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

Emergency Gravity Free-fall Deployment Systems For Retractable Aircraft Landing Gear Assemblies

A deployment system, landing gear technology, applied in the direction of the chassis, etc., which can solve problems such as lack of harmonious movement, ineffective structure and/or equipment, jamming of landing gear doors, etc.

Active Publication Date: 2015-06-24
EMBRAER SA
View PDF5 Cites 11 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] However, additional structures and / or devices to ensure the opening of the gear doors during free fall of the gear are not effective in some cases, for example, in these cases the movement of the gear doors does not have Harmonious movement in the same direction of the landing gear of
In this case there is a real risk that the gear will jam its associated gear door and such an event is certainly unacceptable

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
  • Emergency Gravity Free-fall Deployment Systems For Retractable Aircraft Landing Gear Assemblies
  • Emergency Gravity Free-fall Deployment Systems For Retractable Aircraft Landing Gear Assemblies
  • Emergency Gravity Free-fall Deployment Systems For Retractable Aircraft Landing Gear Assemblies

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0021] According to an embodiment of the present invention, figure 1 The layout of an emergency aircraft landing gear deployment system 10 installed in a transport category aircraft AC is depicted. In this regard, aircraft AC will include conventional port and starboard main and nose gear assemblies, indicated by reference numerals 10-P, 10-S and 10-N, respectively. As is conventional, when each of these assemblies 10-P, 10-S, and 10-N is in a retracted (i.e., flight) state, fuselage grooves (the assemblies retract into these fuselage groove) will be closed by one (or more) landing gear doors 12-P, 12-S and 12-N, respectively, so as to minimize contact with the landing gear assemblies 10-P, 10-S and 10-S during aircraft flight. 10-N and their associated air drag relative to fuselage grooves.

[0022] System 10 includes a pilot-actuated emergency gear deployment lever 14 positioned in a forward crew cab FCC of aircraft AC. The lever is operatively connected to the hydraulic ...

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

Systems are disclosed to allow for the landing gear doors to be opened in the event of an emergency gravity free-fall landing gear deployment with little or no contact with the landing gear tires. The emergency gear extension systems according to the embodiments disclosed herein thus permit the free-fall movement of the landing gear to be synchronized with the opening of the associated gear doors. That is, according to the embodiments disclosed herein deployment of the landing gear assembly is time-delayed relative to the opening of the associated gear door(s). In such a manner, the landing gear assembly is synchronously released only after the associated gear door is in a safe position during its opening sequence thereby avoiding the risk that the gear door will jam the full extension of the landing gear during an emergency gear deployment due to contact between the landing gear tires and the gear door.

Description

technical field [0001] Embodiments disclosed herein relate generally to systems for emergency deployment of retractable aircraft landing gear assemblies. Background technique [0002] Aircraft with retractable landing gear must be provided with a dedicated system as a backup to the aircraft's normal on-board landing gear retract / extend system, which will allow in the event of an emergency (e.g., The normal airborne landing gear extension system is deployed to the extended state) to extend the aircraft's landing gear. Under normal circumstances, all emergency backup gear extension systems should be both easy to operate and completely separate from the normal on-board gear actuation system. [0003] There are several types of emergency backup landing gear extension systems routinely available to aircraft including, for example, electric actuation systems, hydraulic actuation systems, spring actuation systems, and energy transfer systems where the energy to release the landing...

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): B64C25/30B64C25/16
CPCB64C25/16B64C25/30B64C25/20B64C25/22
Inventor 卡洛斯·罗古斯基·菲柳
Owner EMBRAER SA
Features
  • R&D
  • Intellectual Property
  • Life Sciences
  • Materials
  • Tech Scout
Why Patsnap Eureka
  • Unparalleled Data Quality
  • Higher Quality Content
  • 60% Fewer Hallucinations
Social media
Patsnap Eureka Blog
Learn More