Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Civil aircraft with special fuel engine

A technology of engines and airliners, which is applied in the field of civil aviation airliners, can solve problems such as fuel shortage, and achieve the effect of long flight time

Inactive Publication Date: 2007-08-08
徐德芳
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0009] The purpose of the present invention is to avoid the shortcomings in the background. The special fuel of the present invention is lighter than the fuel oil of the same volume, the flight time is longer, the exhaust gas discharged is environmentally friendly, and the problem of increasingly scarce fuel oil is solved.

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

Examples

Experimental program
Comparison scheme
Effect test

example 1

[0016] Example 1, the civil aviation airliner of special fuel engine, it is characterized in that, civil aviation airliner is integrally formed by body, wing, fuselage tail balance wing and machine foot rises, retracts system device:

[0017] (1) The aluminum-magnesium alloy sheet is placed in the model of the airframe of the civil aviation airliner, and various parts of the airframe are made after hydraulic pressure, and then assembled and welded into the airframe of the civil aviation airliner.

[0018] (2) Put the aluminum-magnesium alloy sheet into the wing model of the civil aviation airliner, hydraulically make various parts of the wing, and then assemble and weld it into a complete body and wing of the civil aviation airliner.

[0019] (3) Put the aluminum-magnesium alloy sheet into the tail balance wing model of the civil aviation airliner, hydraulically make various parts of the balance wing, and then assemble and weld it into a complete body, wing, and tail balance wi...

example 2

[0021] Example 2, the civil aviation airliner of special fuel engine, it is characterized in that, civil aviation passenger aircraft fuselage both sides at the wing bottom force distance place ascending and descending device system device and body tail balance wing force distance place left and right flight direction device system device;

[0022] (1) Various components of the lifter and lowerer system are precisely made of aluminum-magnesium alloy materials, and then the force distance is installed at the bottom of the wings on both sides of the body, and has the function of automatic control of the lift and lowering.

[0023] (2) Precisely make various parts of the left and right flight direction device system of the passenger aircraft with aluminum-magnesium alloy materials, and then install the balance wing at the rear of the aircraft body, and have the function of automatic control of left and right flight.

example 3

[0024] Example 3, a civil aviation airliner with a special fuel engine, which is characterized in that the special fuel engine system of the civil aviation airliner;

[0025] (1) Equipped with high-pressure gas fuel (methane CH 4 Also known as gas or biogas), a high-pressure aluminum-magnesium alloy bottle is connected with a metal gas pipe, then a gas high-pressure device and a speed controller are connected to the metal gas pipe system, and then a gas high-pressure device The high-pressure gas fuel is connected to the intake pipe of the closed system of the engine with a metal gas pipe, and a qualified hole is set at the closed intake pipe, and a small movable ball is installed in the hole, and the small ball has The air in the small hole can only enter the function, and finally install the dust collector system on the outer opening of the closed air intake pipe.

[0026] (2) The mixed gas fuel enters the engine cylinder, and the intake valve and exhaust valve of the engine...

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 relates to a special fuel powered helicopter. The fighter aircraft comprises the body, tail wing, equilibrator, under chassis automatic alighting and shrink system, alight system at the wing bottom torque, and left and right flight direction system at the equilibrator, special fuel engine system, gear box, impeller, screw, hollow round shell, electric circuit, signal light system, guide system, missile system and special fuel formulation.

Description

technical field [0001] The invention relates to a civil aviation passenger plane with a new type of engine, which is mainly used for transporting passengers by air. The civil aviation airliner of the special fuel engine of the present invention has many machine part systems and the special fuel of the special fuel engine to form: [0002] (1) The civil aviation airliner with special fuel engine is composed of the fuselage, wing, stabilizer at the tail of the fuselage, and the lifting and retracting system of the feet. [0003] (2) Elevator and descender system devices at the moment distance at the bottom of the wing of civil aviation passenger aircraft and left and right flight direction device system devices at the moment distance of the balance wing at the rear of the fuselage. [0004] (3) Special fuel engine systems for civil aviation airliners. [0005] (4) Gearboxes, propellers, propellers and hollow shell devices of civil aviation airliners. [0006] (5) Signal light...

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
Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/02B64C9/00
Inventor 徐德芳
Owner 徐德芳
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com