TEAM DO NOW: DAY # Lesson # September 8, 2015 1. List the three primary flight control surfaces. 2. What is the purpose of the trim tab? 3. Explain the.

Slides:



Advertisements
Similar presentations
Uncontrolled copy not subject to amendment
Advertisements

Airframes and Environmentals
4 2 . Parts of the Airplane.
Aerospace Materials Failure Modes
Chapter 33 Heavy-duty Truck Trailers. Objectives (1 of 2) Describe what is meant by semi-trailers and full trailers. Identify the various different tractor/trailer.
The Fuselage and Empennage
Chapter 34 Bridge Construction.
Theory Of Flight 1 PO 402 CI Norwood
Basic Aircraft Structure
Lesson 13: Aircraft Structures And Flight Controls
 Key Learning ◦ Various shaped objects offer different strengths.  Unit Essential Question ◦ Why is it important to know the strengths of various shaped.
AVIATION HISTORY Lecture 10 : Airliners. OBJECTIVES  By end of this section, students will be able to explain:  About Boeing & Airbus aircraft,  Why.
BATTAGLIA MARIO FACCIO PEDRO SALAZAR ANDRES 2015 SAE Aero Design East Competition Faculty Advisor: Dr. Dulikravich.
DO NOW April 17, ) Explain how lift is achieved.
The Airplane.
CLARKSON UNIVERSITY Department of Mechanical and Aeronautical Engineering Introduction to AIRCRAFT STRUCTURES Ratan Jha (CAMP 364, ,
AE2302 AIRCRAFT STRUCTURES-II
1 AE 440 Structures Discipline Lecture 6 Eric Loth For AE 440 A/C Lecture.
The History of Aircraft Materials
132,000 sq ft  Fabrication  Composite Structures  Cabin Interiors  Structural Bondments  Compression Molding  Vacuum Forming  NDI  Composite Assembly.
SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 Design.
Prof. Carlos Montestruque
ELEMENT OF AERONAUTICS
Engineering & Beyond Workshop 2005 Civil Engineering Civil, Construction and Environmental Engineering Department.
Ken YoussefiUC Berkeley 1 Structural, Piping, and Welding Drawings.
INTRODUCTION TO THE COURSE
Warm-Up – 8/25 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the four forces of flight? Describes what.
Roof and Ceiling Framing
AE 1350 Lecture Notes #12. Topics to be Studied Importance of Structural Weight and Integrity Development of Aircraft Structures Elements of Aircraft.
AVIATION HISTORY Lecture 10 : Airliners. OBJECTIVES  By end of this section, students will be able to explain:  About Boeing & Airbus aircraft,  Why.
Airplanes By : Hebron Yam,Justin Minucci. How do airplane work? Problem???
Western Hills HS Aeronautical Engineering A Primer to Aircraft Structure and Design: Project Lead the Way - A Discussion on Career Potential and Opportunities.
INTRODUCTION TO THE COURSE
Overview Project Schedule Competition Technology Report Construction Progress Future Work Conclusion.
SR-71 Blackhawk Flight & Space $100 $200 $300 $400 $500 $100 $200 $300 $400 $500 $100 $200 $300 $400 $500 $100 $200 $300 $400 $500 $100 $200 $300 $400.
By Bala Dhareneni.  The fuselage, or body of the airplane, is a long hollow tube which holds all the pieces of an airplane together. The fuselage is.
Utilizing your notes and past knowledge answer the following questions: 1) What parts of the aircraft are included within the empennage? 2) What is the.
AE1202 ELEMENTS OF AERONAUTICS Semester III AERONAUTICAL ENGINEERING Handled by K.PADMANABAN.
West Point Bridge Designer Capstone Course Orientation.
Basic Aircraft Structure
Problems 1. A large plate is fabricated from a steel alloy that has a plane strain fracture toughness of 82.4MPa√m. If, during service use, the plate is.
Warm-Up – 9/9 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the two most popular types of fuselage structures?
National Institute of Technology, Rourkela Role of Composites for gradual improvement of Aircraft Structure Presented By: Ajit Behera Roll no- 210MM1248.
Utilizing your notes and past knowledge answer the following questions: 1) What part of the aircraft is located on the outer portion of the trailing edge.
By Sajad Fadhil A. AL Hussain
6.01 Aircraft Design and Construction References: FTGU pages 9-14, 27
Basic Aircraft Structure
Basic Aircraft Structure
SAE Aero 2017 Midterm Presentation Joe Zongolowicz, Nick Montana, Frank Dixon, Kevin Scheventer, Kathy Hansen, Marquis Ward, Gerald Short, Zhangsiwen Xiao,
Aerospace System Prototyping and Validation- Lecture 2
A321 EMERGENCY EXITS PRESENTATION.
Aircraft Classifications
Design Refining a design.
4 2 . Parts of the Airplane.
Warm-Up – 9/5 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the four forces of flight? Describes what.
The Airplane Chapter 4 Airframe.
Introduction- The Airplane
SAE Aero East 2017 MAE 434W. SAE Aero East 2017 MAE 434W.
MGMT 203 Aerodynamics from a Management Standpoint
MGMT 203 Aerodynamics from a Management Standpoint
c/Maj Christopher Greves
DO NOW 1. Identify 3 major aerospace manufacturing companies.
The Fuselage and Empennage
SAE Aero East 2017 MAE 435 Mid-Term Progress Presentation
NİŞANTAŞI ÜNİVERSİTESİ
Basic Aircraft Structure
Warm-Up – 1/18 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the two most popular types of fuselage structures?
DAILY INSPECTION Purpose:
Structures PDR #1 AAE451 – Team 3 October 28, 2003
Forces of Flight Flight and Space © 2011 Project Lead The Way, Inc.
Presentation transcript:

TEAM DO NOW: DAY # Lesson # September 8, List the three primary flight control surfaces. 2. What is the purpose of the trim tab? 3. Explain the purpose and function of the aileron.

Focus Point: What are the Fuselage Structural Components? Instructional Objectives: 1. List three types of aircraft fuselages. 2. Explain the difference between full & semi monocoque. 3. Describe components of each.

I) What is the Fuselage? 1. Comes from the French word “fusele” meaning spindle shaped. 2. The main body or body portion of the airplane. 3. Supports the tail assembly. 4. Central structure to which all other components (engines, wheels, wings) of the airplane are attached. 5. Carries the payload and crew.(second main purpose).

II) Fuselage Constructions: 1. Truss Type: A. Constructed of steel tubing, carries tension and compression loads. Covered with cotton or fabric.

B. Length wise members are called longerons, carrying all the main forward and aft loads. Truss Type:

2. Monocoque Type: A) Full Monocoque: 1.Stressed skin construction, skin provides strength of structure. 2. Found on small aircraft, similar to an egg 3. It is an single shell relies on the strength of the skin for primary stresses.

B) Semimonocoque Type: 2. Constructed of alloys of aluminum and magnesium. 1. Used on most large aircraft. 3. Most of the strength is in the skin, skin is supported on a substructure of formers and stringers that give the skin its shape. *Alloy: combination of 2 or more metals.

Additional strength is provided in a semi- monocoque structure by a substructure that reinforces the skin.

Photo courtesy Airbus SAS A380 fuselage components on the Garonne river, crossing the Pont de Pierre in Bordeaux, FranceAirbus SAS

A380 fuselage components on the Garonne river, crossing the Pont de Pierre in Bordeaux, France

Summary - Accountable Talk: 1) What are the three types of fuselage structures? 2) What is the truss type fuselage? 3) Explain the semi - monocoque fuselage. Lesson # September 8, 2015