538668Y (en) * | 2001-07-31 | 2003-03-05 | 钟云川 | Fan power type parachute |
| CN201284013Y (en) * | 2008-10-27 | 2009-08-05 | 陆建收 | Automotive elevating umbrella |
| US20120152654A1 (en) * | 2010-12-15 | 2012-06-21 | Robert Marcus | Uav-delivered deployable descent device |
| KR20130002491A (en) * | 2011-06-29 | 2013-01-08 | 주식회사 네스앤텍 | Propelar tower and unmanned aerial vehicle having parachute |
| CN103144779A (en) * | 2012-11-30 | 2013-06-12 | 中国电子科技集团公司第七研究所 | Multi-rotor-wing unmanned aerial vehicle mooring system |
| US20130233964A1 (en) * | 2012-03-07 | 2013-09-12 | Aurora Flight Sciences Corporation | Tethered aerial system for data gathering |
| CN103463743A (en) * | 2013-09-16 | 2013-12-25 | 温雪峰 | Escape device for high altitude |
-
2015
- 2015-09-18 CN CN201510595104.6A patent/CN105173091A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2242220Y (en) * | 1995-08-01 | 1996-12-11 | 赵春伟 | Portable aircraft withlifting and lowering function |
| CN2538668Y (en) * | 2001-07-31 | 2003-03-05 | 钟云川 | Fan power type parachute |
| CN201284013Y (en) * | 2008-10-27 | 2009-08-05 | 陆建收 | Automotive elevating umbrella |
| US20120152654A1 (en) * | 2010-12-15 | 2012-06-21 | Robert Marcus | Uav-delivered deployable descent device |
| KR20130002491A (en) * | 2011-06-29 | 2013-01-08 | 주식회사 네스앤텍 | Propelar tower and unmanned aerial vehicle having parachute |
| US20130233964A1 (en) * | 2012-03-07 | 2013-09-12 | Aurora Flight Sciences Corporation | Tethered aerial system for data gathering |
| CN103144779A (en) * | 2012-11-30 | 2013-06-12 | 中国电子科技集团公司第七研究所 | Multi-rotor-wing unmanned aerial vehicle mooring system |
| CN103463743A (en) * | 2013-09-16 | 2013-12-25 | 温雪峰 | Escape device for high altitude |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112972918A (en) * | 2021-03-02 | 2021-06-18 | 焦作大学 | High-rise building escape device for disabled people |
| CN112972918B (en) * | 2021-03-02 | 2021-12-21 | 焦作大学 | High-rise building escape device for disabled people |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| CB02 | Change of applicant information |
Address after: 317500 Zhejiang province Wenling City Taiping Street South Road 109 Lane 9 Applicant after: Shi Kanchao Address before: 200336 Shanghai City, Changning District Xianxia Road, Lane 780 No. 38 Room 302 Applicant before: Shi Kanchao |
|
| COR | Change of bibliographic data | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20151223 |