CN208630845U - Small drone wheel-retracting gear - Google Patents

Small drone wheel-retracting gear Download PDF

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Publication number
CN208630845U
CN208630845U CN201821166263.XU CN201821166263U CN208630845U CN 208630845 U CN208630845 U CN 208630845U CN 201821166263 U CN201821166263 U CN 201821166263U CN 208630845 U CN208630845 U CN 208630845U
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CN
China
Prior art keywords
gear
steering engine
wheel
drive shaft
gear drive
Prior art date
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Active
Application number
CN201821166263.XU
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Chinese (zh)
Inventor
张利辉
谭现洪
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Computational Aerodynamics Institute of China Aerodynamics Research and Development Center
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Sichuan Biaolei Technology Co Ltd
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Priority to CN201821166263.XU priority Critical patent/CN208630845U/en
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Publication of CN208630845U publication Critical patent/CN208630845U/en
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Abstract

The utility model discloses a kind of small drone wheel-retracting gears, including steering engine, steering engine bracket, pinion gear, gear wheel, transmission swing arm, main support, gear drive shaft, the steering engine is on steering engine bracket, steering engine bracket is on main support, the drive shaft of pinion gear is located on steering engine, and for gear drive shaft through bearing on main support, gear wheel is packed in gear drive shaft one end, gear wheel engages composition gear drive with pinion gear, and rotation swing arm is packed in gear drive shaft.The utility model, as driving mechanism, the rotation of folding and unfolding shaft is directly driven by gear drive, to control undercarriage control using steering engine.Hydraulic drive circuit in the prior art and push-pull device at fixed is omitted in the utility model, greatly simplifies structure and control is easy, is reliable.

Description

Small drone wheel-retracting gear
Technical field
The utility model belongs to vehicle technology field, in particular to a kind of small drone wheel-retracting gear.
Background technique
Undercarriage, which is aircraft, which to be parked on ground, slides, takeoff and anding is sliding is used to support aircraft gravity when running, and bears corresponding carry The device of lotus.
When aircraft flies at low speed, the requirement to Aerodynamic Configuration of Aireraft is not very stringent, therefore the undercarriage of this kind of aircraft is all Be it is fixed, such manufacture difficulty is accordingly smaller, and when aircraft flight in the sky, undercarriage is still exposed to except fuselage.
With the continuous improvement of aircraft flight speed, the resistance of flight can also sharply increase therewith, at this moment, be exposed to outer Undercarriage has just seriously affected the aeroperformance of aircraft, therefore, it is necessary to design retractable undercarriage, can be retracted into flight Within wing or fuselage, when landing, puts down the respective loads for bearing aircraft again.
Conventional Take-off and Landing frame is acted using hydraulic-driven pressurized strut, is rotated around folding and unfolding shaft to push and pull undercarriage to realize Draw-in and draw-off function, this structure will have a set of hydraulic drive circuit, and system complex, control difficulty is big, not be suitable for small-sized nothing On man-machine.
Utility model content
The utility model provides a kind of novel small drone wheel-retracting gear, solves the above conventional Take-off and Landing Frame jack in small drone with when there are the problem of.The mechanism is directly driven using steering engine by gear drive The rotation of folding and unfolding shaft, and folding and unfolding shaft and undercarriage are connected, the rotation of folding and unfolding shaft can drive undercarriage control, this is practical new Type greatly simplifies the structure of Landing Gear System, and this mechanism controls is easy, is reliable.
The utility model uses following technical scheme: a kind of small drone wheel-retracting gear, including steering engine, steering engine Bracket, pinion gear, gear wheel, transmission swing arm, main support, gear drive shaft, the steering engine is on steering engine bracket, steering engine bracket On main support, the drive shaft of pinion gear is located on steering engine, and for gear drive shaft through bearing on main support, gear wheel is solid Mounted in gear drive shaft one end, gear wheel engages composition gear drive with pinion gear, and rotation swing arm is packed in gear driving On axis.
Preferably, the steering engine is two, which is provided with the pinion gear of same size, is meshed respectively with gear wheel.
A kind of small drone wheel-retracting gear of the utility model, for pinion gear on steering engine, steering engine is mounted in steering engine On bracket, for gear drive shaft on main support, pinion gear and gear wheel form gear drive.The utility model uses rudder Machine directly drives the rotation of folding and unfolding shaft by gear drive, to control undercarriage control as driving mechanism.This is practical new Hydraulic drive circuit in the prior art and push-pull device at fixed is omitted in type, greatly simplifies structure and control is easy, is reliable.
The wheel-retracting gear has the following advantages:
1. the utility model, as driving mechanism, is omitted a big set hydraulic drive circuit, simplifies structure using steering engine, Control is easy, is reliable;
2. the utility model directly drives the rotation of folding and unfolding shaft using gear drive to realize undercarriage control, it is omitted and pushes away Drawing device further simplifies structure.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the small drone wheel-retracting gear of the utility model embodiment 1.
Figure label respectively indicates are as follows: (1) steering engine;(2) steering engine bracket;(3) pinion gear;(4) gear wheel;(5) transmission pendulum Arm;(6) main support;(7) gear drive shaft.
Specific embodiment
Embodiment 1
Technical solutions of the utility model are discussed in detail with reference to the accompanying drawing.
As shown in Figure 1, the present embodiment uses Twin Rudders present embodiment discloses a kind of small drone wheel-retracting gear Machine driving, one-stage gear are driven.Two steering engines 1 are attached separately on steering engine bracket 2, and steering engine bracket 2 is mounted on main support 6, Pinion gear 3 is on steering engine 1, and for gear drive shaft 7 through bearing on main support 6, gear wheel 4 is packed in gear drive shaft 7 The other end, gear wheel 4 engage composition gear drive with pinion gear 3, and rotation swing arm 5 is packed in gear drive shaft 7.
1 driving pinion 3 of double steering engine of the present embodiment rotates, and is rotated by gear pair, then band moving gear drive shaft 7, and Driving torque can be amplified by the transmission of gear, transmission swing arm 5 is connected in gear drive shaft 7, this can drive biography function The deflection up and down of swing arm 5, to realize the folding and unfolding of undercarriage.
Embodiment 2
Present embodiment discloses a kind of small drone wheel-retracting gears, unlike the first embodiment, using single rudder Machine driving, can meet the undercarriage of less demanding to driving torque.
The utility model small drone wheel-retracting gear can be used single steering engine or more servo drivings, can also adopt It is driven with multi-stage gear, requirement of the undercarriage to topology layout can be met.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, although ginseng The utility model is described in detail according to previous embodiment, it for those skilled in the art, still can be with It modifies the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features.It is all Within the spirit and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in practical Within novel protection scope.

