CN104309806A

CN104309806A - Cruise missile carrier vehicle

Info

Publication number: CN104309806A
Application number: CN201410525496.4A
Authority: CN
Inventors: 蒋汉杰; 段卓毅; 蒲宏斌; 任江涛
Original assignee: Xian Aircraft Design and Research Institute of AVIC
Current assignee: Xian Aircraft Design and Research Institute of AVIC
Priority date: 2014-10-08
Filing date: 2014-10-08
Publication date: 2015-01-28

Abstract

The invention belongs to airplane design technology, and relates to a cruise missile carrier vehicle. The cruise missile carrier vehicle comprises an unmanned aerial carrier (1), wherein the aerial carrier (1) is provided with a twin vertical fin and a backpack motor (2); the cruise missile carrier vehicle is characterized in that a semi-buried type magazine is arranged at the belly of the aerial carrier (1) along a fuselage axis from a nose to a tail, and a vertically telescopic cruise missile hanger (4) is arranged in the semi-buried type magazine. According to the cruise missile carrier vehicle provided by the invention, a large cruise missile can be hung and carried, the launching risk of a cruise missile aerial vehicle is reduced, and the research and development cost and the use cost are lowered.

Description

A kind of cruise missile carrying aircraft

Technical field

The invention belongs to airplane design technology, relate to a kind of cruise missile carrying aircraft.

Background technology

Current airborne cruise missile has generally adopted people's operational aircraft carry.Small-sized cruise missile is by fighter plane carry, but the range of guided missile is limited, and needing fighter plane to approach Operation Target could launch, and increases the transmitting risk of fighter plane under the air defence system condition of advanced person.Large-scale cruise missile generally has large-scale bomber carry, although the range of guided missile is comparatively far away, reduce the threat of enemy air defences system to carrier aircraft, research and development and the operating costs of large-scale bomber are high, and the R&D cycle is long, are difficult to equip our troops on a large scale.

Summary of the invention

The object of the invention is: propose a kind of cruise missile carrying aircraft, to reduce the transmitting risk of carrier aircraft, reduce R & D Cost and operating costs.

Technical scheme of the present invention is: a kind of cruise missile carrying aircraft, and comprise a unpiloted carrier aircraft 1, carrier aircraft 1 is with twin vertical fin and backpack driving engine 2; It is characterized in that: there are one and half buried magazines at carrier aircraft 1 ventral place along fuselage axis from head to tail, in half buried magazine, have a cruise missile hanger 4 that can stretch up and down, the lower end of cruise missile hanger 4 is connected with the sling point of cruise missile 3; When cruise missile hanger 4 is positioned at upper extreme position, cruise missile 3 is accommodated in half buried magazine of carrier aircraft 1, the inwall of the first half profile of cruise missile 3 body and half buried magazine of carrier aircraft 1 fits, the lower part profile of cruise missile 3 body and the outer surface smoother transition of carrier aircraft 1 fuselage, the fairing of cruise missile 3 front end forms the nose-ring of carrier aircraft 1; When cruise missile hanger 4 is positioned at lower limit position, cruise missile 3 leaves half buried magazine of carrier aircraft 1, keeps secure transmission distance with carrier aircraft 1.

Advantage of the present invention is: propose a kind of cruise missile carrying aircraft, can the large-scale cruise missile of carry, reduces the transmitting risk of cruise missile carrier aircraft, reduces R & D Cost and operating costs.

Accompanying drawing explanation

Fig. 1 is structural principle schematic diagram of the present invention, and this figure shows schematic side view when cruise missile is accommodated into carrier aircraft half buried magazine.

Fig. 2 is the left view of Fig. 1.This figure shows front-view schematic diagram when cruise missile is accommodated into carrier aircraft half buried magazine.

Fig. 3 is the schematic side view of cruise missile when stretching out carrier aircraft half buried magazine.

Fig. 4 is the front-view schematic diagram of cruise missile when stretching out carrier aircraft half buried magazine.

Detailed description of the invention

Below the present invention is described in further details.See Fig. 1 to Fig. 4, a kind of cruise missile carrying aircraft, comprise a unpiloted carrier aircraft 1, carrier aircraft 1 is with twin vertical fin and backpack driving engine 2; It is characterized in that: there are one and half buried magazines at carrier aircraft 1 ventral place along fuselage axis from head to tail, in half buried magazine, have a cruise missile hanger 4 that can stretch up and down, the lower end of cruise missile hanger 4 is connected with the sling point of cruise missile 3; When cruise missile hanger 4 is positioned at upper extreme position, cruise missile 3 is accommodated in half buried magazine of carrier aircraft 1, the inwall of the first half profile of cruise missile 3 body and half buried magazine of carrier aircraft 1 fits, the lower part profile of cruise missile 3 body and the outer surface smoother transition of carrier aircraft 1 fuselage, the fairing of cruise missile 3 front end forms the nose-ring of carrier aircraft 1; When cruise missile hanger 4 is positioned at lower limit position, cruise missile 3 leaves half buried magazine of carrier aircraft 1, keeps secure transmission distance with carrier aircraft 1.

Principle of work of the present invention is: adopt backpack engine type, for the layout of built-in type magazine provides structure space, is also conducive to the radar scattering shielding engine compressor blade simultaneously, improves Stealth Fighter.Adopt the design of built-in type magazine, add cruise missile body lower part profile and the transition of fuselage outer surface smoother, reduce the interference drag of cruise missile and carrier aircraft, improve 1ift-drag ratio, when adding boat and voyage.The front end fairing of cruise missile forms the nose-ring of carrier aircraft, is convenient to the target seeker search of cruise missile and identification target.

One embodiment of the present of invention, when the cruise missile length of carry is 10m, the length of full machine is 12m, span 14m, take-off weight 14t, and carrier aircraft combat radius is 500Km, and the range of cruise missile is greater than 2000Km.

Claims

1. a cruise missile carrying aircraft, comprises a unpiloted carrier aircraft (1), and carrier aircraft (1) is with twin vertical fin and backpack driving engine (2); It is characterized in that: there are one and half buried magazines at carrier aircraft (1) ventral place along fuselage axis from head to tail, in half buried magazine, have the cruise missile hanger (4) that can be stretched up and down, the lower end of cruise missile hanger (4) is connected with the sling point of cruise missile (3); When cruise missile hanger (4) is positioned at upper extreme position, cruise missile (3) is accommodated in half buried magazine of carrier aircraft (1), the inwall of the first half profile of cruise missile (3) body and half buried magazine of carrier aircraft (1) fits, the lower part profile of cruise missile (3) body and the outer surface smoother transition of carrier aircraft (1) fuselage, the fairing of cruise missile (3) front end forms the nose-ring of carrier aircraft (1); When cruise missile hanger (4) is positioned at lower limit position, cruise missile (3) leaves half buried magazine of carrier aircraft (1), keeps secure transmission distance with carrier aircraft (1).