D-JET: a New Day Dawning!
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
BUSINESS JETS Oems and Startups Working on Wide Array of New Designs and Derivatives by Matt Thurber Cessna Citation CJ4 Program Launch Date Oct
NEW BUSINESS JETS OEMs and startups working on wide array of new designs and derivatives by Matt Thurber Cessna Citation CJ4 Program launch date Oct. 2006 There are an extraordinary number of business jets in flight test or development First flight date Est. 1H/08 or that were certified during the past 12 months, and indications before this Certification date Est. 1H/10 year’s NBAA Convention were that more new jets are coming from Dassault First delivery date Est. 1H/10 Number of crew and passengers 1 + 8 Falcon, Embraer, Gulfstream and likely other manufacturers. Look for New equipped with a ballistic parachute system Cabin dimensions 17.3 x 4.75 x 4.8 ft designed by Ballistic Recovery Systems. Bizliners in next month’s AIN. Cabin volume N/A Cirrus engineers have refined the jet’s Engine make/model Williams FJ44-4A (2) design in a wind tunnel, with the goal of Engine certification date Est. 1Q/09 bringing to market a jet that combines the Engine thrust rating (sea level, ISA) 3,600 lb IN DEVELOPMENT handling of a Cirrus SR-series piston single Engine derated thrust (sea level, ISA) 3,400 lb with short-field capability and a top speed Avionics suite Rockwell Collins Pro Line 21 CESSNA CITATION CJ4 of 300 knots. The engine is a Williams Inter- MTOW N/A national FJ33-4A-19, which delivers 1,900 MLW N/A The Citation CJ4 takes the single-pilot pounds of thrust. No further specifications ZFW N/A CitationJet into a higher-performance realm are available yet, including the choice of BOW N/A while retaining the signature characteristics avionics manufacturer. -
Very Light Jet Trainer (VLJ) - Phoenix IV
Kennesaw State University DigitalCommons@Kennesaw State University Southern Polytechnic College of Engineering Senior Design Project For Engineers and Engineering Technology Fall 12-3-2020 Very Light Jet Trainer (VLJ) - Phoenix IV Saxton Robinson Eric Gentry Daniyel Holmes Navee Cheng Follow this and additional works at: https://digitalcommons.kennesaw.edu/egr_srdsn Part of the Aerospace Engineering Commons Recommended Citation Robinson, Saxton; Gentry, Eric; Holmes, Daniyel; and Cheng, Navee, "Very Light Jet Trainer (VLJ) - Phoenix IV" (2020). Senior Design Project For Engineers. 45. https://digitalcommons.kennesaw.edu/egr_srdsn/45 This Senior Design is brought to you for free and open access by the Southern Polytechnic College of Engineering and Engineering Technology at DigitalCommons@Kennesaw State University. It has been accepted for inclusion in Senior Design Project For Engineers by an authorized administrator of DigitalCommons@Kennesaw State University. For more information, please contact [email protected]. Very Lightweight Trainer Jet (VLJ) Submitted by Phoenix Aeronautical Company (PAC) Project Manager: Saxton Robinson Chief Engineer: Eric Gentry Master Calculator: Daniyel Holmes Research Advisor: Navee Cheng Submitted to Dr. Adeel Khalid Kennesaw State University | Department of Industrial and Systems Engineering ISYE 4803 Aeronautics Design Project December 3, 2020 This page is left intentionally blank. 2 Executive Summary This project was pursued to bring another possible solution to a major problem within the pilot training industry. When it comes to pilots training with aircraft, they must often use repurposed older aircraft to log their training hours. With few options when it comes to aircraft that are designed specifically for training, we have researched, modeled, and simulated tests for our own trainer jet to add to the market. -
New Business Airplanes
by Chad Trautvetter and expected to fly the twin- engine very light jet (VLJ) by fter a few turbulent years, the business aviation industry is July. However, a nosewheel again strong and healthy, which is reflected by the unprece- shimmy problem occurred dur- dented number of new business aircraft in the works. Last ing high-speed taxi trials, de- year, there were 24 new aircraft in development or flight test; laying first flight until at least athis year there are 35 business aircraft in those categories. last month, if not this month. A majority of the new designs are clean-sheet aircraft, which typically To resolve the issue, ATG early A700 consume more money and time than originally estimated. This is evident last month installed a new nose by the many delays in schedules at established and start-up manufactur- landing gear fitting, which was slated to be tested during more ers alike. However, the start-ups are more vulnerable to these delays, taxi trials last month. which could cause funding to run out or cause new investors to get weak The Williams FJ33-4-17M- knees. This is the case for Safire Aircraft, which closed its doors in June powered Javelin will then be last year after exhausting its available funding to develop the S-26 very cleared for first flight following light jet, prompting us to put the S-26 “on the shelf” for the time being. successful taxi tests with the Speaking of very light jets, the first in this new class of aircraft– new nosewheel configuration. -
Design of Conventional Aircraft
