CN202966660U - Safe high-speed flight bag device - Google Patents
Safe high-speed flight bag device Download PDFInfo
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- CN202966660U CN202966660U CN 201220448740 CN201220448740U CN202966660U CN 202966660 U CN202966660 U CN 202966660U CN 201220448740 CN201220448740 CN 201220448740 CN 201220448740 U CN201220448740 U CN 201220448740U CN 202966660 U CN202966660 U CN 202966660U
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Abstract
The utility model discloses a safe high-speed flight bag device which comprises an I-shaped human body fixing device, propellers, a slow descent parachute pack, a folded wing and an elastic air bag, wherein an embedded binding-mode binding device is arranged along the vertical direction of the I-shaped human body fixing device, and is used for fixing a pilot; two pilot manual control consoles are respectively arranged at the two sides of the waist of the binding device; the surrounding type elastic air bag is arranged around the binding device; the shoulders of the pilot are flushed with an upper cross beam of the I-shaped human body fixing device; the protruding slow descent parachute pack is taken as a machine head and is arranged in the middle of the upper cross beam; the two ducted propellers are respectively arranged at the two sides of the upper cross beam; the folded wing which extends downwards along the inclined direction is arranged in the middle of the I-shaped human body fixing device, so that the posture of a flight bag is more easily controlled, and a higher flight speed can be realized; and the safe high-speed flight bag device is high in safety.
Description
Technical field
The utility model relates to flight packet technology field, refers to that especially a kind of safe high-speed flight packing puts.
Background technology
Along with China spatial domain below 3000 meters will be all-round opening in 2015, the domestic inevitable great development that will welcome the General Aviation industry in future in 10 to 20 years.From the experience of developed country, spatial domain below 3000 meters is mainly take small aircraft as the flight theme." aerial motor " is exactly a kind of single Backpack type high degree of safety of folding wings small aircraft that can fly in spatial domain below 3000 meters.Can serve numerous airhogs at flight experience and the traffic trip in spatial domain below 3000 meters by actv..
The main type of drive of bag is the two cycle engine drive fans drive screw propeller by similar automobile but present " aerial motor " namely flies, the flight bag is unworthy of the standby host wing simultaneously, wayward in take-off attitude and landing attitude like this, also can't reach in flight course at a high speed.Because the speed of existing flight bag is also unhappy, so it is also paid little attention to security measures.
Summary of the invention
In view of this, the main purpose of the utility model embodiment is to provide a kind of safe high-speed flight packing to put, and can solve existing flight bag attitude wayward, and speed is slower, and the inadequate problem of safety.
For achieving the above object, the technical scheme of the utility model embodiment is achieved in that
The utility model provides a kind of safe high-speed flight packing to put, and this device comprises: the human body fixer of I shape, screw propeller, slow pack, folded wing and elastic bag fall, wherein,
On the vertical direction of the human body fixer of I shape, be provided with the binding apparatus of embedded tie-in mode, be used for fixedly aircrew, be provided with aircrew's hand held console in the waist both sides of binding apparatus, be provided with the elastic bag of enclosed in the surrounding of binding apparatus;
Aircrew's shoulder flushes with the upper beam of the human body fixer of I shape; Be provided with the outstanding slow pack that falls at the middle part of described upper beam as head;
Two culvert type propellers are equipped with in the both sides of described upper beam; The middle part of the human body fixer of I shape is provided with the folded wing of oblique downward-extension.
Wherein, the lower beam of the human body fixer of described I shape is provided with support, when being used for vertical takeoff and landing, propping up on the ground support integral flight packing and puts; The back that described flight packing is put also is provided with fuel tank.
Wherein, described two culvert type propellers are specially the two shrouded propellers of single-shot, and the injection direction of duct high velocity air adopts the vector control technology of duct axis direction three-dimensional variable.
Wherein, describedly slow fall pack, be specially outstanding circular arc, be used for the head flight course protection aircrew, when the flight bag runs out of steam or lands in an emergency, slowly fall pack and automatically open.
Wherein, described folded wing is specially: at the front opening wing that takes off, after landing, wing-folding is packed up.
Wherein, described elastic bag is used for opening the elastic bag of described enclosed when the flight bag runs out of steam or lands in an emergency.
A kind of safe high-speed flight packing that the utility model embodiment provides is put, this device comprises: the human body fixer of I shape, screw propeller, slow pack, folded wing and the elastic bag of falling, wherein, on the vertical direction of the human body fixer of I shape, be provided with the binding apparatus of embedded tie-in mode, be used for fixedly aircrew, be provided with aircrew's hand held console in the waist both sides of binding apparatus, be provided with the elastic bag of enclosed in the surrounding of binding apparatus; Aircrew's shoulder flushes with the upper beam of the human body fixer of I shape; Be provided with the outstanding slow pack that falls at the middle part of described upper beam as head; Two culvert type propellers are equipped with in the both sides of described upper beam; The middle part of the human body fixer of I shape is provided with the folded wing of oblique downward-extension, makes the attitude of flight bag more easy to control, and can realize higher flying speed, possesses simultaneously very high safety.
Description of drawings
Fig. 1 is the structural representation that a kind of safe high-speed flight packing of the utility model is put.
The specific embodiment
The basic thought of the utility model embodiment is: for the flight bag adds slow fall pack, wing and elastic bag.
Below by drawings and the specific embodiments, the utility model embodiment is described in further detail again.
