CN205524998U - Hang thing knot, suspension and unmanned helicopter - Google Patents

Hang thing knot, suspension and unmanned helicopter Download PDF

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Publication number
CN205524998U
CN205524998U CN201620282637.9U CN201620282637U CN205524998U CN 205524998 U CN205524998 U CN 205524998U CN 201620282637 U CN201620282637 U CN 201620282637U CN 205524998 U CN205524998 U CN 205524998U
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CN
China
Prior art keywords
suspension
main body
hanging fastener
article hanging
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.)
Active
Application number
CN201620282637.9U
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Chinese (zh)
Inventor
王江平
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.)
Zhuhai Ziyan unmanned aircraft Co. Ltd.
Original Assignee
Zhuhai Ziyan New Technology Co Ltd
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.)
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Priority to CN201620282637.9U priority Critical patent/CN205524998U/en
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Publication of CN205524998U publication Critical patent/CN205524998U/en
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Abstract

The utility model discloses a hang thing knot, suspension and unmanned helicopter. Wherein hang the thing and detain and be used for unmanned helicopter to hang the object, it is equipped with the main part, locate main part one end and be used for fixed connection on unmanned helicopter first link and locate the main part other end and be used for the fixed second link that hangs the object, the second link is equipped with the swallow tail. The utility model has the advantages of easy dismounting, convenient to use, stable performance, simple structure, low in manufacturing cost, the easy manufacturing.

Description

Article hanging fastener, suspension and depopulated helicopter
Technical field
This utility model relates to Article hanging fastener, suspension and depopulated helicopter.
Background technology
Along with science and technology constantly improves, society's development, depopulated helicopter is more and more universal, and user is increasingly higher to the requirement of depopulated helicopter.It is a very important advantage that depopulated helicopter carries object, but common depopulated helicopter typically uses cavity, or binding, or the mode such as suspention carries out carrying object, and conventional art has the disadvantage in that
1, mounting space is little, or lift-launch object can not well be uniformly distributed;
2, dismounting trouble, disassembly and assembly time is long, and dismounting speed is low;
3, carry area damage and can affect the stability of airframe structure;
4, easily come off.
Utility model content
Technical problem to be solved in the utility model is to overcome the deficiencies in the prior art, it is provided that suspension member frame, suspension and depopulated helicopter, and it has easy accessibility, easy to use, stable performance, simple in construction, low cost of manufacture, the advantage easily manufactured.
This utility model be the technical scheme is that
Article hanging fastener, it is for buckling at depopulated helicopter by object, and it is provided with main body and is connected with main body and for coordinating fixing dovetail groove.
Described main body is curved, described main body two ends are respectively the first connection end and second and connect end, described first connects end is provided with one end toward the through through hole of the other end, and described second connects end is provided with screw hole 23, and described first connects end is connected between end with described second and is bolted to connection.
Being provided with the deformation position coordinating deformation in the middle of described main body, described deformation position is provided with perforation.
Described body interior is provided with arc contact surface, and described arc contact surface is smooth arc contact surface.
It is formed in one between main body and dovetail groove.
Suspension, it is at least provided with a described Article hanging fastener, and described suspension also includes the suspension member frame being fixed on depopulated helicopter by Article hanging fastener.
Described suspension member sets up body, be located at body one end and for the first connecting portion being fixedly connected on depopulated helicopter and be located at the body other end and for fixing the second connecting portion of Article hanging fastener;Described second connecting portion is provided with dovetail.
Described dovetail is provided with the first hole.
Described first connecting portion is provided with cross one another located lateral portion and longitudinal register portion, and described located lateral portion is provided with the second hole, and described longitudinal register portion is provided with the 3rd hole.
Depopulated helicopter, it is at least provided with described suspension.
Object is fixedly mounted on the body interior of Article hanging fastener, the distance between end is connected by bolt regulation the first connection end and second, realize fixing and unclamp the object in body interior, dovetail groove is inserted on dovetail, by screw by locking between dovetail groove and dovetail, the first connecting portion of suspension member frame is fixedly mounted on the fuselage of depopulated helicopter.
The beneficial effects of the utility model are: it has easy accessibility, easy to use, stable performance, simple in construction, low cost of manufacture, the advantage easily manufactured.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
Article hanging fastener, it is for buckling at depopulated helicopter by object, and it is provided with main body 22 and is connected with main body 22 and for coordinating fixing dovetail groove 21.
Described main body 22 is curved, described main body 22 two ends are respectively the first connection end and second and connect end, described first connects end is provided with one end toward the through through hole of the other end, and described second connects end is provided with screw hole 23, and described first connects end is connected between end with described second and is bolted to connection.
Being provided with the deformation position 24 coordinating deformation in the middle of described main body 22, described deformation position 24 is provided with perforation.
Described main body 22 is internal is provided with arc contact surface, and described arc contact surface is smooth arc contact surface.
It is formed in one between main body 22 and dovetail groove 21.
Suspension, it also includes, at least provided with a described Article hanging fastener 2, described suspension, the suspension member frame 1 being fixed on depopulated helicopter by Article hanging fastener.
Described suspension member sets up body 12, be located at body 12 one end and for the first connecting portion 11 being fixedly connected on depopulated helicopter and be located at body 12 other end and for fixing the second connecting portion 13 of Article hanging fastener;Described second connecting portion 13 is provided with dovetail.
Described dovetail is provided with the first hole.
Described first connecting portion 11 is provided with cross one another located lateral portion and longitudinal register portion, and described located lateral portion is provided with the second hole, and described longitudinal register portion is provided with the 3rd hole.
Depopulated helicopter, it is at least provided with described suspension.
Object is fixedly mounted on the body interior of Article hanging fastener, the distance between end is connected by bolt regulation the first connection end and second, realize fixing and unclamp the object in body interior, dovetail groove is inserted on dovetail, by screw by locking between dovetail groove and dovetail, the first connecting portion of suspension member frame is fixedly mounted on the fuselage of depopulated helicopter.
The beneficial effects of the utility model are: it has easy accessibility, easy to use, stable performance, simple in construction, low cost of manufacture, the advantage easily manufactured.

