Landing Gear Layout Prof. Rajkumar Pant Aerospace Engineering - PowerPoint PPT Presentation

Landing Gear Layout Prof. Rajkumar Pant Aerospace Engineering Department IIT Bombay AE-332M / 714 Aircraft Design Capsule-2

Introduction  Most difficult subsystem to design & configure  Requirements  Bear static loads while on ground  Allow smooth transition during take-off  Bear impact loads during landing  Provide comfortable ride to the passengers  Desired features  Smallest possible size  Lowest possible weight  Least possible drag  Least complexity during operation and maintenance  Lowest operating cost AE-332M / 714 Aircraft Design Capsule-2

L G is a necessary evil !  Used only for less than 0.5% of a/c life  Many attempts made for disposable LG  Levasseur PL-8  Junkers Ju EF126 Elli  B-52 (in the initial design requirements) AE-332M / 714 Aircraft Design Capsule-2

Levasseur PL-8 White Bird Levasseur PL.8  First to fly across the Atlantic Ocean nonstop (?)  Open-cockpit biplane  One 450 HP Piston Engine  Watertight fuselage that could float on water AE-332M / 714 Aircraft Design Capsule-2

Junkers Ju EF126 Elli  Rapidly producible inexpensive small fighter a/c  Pulsejet powered, with propeller driven startup  RATO, using detachable solid fuel rocket motors  Droppable Take-off dolly, retractable landing skid AE-332M / 714 Aircraft Design Capsule-2

Various Layouts for Landing Gear AE-332M / 714 Aircraft Design Capsule-2

Landing Gear Arrangements AE-332M / 714 Aircraft Design Capsule-2

Tailwheel v/s Nosewheel Type  Nosewheel Type  Tailwheel Type  Most common today  Most common earlier  Also called Tricycle  Also called Tail dragger  MLG strut(s) behind CG  MLG struts ahead of CG  Aux. wheel far ahead  Aux. strut near rear end AE-332M / 714 Aircraft Design Capsule-2

Nosewheel and Tailwheel Type AE-332M / 714 Aircraft Design Capsule-2

Advantages of Nosewheel Type  When on ground, the fuselage, cabin floor of the aircraft are roughly horizontal  The view of the pilot when taxiing is relatively good.  Nosewheel acts as a prop to prevent overturning during braking.  Initial take off attitude has low drag  The nose down pitch resulting from a two point landing helps to shed lift AE-332M / 714 Aircraft Design Capsule-2

Layout of Nosewheel Type AE-332M / 714 Aircraft Design Capsule-2

Advantages of Tailwheel Type  Simplicity  Small and light Tailwheel  Ease in streamlining MLG  Large AOA during ground roll  Large ground clearance for nose propeller  Ease in ground handling  During braking, aircraft tends to pitch nose down  increasing MLG reaction increased  possibility of skidding reduced  Easier to mount MLG onto suitable structure AE-332M / 714 Aircraft Design Capsule-2

Demerits of Tailwheel Type  Instability in landing since CG is behind MLG  If single leg hits ground, then a/c tends to swing in that direction  Pilot has to ensure symmetric landing  Inclined fuselage floor while on ground  Poor pilot visibility during taxiing  Difficulty in Cargo and passenger handling / serving  Increased pressure on fuel pump due to inclination AE-332M / 714 Aircraft Design Capsule-2

Layout of Tailwheel type AE-332M / 714 Aircraft Design Capsule-2

Bicycle Type  Two MLG and small outrigger wheels  Used when  Central fuselage is already occupied  Large CG movement is expected AE-332M / 714 Aircraft Design Capsule-2

Merits and Demerits of Bicycle layout  Disadvantages:  Advantages:  Outriggers necessary  MLG located roughly aft of  The aircraft landing attitude the CG. must be carefully controlled  Wheels are located on the  Considerable elevator centerline of the aircraft power for nosewheel liftoff AE-332M / 714 Aircraft Design Capsule-2

Examples of Bicycle type AE-332M / 714 Aircraft Design Capsule-2

Bicycle landing gear geometry AE-332M / 714 Aircraft Design Capsule-2

Single Wheel Type  Subcategory of the Bicycle Type  Single MLG with small Aux. wheel  Outriggers needed for stability AE-332M / 714 Aircraft Design Capsule-2

Advantages of Single Wheel Type  Simple, lightweight, and low drag  May include skids rather than wheels  Used on light planes like gliders and sailplanes  Generally impractical for larger aircraft  Example: U-2 Reconnaissance aircraft Removable outriggers (Pogos) AE-332M / 714 Aircraft Design Capsule-2

Quadricycle Type  Subset of Bicycle type  MLG at the side of fuselage  Advantages  Low cargo floor for easy loading / unloading  Lateral stability without outrigger wheels AE-332M / 714 Aircraft Design Capsule-2

Multibogey Type  No. of wheels per strut  W TO ≤ 50,000 lb One  50,000 ≤ W TO ≤ 200,000 lb Two  200,000 ≤ W TO ≤ 400,000 lb Four  W TO ≥ 400,000 lb Six AE-332M / 714 Aircraft Design Capsule-2

LG of AN-225 Mriya  Seven pairs of wheels on MLG, two pairs on nosewheels  Possible to adjust pressure of each tire on MLG AE-332M / 714 Aircraft Design Capsule-2

L G layout for higher floatation  Track Type Layout  Reduces loading on runway  Operation from soft ground / unprepared strips AE-332M / 714 Aircraft Design Capsule-2

Landing Gear Layout Prof. Rajkumar Pant Aerospace Engineering - PowerPoint PPT Presentation

Landing Gear Layout Prof. Rajkumar Pant Aerospace Engineering Department IIT Bombay AE-332M / 714 Aircraft Design Capsule-2 Introduction Most difficult subsystem to design & configure Requirements Bear static loads while on

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