CN202686084U - Compartment of unmanned helicopter - Google Patents

Compartment of unmanned helicopter Download PDF

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Publication number
CN202686084U
CN202686084U CN 201220302041 CN201220302041U CN202686084U CN 202686084 U CN202686084 U CN 202686084U CN 201220302041 CN201220302041 CN 201220302041 CN 201220302041 U CN201220302041 U CN 201220302041U CN 202686084 U CN202686084 U CN 202686084U
Authority
CN
China
Prior art keywords
platform
compartment
strut bar
hinge
depopulated helicopter
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.)
Expired - Fee Related
Application number
CN 201220302041
Other languages
Chinese (zh)
Inventor
张宁
雷志荣
唐强
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.)
No 618 Research Institute of China Aviation Industry
Original Assignee
No 618 Research Institute of China Aviation Industry
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by No 618 Research Institute of China Aviation Industry filed Critical No 618 Research Institute of China Aviation Industry
Priority to CN 201220302041 priority Critical patent/CN202686084U/en
Application granted granted Critical
Publication of CN202686084U publication Critical patent/CN202686084U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model belongs to an unmanned helicopter delivery technology and relates to a compartment of an unmanned helicopter. The compartment of the unmanned helicopter comprises a compartment body (8) provided with a rectangular hexahedron cavity and is characterized in that two sets of unmanned helicopter fixing devices are installed in the compartment body (8). Each set of unmanned helicopter fixing devices consists of a platform hook (1), a platform hinge (2), two undercarriage fixing mechanism (3), a platform (4), a platform support rod (5), a support rod positioning mechanism (6) and a support rod hinge (7). The compartment of the unmanned helicopter greatly simplifies the loading process, reduces manpower and material resources consumption and improves the work efficiency.

Description

A kind of compartment that delivers depopulated helicopter
Technical field
The utility model belongs to the depopulated helicopter delivery technology, relates to a kind of compartment of delivery.
Background technology
At present, before the depopulated helicopter long distance transportation, at first will be with the consumable accessory (such as dismountings such as main oar, tail-rotors) of helicopter, then pack into in the special carton of depopulated helicopter, and between carton and depopulated helicopter, add enough foamed plastic and prevent the depopulated helicopter strenuous vibration, the carton that will load depopulated helicopter with modes such as splicing or screw connections at last is fixed in inside, boxcar.Whole process is very complicated, consumes a large amount of human and material resources, inefficiency.
Summary of the invention
The purpose of this utility model is: propose a kind of business car that delivers depopulated helicopter, to simplify loading process, reduce human and material resources consumption, increase work efficiency.
The technical solution of the utility model is: a kind of compartment that delivers depopulated helicopter, comprise a compartment with rectangular hexahedron cavity volume, it is characterized in that, two cover depopulated helicopter anchor fittings are installed in the compartment, one cover depopulated helicopter anchor fitting respectively is installed on the sidewall of the left and right sides of compartment longitudinal axis, and two cover depopulated helicopter anchor fittings are at least 20cm along the interval d that the compartment longitudinal axis staggers mutually; Every cover depopulated helicopter anchor fitting is comprised of platform hook, platform hinge, two alighting gear fixed mechanisms, platform, platform strut bar, strut bar detent mechanism and strut bar hinges; Platform is a rectangular flat, a long limit of platform consists of chain connection by a side sidewall in platform hinge and compartment, two corresponding positions of upper surface that the alighting gear fixed mechanism is installed in platform, the platform hook is installed on the railroad car lateral wall at platform hinge place, after platform is upwards packed up, platform hooks another long limit of platform, one end of platform strut bar consists of chain connection by the railroad car lateral wall at strut bar hinge and platform hinge place, the platform strut bar be positioned at platform below, the strut bar detent mechanism is fixed on the lower surface of platform, when the other end of platform strut bar after the strut bar detent mechanism is combined, platform is parallel with the floor in compartment.
The utility model has the advantages that: proposed a kind of business car that delivers depopulated helicopter, greatly simplified loading process, reduced human and material resources consumption, improved work efficiency.Evidence, the utility model is compared with present stowage, and work efficiency has improved more than 5 times.
Description of drawings
Fig. 1 is structural representation of the present utility model.The depopulated helicopter anchor fitting is in loading condition among this figure.
Fig. 2 is the birds-eye view of Fig. 1.
Fig. 3 is also structural representation of the present utility model.The depopulated helicopter anchor fitting is in collapsed state among this figure.
The specific embodiment
The below is described in further details the utility model.Referring to Fig. 1,2, a kind of compartment that delivers depopulated helicopter, comprise a compartment 8 with rectangular hexahedron cavity volume, it is characterized in that, two cover depopulated helicopter anchor fittings are installed in compartment 8, one cover depopulated helicopter anchor fitting respectively is installed on the sidewall of the left and right sides of compartment 8 longitudinal axis, and the two cover depopulated helicopter anchor fitting interval d that 8 longitudinal axis stagger mutually along the compartment are at least 20cm; Every cover depopulated helicopter anchor fitting is comprised of platform hook 1, platform hinge 2, two alighting gear fixed mechanisms 3, platform 4, platform strut bar 5, strut bar detent mechanism 6 and strut bar hinges 7; Platform 4 is rectangular flats, a long limit of platform 4 is by the side sidewall formation chain connection of platform hinge 2 with compartment 8, two corresponding positions of upper surface that alighting gear fixed mechanism 3 is installed in platform 4, platform hook 1 is installed on the railroad car lateral wall at platform hinge 2 places, after platform 4 is upwards packed up, platform hook 1 hooks another long limit of platform 4, one end of platform strut bar 5 is by the railroad car lateral wall formation chain connection of strut bar hinge 7 with platform hinge 2 places, platform strut bar 5 be positioned at platform 4 below, strut bar detent mechanism 6 is fixed on the lower surface of platform 4, behind the other end and 6 combinations of strut bar detent mechanism of platform strut bar 5, platform 4 is parallel with the floor in compartment 8.
Principle of work of the present utility model is: when the delivery depopulated helicopter, referring to Fig. 1, put down platform 4 after opening platform hook 1, by strut bar detent mechanism 6, with platform 4 and 5 combinations of platform strut bar, make platform 4 parallel with the floor in compartment 8, depopulated helicopter is placed on platform 4 upper surfaces, cross over respectively two waling stripe tops that are installed in the depopulated helicopter alighting gear with two alighting gear fixed mechanisms 3, with screw two alighting gear fixed mechanisms 3 are locked at respectively on the platform 4, make depopulated helicopter steady without rocking in transportation.Behind the unloading depopulated helicopter, referring to Fig. 3, pack up platform 4, with platform hook 1 a long limit of hooking platform 4, platform strut bar 5 freely falls, and for the compartment saves large quantity space, can transport other goods.
Embodiment 1, the two cover depopulated helicopter anchor fitting interval d=20cm that 8 longitudinal axis stagger mutually along the compartment.Said platform hook 1 is an elastic hook, in the platform 4 lower surfaces position corresponding with elastic hook a locking slot is arranged, and after platform 4 was upwards packed up, above-mentioned elastic hook entered locking slot, and platform 4 is compressed.Said alighting gear fixed mechanism 3 is a U-shaped pressing plate, and after the depopulated helicopter alighting gear was placed on the platform 4, above-mentioned U-shaped pressing plate was crossed over and is installed in alighting gear waling stripe top, and by screw alighting gear is locked.Said strut bar detent mechanism 6 is a long aluminum cylinder of 5cm, tilts to be installed in platform 4 lower surfaces, and when platform 4 put down, platform strut bar 5 just can penetrate this aluminum cylinder, with platform 4 lockings, and makes platform 4 parallel with the floor in compartment 8.
Embodiment 2, the two cover depopulated helicopter anchor fitting interval d=25cm that 8 longitudinal axis stagger mutually along the compartment.Said platform hook 1 is a steel hook that angle is adjustable, on steel hook surface tapped through hole is arranged, and also there is a tapped through hole position corresponding with the steel hook at platform 4 lower surfaces, after platform 4 is upwards packed up, by screw above-mentioned steel hook and platform is locked.Said alighting gear fixed mechanism 3 is a strip plate, and after the depopulated helicopter alighting gear was placed on the platform 4, above-mentioned strip plate was crossed over and is installed in alighting gear waling stripe top, and by screw alighting gear is locked.Said strut bar detent mechanism 6 is a steel annulus, be installed in platform 4 lower surface appropriate locations, one end of said platform strut bar 5 consists of chain connection by strut bar hinge 7 and railroad car lateral wall, platform strut bar 5 other ends are steel hook, when platform 4 puts down, platform strut bar 5 just can tangle above-mentioned steel annulus, with platform 4 lockings, and makes platform 4 parallel with the floor in compartment 8.

