This made it possible to carry out a generalized calculation of the required energy characteristics of consumers and the system as a whole for the modes: takeoff, flight and landing, as well as to develop a kinematic diagram and calculate the hydraulic cylinder-lift of the front landing gear....
HYDRAULIC SYSTEM USERS (1)GREEN, BLUE, YELLOW USERS The three independent hydraulic systems respectively supply the users indicated on the diagram. Between these systems, the users are shared in order to ensure the aircraft control, even if only one hydraulic system is inoperative. On the blue ...
In today’s aircraft, hydraulic and pneumatic actuation systems are increasingly being replaced by electrical systems. Actuators for primary flight control surfaces (such as the aileron and the elevator), as well as actuators in landing gear, braking systems, and fuel ...
19 Pump drive system T/M PTO Drive / Full power, Split Shaft PTO Speed control gear box below chassis. Control Provided at Control Panel as well as Cabin 20 Clamp Rings Suitable Qty of Clamp rings for shipment, located at appropriate locations 21 ...
1.11Hydraulicpowersources(supplyingintendedindependentequipment)shouldbesufficientlyindependent? Considermeansofpowergeneration,piperouting,commoncomponents,possibletrajectories,intrinsic risks,etc. 1.12Datainputs(tointendedindependentequipment)shouldalsobeindependenti.e.,alossofasingledata ...
Includes oil, unusable fuel, and hydraulic fluids. Design Gross Weight − W0 The maximum T-O weight for the mission the airplane is designed for. Useful Load − Wu = Wuseful load Useful load is defined as the difference between the design gross weight and the empty weight. It is the...
et al., "Simplified Model Eases Hydraulic System Simulation", pp. 65, 66, Apr. 1978. Primary Examiner: Goldberg, Gerald Assistant Examiner: Roskos, Joseph W. Attorney, Agent or Firm: Christensen, O'Connor, Johnson & Kindness Claims: The embodiments of the invention in which an exclusive ...
system52a. Servo systems52a-52nuse the fuel as a source of hydraulic power to operate the servos which control actuators within an aircraft system. For example, servo system52amay use the fuel provided to it as hydraulic power to drive an actuator that allows compressed air to escape from ...
Accordingly, there is a need in the art for a more versatile aircraft refueling system. SUMMARY OF THE DETAILED DESCRIPTION Embodiments described in the present disclosure include a hydraulic fuel pump apparatus for a fuel delivery chassis, suitable for refueling aircraft, and related devices, ...
Generator 115 is configured to supply electrical power to power system 120, e.g., electrical loads. In addition, in various embodiments, engine 110 may be configured to supply hydraulic power and/or pneumatic power, e.g., bleed air, to power system 120. In one form, power system 120 ...