CN106800093A - A kind of wheeled depopulated helicopter is taken a flight test protection device - Google Patents
A kind of wheeled depopulated helicopter is taken a flight test protection device Download PDFInfo
- Publication number
- CN106800093A CN106800093A CN201510846421.0A CN201510846421A CN106800093A CN 106800093 A CN106800093 A CN 106800093A CN 201510846421 A CN201510846421 A CN 201510846421A CN 106800093 A CN106800093 A CN 106800093A
- Authority
- CN
- China
- Prior art keywords
- anchor tip
- flight test
- depopulated helicopter
- protection device
- protection frame
- 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.)
- Pending
Links
- 239000007787 solid Substances 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 5
- 241000256844 Apis mellifera Species 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000994 depressogenic effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
Classifications
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Sampling And Sample Adjustment (AREA)
Abstract
Taken a flight test guarantee apparatus field the invention belongs to depopulated helicopter, be related to test when taking a flight test using to a kind of special protection device of taking a flight test of wheel undercarriage depopulated helicopter.Wheeled depopulated helicopter protection device of taking a flight test is used for reference Air China's industry all of skid landing gear of helicopter and is taken a flight test the principle of protection device; actual installation according to wheel undercarriage depopulated helicopter needs to redesign the structure type and mounting means of protection device erection joint of taking a flight test, and makes full use of the structure of body to be fixed protection device of taking a flight test.
Description
Technical field
Take a flight test guarantee apparatus field the invention belongs to depopulated helicopter, be related to test when taking a flight test using arriving
A kind of special protection device of taking a flight test of wheel undercarriage depopulated helicopter.
Background technology
Depopulated helicopter is different with unmanned fixed wing aircraft, and due to there is rotor, its aerodynamic characteristic and dynamics are special
Property it is complicated far beyond fixed wing aircraft, be that item is multidisciplinary, mutli-system integration modernization high-tech project, therefore
Technically difficulty is very big.Depopulated helicopter is balance, compensation, decoupling of pilot guidance helicopter etc.
Technology, reflects in flight control system exactly, thus the research of depopulated helicopter plant characteristic is more than having
The requirement of people's helicopter is high, is also to carry out the technical scheme that over the horizon autonomous flight must be studied and solved.
Because depopulated helicopter is operated without pilot on body, and new body is unstable also unreliable, flies control
System imperfection, on trickle Parameters variation, flight control system can not pass through fuzzy operation as pilot
Carry out the pose adjustment of body, it is necessary to first be tethered at taking a flight test.It is tethered at that to take a flight test be to check depopulated helicopter
Each system working condition of full machine, and the ability to work and state of each system are tentatively examined, particularly fly control system
The function and state of system, make full machine reach the state of the art that can be taken a flight test with near-earth hovering.And be tethered at and take a flight test therewith
Near-earth hovering afterwards, is protection body, increases the scope of contacting to earth of body undercarriage, it is necessary to using to the guarantor that takes a flight test
Protection unit, so as to can to a certain extent reduce the rollover of body and preceding turn over that (body carries shoe, can prevent
Turned over after body).
The protection device of taking a flight test of existing depopulated helicopter is all only applicable to the body of skid landing gear, such as V750
With honeybee depopulated helicopter.The protection device of V750 has reached increase body undercarriage and has contacted to earth the purpose of scope,
But it is completely independent between protection device, it is impossible to the impact for bearing to rise and fall when colliding with, is not had under case of emergency
Protect the effect of body.Honeybee depopulated helicopter is coaxial dual-propeller, itself flight attitude stabilization, protection
All around span is not enough for device, and the protective effect played under case of emergency is not enough.Industry helicopter institute of Air China
Skid landing gear depopulated helicopter take a flight test protection device use for reference honeybee depopulated helicopter take a flight test protection dress
Put, and carry out the extension of span, successfully protect nobody to go straight up to when hovering with entering and taking a flight test being tethered to take a flight test
Machine.
The content of the invention
Wheeled depopulated helicopter protection device of taking a flight test uses for reference Air China's industry helicopter all of skid landing gear
The principle of protection device of taking a flight test, the actual installation according to wheel undercarriage depopulated helicopter needs to redesign examination
Fly the structure type and mounting means of protection device erection joint, make full use of the structure of body to be fixed examination
Fly protection device.