Claims (10)

1. Article hanging fastener, it is for buckling at depopulated helicopter by object, it is characterised in that: it is provided with main body (22) and is connected with main body (22) and for coordinating fixing dovetail groove (21).
Article hanging fastener the most according to claim 1, it is characterized in that: described main body (22) is curved, described main body (22) two ends are respectively the first connection end and second and connect end, described first connects end is provided with one end toward the through through hole of the other end, described second connects end is provided with screw hole (23), and described first connects end is connected between end with described second and is bolted to connection.
Article hanging fastener the most according to claim 2, it is characterised in that: being provided with the deformation position (24) coordinating deformation in the middle of described main body (22), described deformation position (24) is provided with perforation.
Article hanging fastener the most according to claim 3, it is characterised in that: described main body (22) is internal is provided with arc contact surface, and described arc contact surface is smooth arc contact surface.
Article hanging fastener the most according to claim 4, it is characterised in that: it is formed in one between main body (22) and dovetail groove (21).
6. suspension, it is characterised in that: it also includes, at least provided with an Article hanging fastener (2) as described in claim 1 to 5 any one, described suspension, the suspension member frame (1) being fixed on depopulated helicopter by Article hanging fastener.
Suspension the most according to claim 6, it is characterised in that: described suspension member sets up body (12), be located at body (12) one end and for the first connecting portion (11) of being fixedly connected on depopulated helicopter and be located at body (12) other end and for fixing second connecting portion (13) of Article hanging fastener;Described second connecting portion (13) is provided with dovetail.
Suspension the most according to claim 7, it is characterised in that: described dovetail is provided with the first hole.
Suspension the most according to claim 7, it is characterised in that: described first connecting portion (11) is provided with cross one another located lateral portion and longitudinal register portion, and described located lateral portion is provided with the second hole, and described longitudinal register portion is provided with the 3rd hole.
10. depopulated helicopter, it is characterised in that: it is at least provided with the suspension as described in claim 7 to 9 any one.
CN201620282637.9U 2016-04-07 2016-04-07 Hang thing knot, suspension and unmanned helicopter Active CN205524998U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620282637.9U CN205524998U (en) 2016-04-07 2016-04-07 Hang thing knot, suspension and unmanned helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620282637.9U CN205524998U (en) 2016-04-07 2016-04-07 Hang thing knot, suspension and unmanned helicopter

Publications (1)

Publication Number Publication Date
CN205524998U true CN205524998U (en) 2016-08-31

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620282637.9U Active CN205524998U (en) 2016-04-07 2016-04-07 Hang thing knot, suspension and unmanned helicopter

Country Status (1)

Country Link
CN (1) CN205524998U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105818986A (en) * 2016-04-07 2016-08-03 珠海紫燕新科技有限公司 Hang frame, suspension system and unmanned helicopter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105818986A (en) * 2016-04-07 2016-08-03 珠海紫燕新科技有限公司 Hang frame, suspension system and unmanned helicopter

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

Effective date of registration: 20170504

Address after: 519000 Xiangzhou, Guangdong Province, lemon Creek Taihe business center 16E

Patentee after: Zhuhai Ziyan unmanned aircraft Co. Ltd.

Address before: 519000, block B, Guoxin Plaza, No. 338, Xi Xi Road, Zhuhai, Guangdong, China 13F

Patentee before: ZHUHAI ZIYAN NEW TECHNOLOGY CO., LTD.