CN107972858A - A kind of special aircraft - Google Patents
A kind of special aircraft Download PDFInfo
- Publication number
- CN107972858A CN107972858A CN201711276768.1A CN201711276768A CN107972858A CN 107972858 A CN107972858 A CN 107972858A CN 201711276768 A CN201711276768 A CN 201711276768A CN 107972858 A CN107972858 A CN 107972858A
- Authority
- CN
- China
- Prior art keywords
- telescopic rod
- placing
- motor
- motor apparatus
- rotor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000010276 construction Methods 0.000 claims abstract description 4
- 238000000034 method Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 230000001681 protective effect Effects 0.000 claims 1
- 238000005516 engineering process Methods 0.000 abstract description 4
- 230000007812 deficiency Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A kind of special aircraft, belongs to vehicle technology field, more particularly to a kind of special aircraft, including fuselage, rotor, telescopic rod, motor, ring protection shell, motor apparatus for placing and rack.It is furnished with control system and airborne equipment in the fuselage.The rotor fin is symmetrical and fin Windward angle can be adjusted between 15 30 degree.The telescopic rod is divided into interior bar and outer bar.The telescopic rod is distributed in fuselage both sides for hollow-core construction loop bar.The motor apparatus for placing is located at each telescopic rod outer end and agrees with.The motor apparatus for placing can rotate horizontally on telescopic rod.The motor is positioned on motor apparatus for placing.Interior smooth recessed structure can place rotor wing tip wherein the ring protection shell marginal center in a ring.A kind of special aircraft of the present invention, safety and stability, convenient control.
Description
Technical field
A kind of special aircraft, belongs to vehicle technology field, more particularly to a kind of special aircraft.
Background technology
Aircraft has come into the sight of people gradually with advances in technology, thus be widely used in exploration, agricultural,
The place of people's needs operation in the air in military, postal delivery, rescue and relief work and daily life, but traditional aircraft takeoff
Time takes longer, and not nimble, the narrow and small place that turns in the air is not easy into.
The content of the invention
The purpose of the present invention is overcoming the above-mentioned deficiency of traditional aircraft, it is simple to invent a kind of structure of convenient control
The higher special aircraft of efficiency.
A kind of special aircraft, including fuselage, rotor, telescopic rod, motor, ring protection shell, motor apparatus for placing and machine
Frame.
It is furnished with control system and airborne equipment in the fuselage.The rotor fin is symmetrical and can be between 15-30 degree
Adjust fin Windward angle.The telescopic rod is divided into interior bar and outer bar.The telescopic rod is distributed in fuselage for hollow-core construction loop bar
Both sides.The motor apparatus for placing is located at each telescopic rod outer end and agrees with.The motor apparatus for placing can on telescopic rod water
Flat rotation.The motor is positioned on motor apparatus for placing.The ring protection shell marginal center interior smooth recessed structure in a ring
Rotor wing tip can be placed wherein.
The working method of the special aircraft is:Special aircraft is gone up to the air operation after quickly taking off, in the air during deflecting
Motor apparatus for placing is rotatable to adjust direction, runs into narrow region by shrinking telescopic rod and reduces flight area.
A kind of special aircraft of the present invention, safety and stability, convenient control.
Brief description of the drawings
Fig. 1 is the schematic perspective view of special aircraft.
In figure, 1- fuselages, 2- rotors, 3- telescopic rods, 4- motors, 5- ring protection shells, 6- motor apparatus for placing, 7- machines
Frame.
Embodiment
The present invention is illustrated in conjunction with attached drawing, a kind of special aircraft, including fuselage 1, rotor 2, telescopic rod
3rd, motor 4, ring protection shell 5, motor apparatus for placing 6 and rack 7.
It is furnished with control system and airborne equipment in the fuselage 1.2 fin of rotor it is symmetrical and can 15-30 degree it
Between adjust fin Windward angle.The telescopic rod 3 divides for interior bar and outer bar.The telescopic rod 3 is distributed in for hollow-core construction loop bar
1 both sides of fuselage.4 apparatus for placing of motor is located at each 3 outer end of telescopic rod and agrees with.The motor apparatus for placing 6 can stretched
Rotated horizontally on contracting bar 3.The motor 4 is positioned on motor apparatus for placing 6.5 marginal center of ring protection shell is in a ring
Interior smooth recessed structure can place 5 wing tip of rotor wherein.
The working method of the special aircraft is:Special aircraft is gone up to the air operation after quickly taking off, in the air during deflecting
Motor apparatus for placing 6 is rotatable to adjust direction, runs into narrow region and passes through to contract and shrinks telescopic rod 3 and reduce flight area.
A kind of special aircraft of the present invention, safety and stability, is not easy to damage.