Claims (2)

1. a kind of small drone wheel-retracting gear, which is characterized in that including steering engine, steering engine bracket, pinion gear, canine tooth Wheel, transmission swing arm, main support, gear drive shaft, for the steering engine on steering engine bracket, steering engine bracket is small on main support The drive shaft of gear is located on steering engine, and for gear drive shaft through bearing on main support, gear wheel is packed in gear drive shaft One end, gear wheel engage composition gear drive with pinion gear, and rotation swing arm is packed in gear drive shaft.
2. small drone wheel-retracting gear according to claim 1, which is characterized in that the steering engine is two, It which is provided with identical pinion gear, be meshed respectively with gear wheel.
CN201821166263.XU 2018-07-23 2018-07-23 Small drone wheel-retracting gear Active CN208630845U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821166263.XU CN208630845U (en) 2018-07-23 2018-07-23 Small drone wheel-retracting gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821166263.XU CN208630845U (en) 2018-07-23 2018-07-23 Small drone wheel-retracting gear

Publications (1)

Publication Number Publication Date
CN208630845U true CN208630845U (en) 2019-03-22

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821166263.XU Active CN208630845U (en) 2018-07-23 2018-07-23 Small drone wheel-retracting gear

Country Status (1)

Country Link
CN (1) CN208630845U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112478139A (en) * 2020-11-30 2021-03-12 重庆空翼航天科技有限公司 Undercarriage control system and method for unmanned aerial vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112478139A (en) * 2020-11-30 2021-03-12 重庆空翼航天科技有限公司 Undercarriage control system and method for unmanned aerial vehicle
CN112478139B (en) * 2020-11-30 2023-02-07 重庆空翼航天科技有限公司 Undercarriage control system and method for unmanned aerial vehicle

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GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20220211

Address after: 622750 No. 5, Wangchong street, Yongchang Town, Beichuan Qiang Autonomous County, Mianyang City, Sichuan Province (Beichuan General Aviation Industrial Park, China Science and technology city)

Patentee after: SICHUAN SPECIAL VEHICLE SCIENCE AND TECHNOLOGY CO.,LTD.

Address before: 621000 3-2-2-1, No. 70, east section of Puming South Road, high tech Zone, Mianyang City, Sichuan Province

Patentee before: SICHUAN YAOLEI TECHNOLOGY Co.,Ltd.

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20240805

Address after: 621000 No.6, south section of the Second Ring Road, Fucheng District, Mianyang City, Sichuan Province

Patentee after: COMPUTATIONAL AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RESEARCH AND DEVELOPMENT CENTER

Country or region after: China

Address before: 622750 No. 5, Wangchong street, Yongchang Town, Beichuan Qiang Autonomous County, Mianyang City, Sichuan Province (Beichuan General Aviation Industrial Park, China Science and technology city)

Patentee before: SICHUAN SPECIAL VEHICLE SCIENCE AND TECHNOLOGY CO.,LTD.

Country or region before: China