Claims (1)

1. compartment that delivers depopulated helicopter, comprise a compartment (8) with rectangular hexahedron cavity volume, it is characterized in that, two cover depopulated helicopter anchor fittings are installed in compartment (8), one cover depopulated helicopter anchor fitting respectively is installed on the sidewall of the left and right sides of compartment (8) longitudinal axis, and the two cover depopulated helicopter anchor fitting interval d that (8) longitudinal axis staggers mutually along the compartment are at least 20cm; Every cover depopulated helicopter anchor fitting is comprised of platform hook (1), platform hinge (2), two alighting gear fixed mechanisms (3), platform (4), platform strut bar (5), strut bar detent mechanism (6) and strut bar hinge (7); Platform (4) is a rectangular flat, a long limit of platform (4) is by the side sidewall formation chain connection of platform hinge (2) with compartment (8), two alighting gear fixed mechanisms (3) are installed in the corresponding position of upper surface of platform (4), platform hook (1) is installed on the railroad car lateral wall at platform hinge (2) place, after platform (4) is upwards packed up, platform hook (1) hooks another long limit of platform (4), one end of platform strut bar (5) is by the railroad car lateral wall formation chain connection of strut bar hinge (7) with platform hinge (2) place, platform strut bar (5) be positioned at platform (4) below, strut bar detent mechanism (6) is fixed on the lower surface of platform (4), behind the other end and strut bar detent mechanism (6) combination of platform strut bar (5), platform (4) is parallel with the floor of compartment (8).
CN 201220302041 2012-06-26 2012-06-26 Compartment of unmanned helicopter Expired - Fee Related CN202686084U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220302041 CN202686084U (en) 2012-06-26 2012-06-26 Compartment of unmanned helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220302041 CN202686084U (en) 2012-06-26 2012-06-26 Compartment of unmanned helicopter

Publications (1)

Publication Number Publication Date
CN202686084U true CN202686084U (en) 2013-01-23

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220302041 Expired - Fee Related CN202686084U (en) 2012-06-26 2012-06-26 Compartment of unmanned helicopter

Country Status (1)

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CN (1) CN202686084U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103963991A (en) * 2013-01-30 2014-08-06 中国科学院沈阳自动化研究所 Mechatronics on-board system for unmanned helicopter
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103963991A (en) * 2013-01-30 2014-08-06 中国科学院沈阳自动化研究所 Mechatronics on-board system for unmanned helicopter
CN103963991B (en) * 2013-01-30 2016-04-06 中国科学院沈阳自动化研究所 A kind of electromechanical integration unmanned plane onboard system
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

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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: 20130123

Termination date: 20180626

CF01 Termination of patent right due to non-payment of annual fee