CN203612199U - Embedded pedal - Google Patents

Embedded pedal Download PDF

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Publication number
CN203612199U
CN203612199U CN201320792492.3U CN201320792492U CN203612199U CN 203612199 U CN203612199 U CN 203612199U CN 201320792492 U CN201320792492 U CN 201320792492U CN 203612199 U CN203612199 U CN 203612199U
Authority
CN
China
Prior art keywords
hinge
strut member
cover plate
outer cover
pedal
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 - Lifetime
Application number
CN201320792492.3U
Other languages
Chinese (zh)
Inventor
李进
胡泊
陆富全
陈芳育
李成行
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.)
China Helicopter Research and Development Institute
Original Assignee
China Helicopter Research and Development Institute
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 China Helicopter Research and Development Institute filed Critical China Helicopter Research and Development Institute
Priority to CN201320792492.3U priority Critical patent/CN203612199U/en
Application granted granted Critical
Publication of CN203612199U publication Critical patent/CN203612199U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model discloses an embedded pedal, which can be treaded while can be used as a handle, and does not protrude out of a helicopter at any time. The technical scheme is that the embedded pedal includes an inner protective cover, a support piece, a hinge, a hinge rotating shaft, a torsional spring and an outer cover plate, wherein a handle lug boss and a sole support surface are arranged at the lower part of the support piece; liquid discharge holes are formed in the bottom of the support piece; the hinge is arranged at the upper part of the support piece; the outer cover plate is connected with the hinge; the torsional spring is arranged on the hinge, and penetrates the hinge rotating shaft; the outer cover plate is supported by the hinge and the torsional spring, and is always kept to be fitted with the outline of the helicopter body; the inner protective cover is arranged on the support piece to separate the support piece from the inside of the helicopter body. The embedded pedal provided by the utility model does not protrude out of the helicopter during the use, requires no extra operation, can be used as a pedal and a handle at the same time.

Description

A kind of embedded pedal
Technical field
The utility model relates to helicopter design field, relates in particular to a kind of embedded pedal.
Background technology
Pedal is used to helicopter to safeguard or user of service provides the passage that arrives maintenance or use location, as shown in Figure 1, conventionally adopts flat board (or tubulose) structure 1 of outstanding helicopter profile, and this structure both can be used as pedal, also can be used as handle and uses.
Due to the outstanding profile of dull and stereotyped (or tubulose) structure 1, affect helicopter attractive in appearance, and the accident such as easily cause that personnel collide with.
Utility model content
The technical problems to be solved in the utility model: propose a kind of embedded pedal, can meet that pin is stepped on and handle function, and in the neither outstanding helicopter profile of any process.
The technical solution of the utility model: a kind of embedded pedal, comprising:
Interior protective case, strut member, hinge, hinge rotating shaft, torsion spring and outer cover plate composition, strut member bottom is provided with handle boss and sole bearing surface, and strut member bottom is provided with rushes down liquid hole; Strut member top is provided with hinge, gemel connection outer cover plate, and hinge is provided with torsion spring, and torsion spring penetrates hinge rotating shaft, and outer cover plate is by hinge and torsional-spring supported, and remains with fuselage appearance face and fit; Strut member is provided with interior protective case, and strut member and fuselage interior are separated.
The beneficial effects of the utility model: a kind of embedded pedal of the utility model is not outstanding fuselage appearance in use, does not use operation bidirectional, both can make pedal and use, and also can make handle and use.
Accompanying drawing explanation
Fig. 1 is existing pedal structure schematic diagram.
Fig. 2 is the scheme of installation of the embedded pedal 2 of the utility model on covering 3.
Fig. 3 is the utility model structure composition sketch.
Fig. 4 a is that the utility model uses schematic diagram one.
Fig. 4 b is that the utility model uses schematic diagram two.
The specific embodiment
Below the utility model is described in further details.
Fig. 2 is the installation signal of the embedded pedal 2 of the utility model on covering 3.
Fig. 3 is the utility model structure composition sketch, and a kind of embedded pedal of the utility model, comprising:
Interior protective case 4, strut member 5, hinge 6, hinge rotating shaft 7, torsion spring 8 and outer cover plate 9 form, and strut member 5 bottoms are provided with handle boss 10 and sole bearing surface 11, and strut member 5 bottoms are provided with rushes down liquid hole 12; Strut member 5 tops are provided with hinge 6, hinge 6 connecting lid plates 9, and hinge 6 is provided with torsion spring 8, and torsion spring 8 penetrates hinge rotating shaft 7, and outer cover plate 9 is supported by hinge 6 and torsion spring 8, and remains with fuselage appearance face and fit; Strut member 5 is provided with interior protective case 4, and strut member 5 and fuselage interior are separated.
Fig. 4 a, b are for using schematic diagram.During as handle, user of service is directly with hand propelled outer cover plate 9 and fasten handle boss 10; During as pedal, user of service directly promotes outer cover plate 9 and steps on sole bearing surface 11 with tiptoe.
A kind of embedded pedal of the utility model is not outstanding fuselage appearance in use, does not use operation bidirectional, both can make pedal and use, and also can make handle and use.

Claims (1)

1. an embedded pedal, is characterized in that, comprising:
Interior protective case, strut member, hinge, hinge rotating shaft, torsion spring and outer cover plate composition, strut member bottom is provided with handle boss and sole bearing surface, and strut member bottom is provided with rushes down liquid hole; Strut member top is provided with hinge, gemel connection outer cover plate, and hinge is provided with torsion spring, and torsion spring penetrates hinge rotating shaft, and outer cover plate is by hinge and torsional-spring supported, and remains with fuselage appearance face and fit; Strut member is provided with interior protective case, and strut member and fuselage interior are separated.
CN201320792492.3U 2013-12-04 2013-12-04 Embedded pedal Expired - Lifetime CN203612199U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320792492.3U CN203612199U (en) 2013-12-04 2013-12-04 Embedded pedal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320792492.3U CN203612199U (en) 2013-12-04 2013-12-04 Embedded pedal

Publications (1)

Publication Number Publication Date
CN203612199U true CN203612199U (en) 2014-05-28

Family

ID=50764859

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320792492.3U Expired - Lifetime CN203612199U (en) 2013-12-04 2013-12-04 Embedded pedal

Country Status (1)

Country Link
CN (1) CN203612199U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105564660A (en) * 2014-10-15 2016-05-11 哈尔滨飞机工业集团有限责任公司 Helicopter externally hung tread beam structure
CN108100290A (en) * 2017-11-29 2018-06-01 中国直升机设计研究所 A kind of helicopter is rotatably ridden

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105564660A (en) * 2014-10-15 2016-05-11 哈尔滨飞机工业集团有限责任公司 Helicopter externally hung tread beam structure
CN108100290A (en) * 2017-11-29 2018-06-01 中国直升机设计研究所 A kind of helicopter is rotatably ridden

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20140528

CX01 Expiry of patent term