APPENDIX C1: Design of Conventional Aircraft This appendix is a part of the book General Aviation Aircraft Design: Applied Methods and Procedures by Snorri Gudmundsson, published by Elsevier, Inc. The book is available through various bookstores and online retailers, such as www.elsevier.com, www.amazon.com, and many others. The purpose of the appendices denoted by C1 through C5 is to provide additional information on the design of selected aircraft configurations, beyond what is possible in the main part of Chapter 4, Aircraft Conceptual Layout . Some of the information is intended for the novice engineer, but other is advanced and well beyond what is possible to present in undergraduate design classes. This way, the appendices can serve as a refresher material for the experienced aircraft designer, while introducing new material to the student. Additionally, many helpful design philosophies are presented in the text. Since this appendix is offered online rather than in the actual book, it is possible to revise it regularly and both add to the information and new types of aircraft. The following appendices are offered: C1 – Design of Conventional Aircraft (this appendix) C2 – Design of Canard Aircraft C3 – Design of Seaplanes C4 – Design of Sailplanes C5 – Design of Unusual Configurations Figure C1-1: An EDRA Super Petrel LS on final. The airplane combines a number of configuration features presented in appendices C1 and C3; an amphibian, a biplane, and a pusher. (Photo by Phil Rademacher) GUDMUNDSSON – GENERAL AVIATION AIRCRAFT DESIGN APPENDIX C1 – DESIGN OF CONVENTIONAL AIRCRAFT 1 ©2013 Elsevier, Inc. This material may not be copied or distributed without permission from the Publisher. -
Vysoké Učení Technické V Brně Koncepční Studie
VYSOKÉ UČENÍ TECHNICKÉ V BRNĚ BRNO UNIVERSITY OF TECHNOLOGY FAKULTA STROJNÍHO INŽENÝRSTVÍ LETECKÝ ÚSTAV FACULTY OF MECHANICAL ENGINEERING INSTITUTE OF AEROSPACE ENGINEERING KONCEPČNÍ STUDIE LEHKÉHO DVOUMOTOROVÉHO PROUDOVÉHO LETOUNU CONCEPTUAL STUDY OF VERY LIGHT TWIN JET AIRCRAFT DIPLOMOVÁ PRÁCE MASTER'S THESIS AUTOR PRÁCE Bc. MICHAL SMÝKAL AUTHOR VEDOUCÍ PRÁCE Ing. TOMÁŠ URÍK SUPERVISOR BRNO 2015 Vysoké učení technické v Brně, Fakulta strojního inženýrství Letecký ústav Akademický rok: 2014/2015 ZADÁNÍ DIPLOMOVÉ PRÁCE student(ka): Bc. Michal Smýkal který/která studuje v magisterském navazujícím studijním programu obor: Stavba letadel (2301T039) Ředitel ústavu Vám v souladu se zákonem č.111/1998 o vysokých školách a se Studijním a zkušebním řádem VUT v Brně určuje následující téma diplomové práce: Koncepční studie lehkého dvoumotorového proudového letounu v anglickém jazyce: Conceptual study of very light twin jet aircraft Stručná charakteristika problematiky úkolu: Diplomová práce se zabývá studií proveditelnosti lehkého letadla se dvěma proudovými motory. Stěžejní náplní práce je zpracování rešerše letounů obdobného charakteru, stanovení předpisové báze pro návrh a provedení koncepčního aerodynamického návrhu spolu s předběžným výpočet výkonů a vlastností letounu. Součástí práce je i výběr pohonné jednotky, vypracování hmotového rozboru, koncepční návrh hlavních konstrukčních celků a rozbor nákladů na vývoj letounu. Cíle diplomové práce: 1. Zpracování rešerše letounů obdobného charakteru. 2. Koncepční aerodynamický návrh letounu. 3. Předběžný výpočet výkonů a vlastností letounu. 4. Vypracování hmotového rozboru letounu. 5. Koncepční návrh hlavních konstrukčních celků letounu. 6. Stanovení a rozbor nákladů na vývoj letounu. Seznam odborné literatury: [1] Jenkinsin, L. R.: Aircraft design projects for engineering students, AIAA, 2003 [2] Jane´s: All the World's Aircraft (všech vydání) [3] Torenbeek, E.: Synthesis of Subsonic Airplane Design, Delft University Pres, 1976 [4] Roskam, J.: Airplane Design (Parts), The University of Kansas, 1989 [5] Raymer, D. -
Flight 2007 Pocket Guide to Business Aircraft
2007 POCKET GUIDE TO BUSINESS AIRCRAFT ALAN PEAFORD SUPPORTED BY Foreword aviation is probably at its most exciting since the day the BUSINESSworld woke up to Bill Lear’s concept that led to the coining of the phrase “jetsetter.” In 2006 some 13 business aircraft received certification or were first delivered to customers – as we enter 2007 there are close to another 20 business aircraft in serious development. This pocket book was created to bring together all of the aircraft that are First edition published in 2006 by Aerocomm regularly used for business and corporate purposes – and to look too at those aircraft in development that should see certification within the next Aerocomm Ltd couple of years. The Gatehouse The book wouldn’t have been possible without the support of Rockwell 104, Lodge Lane Collins Inc. During the research phase of this 2007 edition the name Rockwell Grays Collins kept popping up as manufacturers talked of development and Essex RM16 2UL improvement in both cockpit and cabin technologies. The Cedar Rapids’ UK company develops smart communications and aviation electronics solutions and it is clear that its technology and innovation has been put to good work in www.aerocomm.co.uk advancing the goals of business aircraft manufacturers around the world. We are proud that the company wanted to be part of this project. www.flightglobal.com I would also like to acknowledge the assistance of the marketing and communication professionals at the aircraft manufacturers who have Copyright © Aerocomm Ltd, Publishers. 2006 painstakingly dealt with our enquiries to help us ensure the accuracy of the data used in the book.