CN203473247U - Transceiver mounting bracket for helicopter. - Google Patents

Transceiver mounting bracket for helicopter. Download PDF

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Publication number
CN203473247U
CN203473247U CN201320418660.2U CN201320418660U CN203473247U CN 203473247 U CN203473247 U CN 203473247U CN 201320418660 U CN201320418660 U CN 201320418660U CN 203473247 U CN203473247 U CN 203473247U
Authority
CN
China
Prior art keywords
bracket
lower bracket
helicopter
transceiver
holes
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
CN201320418660.2U
Other languages
Chinese (zh)
Inventor
麦海波
周毅
李自俊
陈强
吴江
丁发军
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.)
Civil Aviation Flight University of China
Original Assignee
Civil Aviation Flight University of China
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 Civil Aviation Flight University of China filed Critical Civil Aviation Flight University of China
Priority to CN201320418660.2U priority Critical patent/CN203473247U/en
Application granted granted Critical
Publication of CN203473247U publication Critical patent/CN203473247U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a transceiver mounting bracket for a helicopter. The transceiver mounting bracket comprises an upper bracket and a lower bracket, wherein the upper bracket is U-shaped, through holes are formed in the upper surface of the bottom side of the upper bracket, the lower bracket is U-shaped, flanges are arranged at the tops of the two side edges of the lower bracket, mounting holes are uniformly formed in the upper surfaces of the flanges, the lower bracket is connected with the upper bracket through bolts, lightening holes are symmetrically formed in the two side edges of the lower bracket, and flanges are arranged on both the fronts and the rears of the two side edges of the lower bracket. The transceiver mounting bracket has the benefits that the upper bracket is used for being connected with the helicopter, and a transceiver can be conveniently mounted by the lower bracket; the arrangement of the through holes assists the installation of screws and meanwhile plays a lightening function, the weight of the whole bracket can be reduced by the lightening holes to a certain degree, and the strength of the device can be increased by the arrangement of the flanges.

Description

Helicopter transceiver mounting bracket
Technical field
The utility model belongs to mounting bracket field, is specifically related to a kind of helicopter transceiver mounting bracket.
Background technology
Shi Waze 300C type helicopter is a kind of helicopter type of commonly using.At present, the Shi Waze 300C type helicopter self dispatching from the factory is without ADSB system, and generally in the process that installs ADSB system additional producer technical support is not provided.Therefore, be sought after designing a kind of mounting bracket, with this, GDL transceiver in ADSB system be installed.
Summary of the invention
Technical problem to be solved in the utility model is for above-mentioned the deficiencies in the prior art, and a kind of helicopter transceiver mounting bracket is provided, and can easily be connected with helicopter, and be convenient to install transceiver.
The technical scheme that the utility model adopts is: a kind of helicopter transceiver mounting bracket, comprise upper bracket and lower bracket, upper bracket is U-shaped, upper bracket base upper surface has through hole, and described lower bracket is U-shaped, and lower bracket dual-side top is provided with flange, flange upper surface evenly has mounting hole, lower bracket is connected with upper bracket by bolt, and lower bracket dual-side symmetry has lightening hole, is equipped with flange before and after lower bracket dual-side.
As preferably, described upper bracket and lower bracket thickness are 2cm.
As preferably, described bolt is eight.
The beneficial effects of the utility model are: upper bracket is for being connected with helicopter.Lower bracket can be installed transceiver easily.When facilitating screw to install, the arranging of through hole also play the effect of loss of weight.Lightening hole can alleviate the weight of whole support to a certain extent.And flange the intensity that can increase this device is set.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation.
In figure: 1, upper bracket; 2, lower bracket; 3, through hole; 4, flange; 5, bolt; 6, lightening hole.
The specific embodiment
Below in conjunction with the accompanying drawings and the specific embodiments the utility model is described in further detail.
As shown in Figure 1, a kind of helicopter transceiver mounting bracket, comprise upper bracket 1 and lower bracket 2, upper bracket 1 is U-shaped, and upper bracket 1 base upper surface has through hole 3, described lower bracket 2 is U-shaped, lower bracket 2 dual-side tops are provided with flange 4, and flange 4 upper surfaces evenly have mounting hole, and lower bracket 2 is connected with upper bracket 1 by bolt 5, lower bracket 2 dual-side symmetries have lightening hole 6, before and after lower bracket 2 dual-sides, are equipped with flange 4.As preferably, described upper bracket 1 and lower bracket 2 thickness are 2cm.As preferably, described bolt 5 is eight.
During use, by upper bracket 1, this device is arranged on the bottom section of the left seat of helicopter base.Then transceiver is arranged on lower bracket 2.Wherein, lightening hole 6 arranges the weight that can alleviate to a certain extent whole support.And flange 4 the intensity that can increase this support is set.Both are complementary, in the situation of expendable weight, also can guarantee its intensity by actv..

Claims (3)

1. a helicopter transceiver mounting bracket, it is characterized in that: comprise upper bracket and lower bracket, upper bracket is U-shaped, upper bracket base upper surface has through hole, and described lower bracket is U-shaped, and lower bracket dual-side top is provided with flange, flange upper surface evenly has mounting hole, lower bracket is connected with upper bracket by bolt, and lower bracket dual-side symmetry has lightening hole, is equipped with flange before and after lower bracket dual-side.
2. helicopter according to claim 1 transceiver mounting bracket, is characterized in that: described upper bracket and lower bracket thickness are 2cm.
3. helicopter according to claim 1 and 2 transceiver mounting bracket, is characterized in that: described bolt is eight.
CN201320418660.2U 2013-07-15 2013-07-15 Transceiver mounting bracket for helicopter. Expired - Fee Related CN203473247U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320418660.2U CN203473247U (en) 2013-07-15 2013-07-15 Transceiver mounting bracket for helicopter.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320418660.2U CN203473247U (en) 2013-07-15 2013-07-15 Transceiver mounting bracket for helicopter.

Publications (1)

Publication Number Publication Date
CN203473247U true CN203473247U (en) 2014-03-12

Family

ID=50221629

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320418660.2U Expired - Fee Related CN203473247U (en) 2013-07-15 2013-07-15 Transceiver mounting bracket for helicopter.

Country Status (1)

Country Link
CN (1) CN203473247U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140312

Termination date: 20160715

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