Claims (3)
- A kind of 1. special aircraft, it is characterised in that:Including fuselage(1), rotor(2), telescopic rod(3), motor(4), annular protect Protective case(5), motor apparatus for placing(6)And rack(7);The fuselage(1)It is interior to be furnished with control system and airborne equipment;The rotor (2)Fin is symmetrical and fin Windward angle can be adjusted between 15-30 degree;The telescopic rod(3)It is divided into interior bar and outer bar;Institute State telescopic rod(3)Fuselage is distributed in for hollow-core construction loop bar(1)Both sides;The motor apparatus for placing(6)Positioned at each telescopic rod (3)Simultaneously agree with outer end;The motor apparatus for placing(6)Can be in telescopic rod(3)Upper horizontal rotation;The motor(4)It is positioned over electricity Machine apparatus for placing(6)On;The ring protection shell(5)Interior smooth recessed structure can be by rotor in a ring for marginal center(2)Wing tip is put Put wherein.
- A kind of 2. special aircraft according to claim 1, it is characterised in that:Telescopic rod(3)It horizontal can shrink and stretch out.
- A kind of 3. special aircraft according to claim 1 or 2, it is characterised in that:Its working method is:Special flight Device goes up to the air operation after quickly taking off, in the air motor apparatus for placing during deflecting(6)It is rotatable to adjust direction, run into narrow area Domain is by shrinking telescopic rod(3)Reduce flight area.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711276768.1A CN107972858A (en) | 2017-12-06 | 2017-12-06 | A kind of special aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711276768.1A CN107972858A (en) | 2017-12-06 | 2017-12-06 | A kind of special aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107972858A true CN107972858A (en) | 2018-05-01 |
Family
ID=62009329
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201711276768.1A Withdrawn CN107972858A (en) | 2017-12-06 | 2017-12-06 | A kind of special aircraft |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107972858A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109018325A (en) * | 2018-08-14 | 2018-12-18 | 国网辽宁省电力有限公司辽阳供电公司 | A kind of ultra-high-tension power transmission line tour machine |
CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201800918U (en) * | 2010-09-16 | 2011-04-20 | 中国计量学院 | Rotating telescopic flying device with four rotor wings |
CN103419942A (en) * | 2013-09-10 | 2013-12-04 | 北京臻迪科技有限公司 | Unmanned aerial vehicle |
CN204297097U (en) * | 2014-11-26 | 2015-04-29 | 成都好飞机器人科技有限公司 | For four rotor wing unmanned aerial vehicles that agriculture Pesticides sprays |
CN204406208U (en) * | 2015-03-04 | 2015-06-17 | 杨昊林 | A kind of quadrotor of patrolling and examining for street lamp |
CN204507269U (en) * | 2015-03-27 | 2015-07-29 | 马鞍山市赛迪智能科技有限公司 | A kind of unmanned plane tackling airborne aircraft |
CN105905291A (en) * | 2016-06-04 | 2016-08-31 | 刘海涛 | Multi-rotor craft with tilting rotors |
CN205738086U (en) * | 2016-05-13 | 2016-11-30 | 梅家崎 | A kind of rotor craft propeller protective cover and rotor craft |
CN206186713U (en) * | 2016-09-30 | 2017-05-24 | 潍坊歌尔电子有限公司 | Amphibious unmanned vehicles |
CN206367591U (en) * | 2016-12-25 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of many rotor mechanisms of unmanned plane |
CN107323192A (en) * | 2017-06-21 | 2017-11-07 | 北京理工大学 | A kind of air-ground amphibious mobile robot |
-
2017
- 2017-12-06 CN CN201711276768.1A patent/CN107972858A/en not_active Withdrawn
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201800918U (en) * | 2010-09-16 | 2011-04-20 | 中国计量学院 | Rotating telescopic flying device with four rotor wings |
CN103419942A (en) * | 2013-09-10 | 2013-12-04 | 北京臻迪科技有限公司 | Unmanned aerial vehicle |
CN204297097U (en) * | 2014-11-26 | 2015-04-29 | 成都好飞机器人科技有限公司 | For four rotor wing unmanned aerial vehicles that agriculture Pesticides sprays |
CN204406208U (en) * | 2015-03-04 | 2015-06-17 | 杨昊林 | A kind of quadrotor of patrolling and examining for street lamp |
CN204507269U (en) * | 2015-03-27 | 2015-07-29 | 马鞍山市赛迪智能科技有限公司 | A kind of unmanned plane tackling airborne aircraft |
CN205738086U (en) * | 2016-05-13 | 2016-11-30 | 梅家崎 | A kind of rotor craft propeller protective cover and rotor craft |
CN105905291A (en) * | 2016-06-04 | 2016-08-31 | 刘海涛 | Multi-rotor craft with tilting rotors |
CN206186713U (en) * | 2016-09-30 | 2017-05-24 | 潍坊歌尔电子有限公司 | Amphibious unmanned vehicles |
CN206367591U (en) * | 2016-12-25 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of many rotor mechanisms of unmanned plane |
CN107323192A (en) * | 2017-06-21 | 2017-11-07 | 北京理工大学 | A kind of air-ground amphibious mobile robot |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109018325A (en) * | 2018-08-14 | 2018-12-18 | 国网辽宁省电力有限公司辽阳供电公司 | A kind of ultra-high-tension power transmission line tour machine |
CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
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: 20180501 |