Unlock instant, AI-driven research and patent intelligence for your innovation.

Tail steering assembly of model airplane

A component and aircraft model technology, applied in the field of aircraft models, can solve problems such as the influence of pulling arcs, influence on aircraft model steering, tail deformation, etc., to achieve the effect of reducing deformation and improving the overall flight effect

Inactive Publication Date: 2017-05-17
郑华耀
View PDF4 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Generally, the tail servo rod in the tail steering assembly of the aircraft model is connected by a rod. Because the tail servo rod is connected between the tail control unit and the tail servo, the span is too large, and the force on both ends of the rod is too heavy. The tail will be deformed, and when the tail control unit is pulled by the whole tie rod, the angle between the tie rod and the tail control unit is not perpendicular due to the deformation of the tie rod, which will affect the pulling arc to a certain extent, and even affect the steering of the model aircraft during flight. , it is difficult to control the steering of the tail

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Tail steering assembly of model airplane

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0013] The present invention will be further described below in conjunction with the accompanying drawings.

[0014] refer to figure 1 As shown, the tail steering assembly 100 of the present invention is installed at the end of the aircraft model for controlling the steering of the aircraft model. It includes an empennage control unit 1, a tail steering gear 2 and a connecting piece 3. The empennage control unit 1 and the tail steering gear 2 are respectively installed at both ends of the connecting piece 3, and the tail steering gear 2 is used to control the work of the empennage control unit.

[0015] The connecting part 3 includes at least one tail steering gear rod. In this embodiment, the connecting part 3 includes two tail steering gear rods of different lengths, namely the long tail steering gear rod 31 and the short tail steering gear rod 32 . The connector 3 also includes a stern servo cable clip 33, which is composed of a fixing ring 330 and a connecting arm 331. Th...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention provides a tail steering assembly of a model airplane. The tail steering assembly comprises a connecting piece, an empennage control unit and a tail steering engine. The empennage control unit and the tail steering engine are respectively mounted at two ends of the connecting piece, the connecting piece comprises at least one tail steering engine draw bar, and every two corresponding tail steering engine draw bars are connected with each other, are horizontal to each other or are positioned on the same straight line. The tail steering assembly has the advantages that stress on two ends of each original draw bar can be reduced by the sectional tail steering engine draw bars, the shortcomings of excessively high stress on two ends of an existing draw bar due to excessively long connection and influence on movement radian due to deformation of the existing draw bar can be overcome, deformation due to excessively high stress on the draw bars can be reduced, accordingly, stable steering radian of an empennage can be effectively controlled, and integral flight effects of the model airplane which is helicopter can be further enhanced.

Description

technical field [0001] The invention relates to the field of model airplanes, in particular to a tail steering assembly of model airplanes. Background technique [0002] Generally, the tail servo rod in the tail steering assembly of the aircraft model is connected by a rod. Because the tail servo rod is connected between the tail control unit and the tail servo, the span is too large, and the force on both ends of the rod is too heavy. The tail will be deformed, and when the tail control unit is pulled by the whole tie rod, the angle between the tie rod and the tail control unit is not perpendicular due to the deformation of the tie rod, which will affect the pulling arc to a certain extent, and even affect the steering of the model aircraft during flight. , it is difficult to control the steering of the tail. [0003] In view of this, it is necessary to provide a tail steering assembly capable of controlling the steering of the tail more smoothly. Contents of the inventi...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): A63H27/20A63H27/18
Inventor 郑华耀
Owner 郑华耀