Including depopulated helicopter body, cross-protection frame, symmetrically arranged preceding anchor tip outer member, symmetrically
The preceding anchor tip medial side part for setting, covers, symmetrically arranged vertical protection on symmetrically arranged preceding anchor tip
Frame, rear anchor tip left member, rear anchor tip right member is covered on rear anchor tip；Preceding anchor tip outer member
The left and right both sides in front of depopulated helicopter body are individually fixed in using bolt with preceding anchor tip medial side part
On wheel undercarriage；After rear anchor tip left member and rear anchor tip right member are fixed on into depopulated helicopter body
On the wheel undercarriage of side；Cross-protection frame is positioned over preceding anchor tip outer member cross-protection frame mounting groove
It is interior, vertical protection frame is positioned in the vertical protection frame mounting groove of anchor tip left member and anchor tip right member,
And set respective spacing；By being covered on preceding anchor tip preceding anchor tip outer member is individually fixed in using bolt
With preceding anchor tip medial side part；Will on rear anchor tip lid make to be bolted to rear anchor tip left member and after
In anchor tip right member.
Taken a flight test protection device using the wheeled depopulated helicopter, be tethered at that take a flight test can be maximum when being taken a flight test with near-earth hovering
The safety of limit ground protection depopulated helicopter body, increase undercarriage contacts to earth scope, reduce the rollover of body with
Before the angle turned over.
Brief description of the drawings
Fig. 1 is preceding depressed pole extreme position of the invention,
Fig. 2 is roll extreme position of the invention,
Fig. 3 is installation top view of the invention,
Fig. 4 is preceding anchor tip installation diagram of the invention,
Fig. 5 is the installation diagram of rear anchor tip of the invention.
1 is depopulated helicopter body, and 2 is cross-protection frame, 3 be preceding anchor tip outer member (totally 2,
It is symmetrical member), 4 is preceding anchor tip medial side part (totally 2, be symmetrical member), and 5 are covered on preceding anchor tip
(totally 2, be symmetrical member), 6 is vertical protection frame (totally 2, be symmetrical member), and 7 is rear anchor tip
Left member, 8 is rear anchor tip right member, and 9 is that (above positive direction is depopulated helicopter machine to lid on rear anchor tip
The course direction of body)
Specific embodiment
A kind of wheeled depopulated helicopter is taken a flight test protection device, including depopulated helicopter body 1, cross-protection frame 2,
Symmetrically arranged preceding anchor tip outer member 3, symmetrically arranged preceding anchor tip medial side part 4 is symmetrically arranged
Lid 5 on preceding anchor tip, symmetrically arranged vertical protection frame 6, rear anchor tip left member 7, rear anchor tip
Right member 8, lid 9 on rear anchor tip；Preceding anchor tip outer member 3 and preceding anchor tip medial side part 4 use spiral shell
Bolt is individually fixed on the wheel undercarriage on the left and right both sides in the front of depopulated helicopter body 1；It is fixed by after
Joint left member 7 and rear anchor tip right member 8 are fixed on the wheel undercarriage at the rear of depopulated helicopter body 1；
Cross-protection frame 2 is positioned in the cross-protection frame mounting groove of preceding anchor tip outer member 3, by vertical protection
Frame 6 is positioned in the vertical protection frame mounting groove of anchor tip left member 7 and anchor tip right member 8, and is set
Good respective spacing；Lid 5 on preceding anchor tip is individually fixed in the preceding He of anchor tip outer member 3 using bolt
Preceding anchor tip medial side part 4；Lid 9 on rear anchor tip is made to be bolted to the rear He of anchor tip left member 7
Afterwards in anchor tip right member 8.
It is tethered at and takes a flight test when being taken a flight test with near-earth hovering, it is necessary to install this protection device of taking a flight test.The first step is by preceding fixation
Before joint outer member 3 and preceding anchor tip medial side part 4 are individually fixed in depopulated helicopter body 1 using bolt
On the wheel undercarriage on the left and right both sides of side；Second step is right by rear anchor tip left member 7 and rear anchor tip
Part 8 is fixed on the wheel undercarriage at the rear of depopulated helicopter body 1；3rd step puts cross-protection frame 2
It is placed in the cross-protection frame mounting groove of preceding anchor tip outer member 3, vertical protection frame 6 is positioned over into fixation connects
In the vertical protection frame mounting groove of head left member 7 and anchor tip right member 8, and set respective spacing；4th
Lid 5 on preceding anchor tip is individually fixed in preceding anchor tip outer member 3 and preceding anchor tip by step using bolt
Medial side part 4；Lid 9 on rear anchor tip is made to be bolted to rear anchor tip left member 7 and consolidated afterwards by the 5th step
Determine in joint right member 8.
Take a flight test after finishing, protection device of taking a flight test is dismantled according to above-mentioned backward.
