Glossary Aircraft Anatomy

Unit Daya Bantu (APU) (APU: Auxiliary Power Unit (APU))

Definition

Mesin kecil di bagian ekor yang menyediakan tenaga listrik dan pendingin udara saat mesin utama mati.

Apa Itu an APU?

An Auxiliary Power Unit (APU) is a small gas turbine engine installed in the tailcone of most commercial aircraft. Unlike the main propulsion engines, the APU is not used for thrust; instead, it generates electrical power and compressed air (bleed air) to operate aircraft systems — air conditioning, avionics, and engine starting — independently of the main engines and without relying on ground support equipment.

Fungsi dan Tujuan

The APU fulfils three core functions. First, it provides electrical power: the APU drives generators that supply 115V AC power (typically 90–120 kVA) to the entire aircraft electrical bus when main engines are shut down at the gate, allowing cabin lighting, galley equipment, entertainment systems, and avionics to operate normally during boarding and deplaning.

Second, it supplies bleed air — high-pressure compressed air extracted from the APU compressor — to the aircraft's pneumatic system. This air powers the air conditioning packs that cool or heat the cabin before engine start and, critically, drives the main engine pneumatic starters, spinning the high-pressure spool up to ignition speed.

Third, the APU serves as an emergency backup: if both main engine generators fail in flight, the APU can be started to restore electrical power. On the Boeing 787, which uses an all-electric architecture (no bleed air from engines), the APU still provides electrical power but does not supply pneumatic bleed air to the cabin systems.

Jenis dan Variasi

  • Standard bleed-air APU: Used on the vast majority of commercial jets (Boeing 737, 747, 777; Airbus A320, A330, A340). Supplies both electrical and pneumatic power.
  • No-bleed APU (Boeing 787): The 787's APU (Honeywell HGT1700) provides only electrical power; the all-electric architecture uses electric compressors for cabin pressurization and engine starting motors instead of bleed air.
  • Integrated drive generator (IDG) APU: Some regional jets integrate the APU function more closely with the main electrical system architecture.

Contoh Penting

The Honeywell 131-9(A) APU powers the Boeing 737 Classic and Next Generation families, producing 90 kVA of electrical power and sufficient bleed air to start both CFM56 engines. The Pratt & Whitney Canada APS3200 serves the Airbus A320 family. The Boeing 787's APU is housed in the composite tailcone of the empennage, accessed through a distinctive louvered exhaust vent visible on the tail.

The APU's bleed air output feeds directly into the same pneumatic manifolds used by the main engines, making it a transparent substitute for ground air carts. The APU exhaust exits through the tail of the aircraft via the empennage tailcone structure. The APU is automatically governed by a dedicated control unit and can be started and stopped from the overhead panel of the cockpit, or in some cases remotely from the ground via maintenance interfaces. Paired with turbofan engine starters, the APU forms a self-sufficient system that eliminates the need for ground starting equipment.

Related Terms

Arsitektur No-Bleed

Filosofi desain pesawat modern yang dipelopori Boeing 787 yang menghilangkan seluruh ekstraksi udara bleed mesin, menggantikan sistem pneumatik dengan kompresor, pompa, dan elemen pemanas elektrik untuk efisiensi bahan bakar dan keandalan yang lebih baik.

Bus Elektrik

Jaringan distribusi daya dalam pesawat yang mengalirkan energi listrik dari generator, APU, atau baterai ke avionik dan sistem, yang diorganisir dalam tingkatan prioritas untuk memastikan peralatan kritis mendapat daya terlebih dahulu.

Empennage

Rakitan ekor pesawat, termasuk stabilizer horizontal dan vertikal.

Sistem Kontrol Lingkungan

Sistem terintegrasi yang menjaga suhu, tekanan, dan kualitas udara kabin dengan mengkondisikan udara bleed mesin atau udara terkompresi secara elektris untuk kenyamanan dan keselamatan penumpang dan awak.

Sistem Pneumatik

Sistem pesawat yang menggunakan udara terkompresi — biasanya diekstrak dari tahap kompresor mesin sebagai udara bleed — untuk pressurization kabin, anti-icing, starting mesin, dan pressurization reservoir hidrolik.

Tekanan Kabin

Tekanan udara yang diatur di dalam badan pesawat untuk menjaga kenyamanan penumpang pada ketinggian jelajah.

Turbin Udara Ram

Turbin darurat kecil yang secara otomatis terbuka ke aliran udara saat terjadi kehilangan daya total, menggunakan udara ram untuk menggerakkan baling-baling yang menghasilkan tekanan hidrolik dan daya listrik untuk kendali penerbangan dan instrumen esensial.

Udara Bleed

Udara bertekanan tinggi dan bersuhu tinggi yang disadap dari tahap kompresor mesin, digunakan untuk pressurization kabin, pendingin udara, de-icing sayap, dan sistem pesawat lainnya.

Frequently Asked Questions

What is Unit Daya Bantu (APU) (APU)?
Mesin kecil di bagian ekor yang menyediakan tenaga listrik dan pendingin udara saat mesin utama mati.
What does APU stand for?
APU stands for Unit Daya Bantu (APU) (APU). Mesin kecil di bagian ekor yang menyediakan tenaga listrik dan pendingin udara saat mesin utama mati.
Why is Unit Daya Bantu (APU) (APU) important in aviation?
Apa Itu an APU? An Auxiliary Power Unit (APU) is a small gas turbine engine installed in the tailcone of most commercial aircraft.
What are examples of Unit Daya Bantu (APU) (APU)?
Common examples of Unit Daya Bantu (APU) (APU) include: The Boeing 787 APU provides electrical power only — no bleed air — due to the aircraft's all-electric architecture., The Honeywell 131-9(A) APU on the Boeing 737 produces 90 kVA and starts both CFM56 engines..
How does Unit Daya Bantu (APU) (APU) relate to other aviation concepts?
Unit Daya Bantu (APU) (APU) is closely related to Arsitektur No-Bleed and Bus Elektrik, among other key aviation concepts.

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