CN205044977U - Take parachute of aircraft - Google Patents
Take parachute of aircraft Download PDFInfo
- Publication number
- CN205044977U CN205044977U CN201520722508.2U CN201520722508U CN205044977U CN 205044977 U CN205044977 U CN 205044977U CN 201520722508 U CN201520722508 U CN 201520722508U CN 205044977 U CN205044977 U CN 205044977U
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- China
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- aircraft
- parachute
- state
- external power
- isolation layer
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Abstract
The utility model provides a take parachute of aircraft, characterized by includes parachute and a rotor craft, rotor craft of top trompil of parachute and seamless connection, the aircraft includes the electronic rotor of a plurality of, isolation layer, state of flight computer control system, power, external power source, remote controller and man -machine joint interface, and the isolation layer is a plane object, and state of flight computer control system includes satellite positioning terminal, accelerometer and communication module, the aircraft adopt a set of more than two with external power source with the power transmission line with electric loading component return circuit of aircraft. The utility model discloses can hover and the state that opens of parachute at any station keeping, conveniently implement the rescue to the high building personnel. Adopt a set of more than two with external power source with the power transmission line with electric loading component return circuit of aircraft makes external power source pass through the power transmission line and lasts the supply the aircraft electric energy can almost unrestrictedly strengthen the stagnant empty ability of aircraft.
Description
Technical field
The utility model 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
The purpose of this utility model keeps hovering under will providing the state that can open at parachute and carries out the parachute that loads.
The utility model 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, gyroscope; 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 the utility model band aircraft 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, gyroscope.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, magnetometer, baroceptor, aircraft described in gyroscope and communication module 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 |
|---|---|---|---|
| CN201520722508.2U CN205044977U (en) | 2015-09-18 | 2015-09-18 | Take parachute of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520722508.2U CN205044977U (en) | 2015-09-18 | 2015-09-18 | Take parachute of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205044977U true CN205044977U (en) | 2016-02-24 |
Family
ID=55338576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520722508.2U Expired - Fee Related CN205044977U (en) | 2015-09-18 | 2015-09-18 | Take parachute of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205044977U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108785881A (en) * | 2018-07-02 | 2018-11-13 | 厦门大学 | The inflation Escape ball of lifting controllable |
-
2015
- 2015-09-18 CN CN201520722508.2U patent/CN205044977U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108785881A (en) * | 2018-07-02 | 2018-11-13 | 厦门大学 | The inflation Escape ball of lifting controllable |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160224 Termination date: 20170918 |