Claims (1)
1. a kind of wheeled depopulated helicopter is taken a flight test protection device, it is characterised in that：Including depopulated helicopter body
(1), cross-protection frame (2), symmetrically arranged preceding anchor tip outer member (3) is symmetrically arranged preceding solid
Determine joint medial side part (4), cover (5) on symmetrically arranged preceding anchor tip, symmetrically arranged vertical protection frame
(6), rear anchor tip left member (7), rear anchor tip right member (8) covers (9) on rear anchor tip；Before
Anchor tip outer member (3) and preceding anchor tip medial side part (4) are individually fixed in nobody and go straight up to using bolt
On the wheel undercarriage on the left and right both sides in front of machine body (1)；By rear anchor tip left member (7) and after
Anchor tip right member (8) is fixed on the wheel undercarriage at depopulated helicopter body (1) rear；Will be laterally
Fender bracket (2) is positioned in preceding anchor tip outer member (3) cross-protection frame mounting groove, by vertical protection
Frame (6) is positioned in the vertical protection frame mounting groove of anchor tip left member (7) and anchor tip right member (8),
And set respective spacing；It is individually fixed in (5) are covered on preceding anchor tip outside preceding anchor tip using bolt
Side part (3) and preceding anchor tip medial side part (4)；Make to be bolted to by (9) are covered on rear anchor tip
Afterwards in anchor tip left member (7) and rear anchor tip right member (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510846421.0A CN106800093A (en) | 2015-11-26 | 2015-11-26 | A kind of wheeled depopulated helicopter is taken a flight test protection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510846421.0A CN106800093A (en) | 2015-11-26 | 2015-11-26 | A kind of wheeled depopulated helicopter is taken a flight test protection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106800093A true CN106800093A (en) | 2017-06-06 |
Family
ID=58976832
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510846421.0A Pending CN106800093A (en) | 2015-11-26 | 2015-11-26 | A kind of wheeled depopulated helicopter is taken a flight test protection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106800093A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107792385A (en) * | 2017-09-08 | 2018-03-13 | 中国飞行试验研究院 | It is a kind of to be used for the outdoor device and method parked in helicopter outfield |
| CN108945513A (en) * | 2018-04-19 | 2018-12-07 | 哈尔滨飞机工业集团有限责任公司 | A kind of moveable mooring of helicopter hovering test device |
| CN109094800A (en) * | 2018-10-18 | 2018-12-28 | 北京清航紫荆装备科技有限公司 | A kind of intersection DCB Specimen unmanned helicopter and its fender bracket |
| US11230372B1 (en) | 2021-03-09 | 2022-01-25 | Beta Air, Llc | System for rolling landing gear |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4676461A (en) * | 1984-09-06 | 1987-06-30 | Fpt Industries Limited | Flotation devices for aircraft undercarriages |
| CN101973393A (en) * | 2010-09-30 | 2011-02-16 | 清华大学 | High-strength cage-type undercarriage of unmanned helicopter |
| CN103895873A (en) * | 2012-12-25 | 2014-07-02 | 中国直升机设计研究所 | Helicopter mooring flight testing protective device and mooring method of helicopter mooring flight testing protective device |
| CN104527990A (en) * | 2014-12-18 | 2015-04-22 | 国家电网公司 | Method for power grid transmission line patrol by means of unmanned helicopter |
-
2015
- 2015-11-26 CN CN201510846421.0A patent/CN106800093A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4676461A (en) * | 1984-09-06 | 1987-06-30 | Fpt Industries Limited | Flotation devices for aircraft undercarriages |
| CN101973393A (en) * | 2010-09-30 | 2011-02-16 | 清华大学 | High-strength cage-type undercarriage of unmanned helicopter |
| CN103895873A (en) * | 2012-12-25 | 2014-07-02 | 中国直升机设计研究所 | Helicopter mooring flight testing protective device and mooring method of helicopter mooring flight testing protective device |
| CN104527990A (en) * | 2014-12-18 | 2015-04-22 | 国家电网公司 | Method for power grid transmission line patrol by means of unmanned helicopter |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107792385A (en) * | 2017-09-08 | 2018-03-13 | 中国飞行试验研究院 | It is a kind of to be used for the outdoor device and method parked in helicopter outfield |
| CN108945513A (en) * | 2018-04-19 | 2018-12-07 | 哈尔滨飞机工业集团有限责任公司 | A kind of moveable mooring of helicopter hovering test device |
| CN109094800A (en) * | 2018-10-18 | 2018-12-28 | 北京清航紫荆装备科技有限公司 | A kind of intersection DCB Specimen unmanned helicopter and its fender bracket |
| CN109094800B (en) * | 2018-10-18 | 2024-01-30 | 北京清航紫荆装备科技有限公司 | Cross double-rotor unmanned helicopter and protection frame thereof |
| US11230372B1 (en) | 2021-03-09 | 2022-01-25 | Beta Air, Llc | System for rolling landing gear |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170606 |