The utility model embodiment provides a kind of picture frame device of quick-replaceable picture, Fig. 1 is the structural representation that a kind of safe high-speed flight packing of the utility model is put, as shown in Figure 1, this device comprises: the human body fixer 11 of I shape, screw propeller 12, slow pack 13, folded wing 14 and the elastic bag 15 of falling, wherein
On the vertical direction of the human body fixer 11 of I shape, be provided with the binding apparatus of embedded tie-in mode, be used for fixedly aircrew, be provided with aircrew's hand held console in the waist both sides of binding apparatus, be provided with the elastic bag 15 of enclosed in the surrounding of binding apparatus;
Aircrew's shoulder flushes with the upper beam of the human body fixer of I shape 11; Be provided with the outstanding slow pack 13 that falls at the middle part of described upper beam as head;
Two culvert type propellers 12 are equipped with in the both sides of described upper beam; The middle part of the human body fixer 11 of I shape is provided with the folded wing 14 of oblique downward-extension.
Concrete, described two culvert type propellers 12 are specially the two shrouded propellers of single-shot, and the injection direction of duct high velocity air adopts the vector control technology of duct axis direction three-dimensional variable.So not only can guarantee flying power, can also be when screw propeller of appearance stop in the air, the kinetic force of another screw propeller is guaranteed the aircraft stable landing.
Describedly slow fall pack 13 and be specially outstanding circular arc, be used for the head flight course protection aircrew, when the flight bag runs out of steam or lands in an emergency, slowly fall pack 13 and automatically open.Two equal et out of orders of culvert type propeller 12 can guarantee like this aircraft when 150 meters and above height, if can utilize slow pack 13 emergency landings that fall.
Described folded wing 14 is specially: at the front opening wing that takes off, after landing, wing-folding is packed up.Concrete folding mode can design as required targetedly.
Described elastic bag 15 is used for opening the elastic bag 15 of described enclosed when the flight bag runs out of steam or lands in an emergency.To prevent that pack from not opening fully or to delay and fall the highly not enough injury that the aircrew is caused.
Further, the lower beam of the human body fixer 11 of described I shape is provided with support, when being used for vertical takeoff and landing, propping up on the ground support integral flight packing and puts; The back that described flight packing is put also is provided with fuel tank.
Power system of the present utility model adopts high pressure charging/high atomization technology, and output per litre is near 150 horsepowers.Culvert type propeller will reduce watt loss.The vector control technology of the injection direction employing duct axis direction three-dimensional variable of duct high velocity air is guaranteed in flight and the control of the squareness in landing stage and takes off to fly to flat, and the flight attitude of putting down when flying to landing translate phase and air mobile is controlled.
Flight control system of the present utility model: take off and the flight attitude in the stage of landing is controlled by controlling the duct axis direction and controlled, creeping/descending in flight course/turn to and other air maneuvers are completed jointly by culvert type propeller and wing.
Fax of the present utility model and communication system: except normal flight and controlling, communication and flight parameter center will concentrate on Helmet Mounted Display.Communication and answering system are guaranteed the instant messaging with ground and air control.Airborne hand radar is provided by the anti-collision early warning that mainly provides in 10km.
The above; it is only preferred embodiment of the present utility model; be not be used to limiting protection domain of the present utility model, all any modifications of doing within spirit of the present utility model and principle, be equal to and replace and improvement etc., within all should being included in protection domain of the present utility model.
Claims (4)
1. the high-speed flight of safety packing is put, and it is characterized in that, this device comprises: the human body fixer of I shape, screw propeller, slow pack, folded wing and elastic bag fall, wherein,
On the vertical direction of the human body fixer of I shape, be provided with the binding apparatus of embedded tie-in mode, be used for fixedly aircrew, be provided with aircrew's hand held console in the waist both sides of binding apparatus, be provided with the elastic bag of enclosed in the surrounding of binding apparatus;
Aircrew's shoulder flushes with the upper beam of the human body fixer of I shape; Be provided with the outstanding slow pack that falls at the middle part of described upper beam as head;
Two culvert type propellers are equipped with in the both sides of described upper beam; The middle part of the human body fixer of I shape is provided with the folded wing of oblique downward-extension.
2. device according to claim 1, is characterized in that, the lower beam of the human body fixer of described I shape is provided with support, when being used for vertical takeoff and landing, propping up on the ground support integral flight packing and put; The back that described flight packing is put also is provided with fuel tank.
3. device according to claim 1 and 2, is characterized in that, described two culvert type propellers are specially the two shrouded propellers of single-shot, and the injection direction of duct high velocity air adopts the vector control technology of duct axis direction three-dimensional variable.
4. device according to claim 1 and 2, is characterized in that, describedly slow falls pack, is specially outstanding circular arc, is used for the head flight course protection aircrew, when the flight bag runs out of steam or lands in an emergency, slowly falls pack and automatically open.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220448740 CN202966660U (en) | 2012-09-05 | 2012-09-05 | Safe high-speed flight bag device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220448740 CN202966660U (en) | 2012-09-05 | 2012-09-05 | Safe high-speed flight bag device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202966660U true CN202966660U (en) | 2013-06-05 |
Family
ID=48507768
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220448740 Expired - Fee Related CN202966660U (en) | 2012-09-05 | 2012-09-05 | Safe high-speed flight bag device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202966660U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018209911A1 (en) * | 2017-05-16 | 2018-11-22 | 华南理工大学 | Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system |
| CN112334386A (en) * | 2018-04-17 | 2021-02-05 | 拉兹万·萨比耶 | Personal flight device for vertical takeoff and landing |
-
2012
- 2012-09-05 CN CN 201220448740 patent/CN202966660U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018209911A1 (en) * | 2017-05-16 | 2018-11-22 | 华南理工大学 | Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system |
| US11634222B2 (en) | 2017-05-16 | 2023-04-25 | South China University Of Technology | Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system |
| CN112334386A (en) * | 2018-04-17 | 2021-02-05 | 拉兹万·萨比耶 | Personal flight device for vertical takeoff and landing |
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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 |
Granted publication date: 20130605 Termination date: 20180905 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |