Flight controller ingress and egress system

A flight controller ingress and egress system is implemented using an assembly. The assembly pivots an outboard flight controller. The pivoting of the outboard flight controller creates a space for the pilot to ingress and egress through the aircraft door more easily. The assembly improves pilot saf...

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1. Verfasser:	Hoover, Douglas E
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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creator	Hoover, Douglas E
description	A flight controller ingress and egress system is implemented using an assembly. The assembly pivots an outboard flight controller. The pivoting of the outboard flight controller creates a space for the pilot to ingress and egress through the aircraft door more easily. The assembly improves pilot safety and convenience when during ingress and egress from the aircraft. The assembly includes a seat bracket, a pivot bracket, a carriage, and a link.
format	Patent
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The assembly includes a seat bracket, a pivot bracket, a carriage, and a link.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB2y8lMzyhRSM7PKynKz8lJLVLIzEsvSi0uVkjMS1FIhTCLK4tLUnN5GFjTEnOKU3mhNDeDoptriLOHbmpBfnxqcUFicmpeakl8aLChkaGxiYm5mZOhMTFqAIVXKdo</recordid><startdate>20241105</startdate><enddate>20241105</enddate><creator>Hoover, Douglas E</creator><scope>EVB</scope></search><sort><creationdate>20241105</creationdate><title>Flight controller ingress and egress system</title><author>Hoover, Douglas E</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US12134476B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2024</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Hoover, Douglas E</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Hoover, Douglas E</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Flight controller ingress and egress system</title><date>2024-11-05</date><risdate>2024</risdate><abstract>A flight controller ingress and egress system is implemented using an assembly. The assembly pivots an outboard flight controller. The pivoting of the outboard flight controller creates a space for the pilot to ingress and egress through the aircraft door more easily. The assembly improves pilot safety and convenience when during ingress and egress from the aircraft. The assembly includes a seat bracket, a pivot bracket, a carriage, and a link.</abstract><oa>free_for_read</oa></addata></record>
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subjects	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
title	Flight controller ingress and egress system
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